Solid Mechanics System Design Description

This template follows INL template TEM-140, "IT System Design Description."

note

This document serves as an addendum to Framework System Design Description and captures information for SDD specific to the Solid Mechanics module.

Framework System Design Description

Introduction

Computing mechanical deformation of solids or structures is important for a variety of applications. These can employ a variety of assumptions of material behavior, and can be either run as standalone single-physics problems or couple the mechanical response with that of other physics. The MOOSE Solid Mechanics module provides a foundational set of models for modeling mechanical deformation. This module relies on MOOSE for solving its system of equations, and is designed to be readily extended or coupled with other physics models. This document describes the system design of the Solid Mechanics module.

System Purpose

The Software Design Description provided here is description of each object in the system. The pluggable architecture of the underlying framework of the Solid Mechanics module makes MOOSE and MOOSE-based applications straightforward to develop as each piece of end-user (developer) code that goes into the system follows a well-defined interface for the underlying systems that those object plug into. These descriptions are provided through developer-supplied "markdown" files that are required for all new objects that are developed as part of the Solid Mechanics module. More information about the design documentation for MOOSE-based applications and like the Solid Mechanics module can be found in Documenting MOOSE.

System Scope

The MOOSE Solid Mechanics module provides an extensible set of capabilities for solving for mechanical deformation of solids and structures. It provides a set of C++ base classes that define interfaces for MOOSE Material objects that compute various mechanical behavior of materials at quadrature points, which include elastic properties, strains, eigenstrains, stresses, inelastic behavior, and damage. It also provides the needed Kernel classes to account for the contributions of the stress, inertia and damping in the solution for the displacement field that satisfies equilibrium. These models support one-, two-, and three-dimensional models of continuous materials, with variety of options for the treatment of the lower-dimensional models, including plane stress, plane strain, axisymmetry, and generalized plane strain. These models support both small- and finite-strain assumptions.

For modeling discrete interfaces between solid elements, this module provides a system similar to that for continuous materials that permits the definition of traction-separation laws for cohesive behavior. It also has similar support for lower-dimensional elements to represent structural elements such as beams and shells. As for the continuum models, sets of Material and Kernel classes are defined for these cases.

This module also provides a comprehensive set of boundary conditions relevant for mechanics modeling, such as pressure and traction boundary conditions. It also provides extensive postprocessing capabilities for computing quantities relevant to mechanics, such as fracture integrals.

In addition to defining the base classes that enable modeling arbitrary materials, this module also provides a set of specializations of those models for widely-used assumptions of material behavior. These include elasticity tensors defined in a variety of ways for isotropic and anisotropic materials, basic creep, plasticity and damage models, and models for eigenstrains due to thermal expansion.

Dependencies and Limitations

The MOOSE Solid Mechanics module inherits the software dependencies of the MOOSE framework, with no additional dependencies.

Definitions and Acronyms

This section defines, or provides the definition of, all terms and acronyms required to properly understand this specification.

Definitions

Pull (Merge) Request: A proposed change to the software (e.g. usually a code change, but may also include documentation, requirements, design, and/or testing).
Baseline: A specification or product (e.g., project plan, maintenance and operations (M&O) plan, requirements, or design) that has been formally reviewed and agreed upon, that thereafter serves as the basis for use and further development, and that can be changed only by using an approved change control process (NQA-1, 2009).
Validation: Confirmation, through the provision of objective evidence (e.g., acceptance test), that the requirements for a specific intended use or application have been fulfilled (24765:2010(E), 2010).
Verification: (1) The process of: evaluating a system or component to determine whether the products of a given development phase satisfy the conditions imposed at the start of that phase. (2) Formal proof of program correctness (e.g., requirements, design, implementation reviews, system tests) (24765:2010(E), 2010).

Acronyms

Acronym	Description
API	Application Programming Interface
DOE-NE	Department of Energy, Nuclear Energy
FE	finite element
HIT	Hierarchical Input Text
HPC	High Performance Computing
I/O	Input/Output
INL	Idaho National Laboratory
MOOSE	Multiphysics Object Oriented Simulation Environment
MPI	Message Passing Interface
SDD	Software Design Description

Design Stakeholders and Concerns

Design Stakeholders

Stakeholders for MOOSE include several of the funding sources including DOE-NE and the INL. However, Since MOOSE is an open-source project, several universities, companies, and foreign governments have an interest in the development and maintenance of the MOOSE project.

Stakeholder Design Concerns

Concerns from many of the stakeholders are similar. These concerns include correctness, stability, and performance. The mitigation plan for each of these can be addressed. For correctness, Solid Mechanics module development requires either regression or unit testing for all new code added to the repository. The project contains several comparisons against analytical solutions where possible and also other verification methods such as MMS. For stability, the Solid Mechanics module (located within the MOOSE repository) maintains multiple branches to incorporate several layers of testing both internally and for dependent applications. Finally, performance tests are also performed as part of the the normal testing suite to monitor code change impacts to performance.

System Design

The MOOSE Solid Mechanics module relies on MOOSE to solve the equilibrium equations governing mechanical deformation, which can include contributions from the mechanical deformation models provided by this module, accounting for the couplings that may occur between the mechanical models and other physics models. The design of MOOSE is based on the concept of modular code objects that define all of the aspects of the physics model. This module follows this design, providing code objects that define specific aspects of the solutions for its physics that derive from the base classes defined by the MOOSE framework and the modules that it depends on.

The Solid Mechanics module provides specialized Kernel classes that compute the contributions from the terms in the partial differential equations governing mechanical deformation. It also provides specialized Material classes that define the constitutive behavior of solid materials. In addition, it provides BC, Action, Postprocessor and VectorPostprocessor classes to facilitate various aspects of these simulations.

System Structure

The MOOSE Solid Mechanics module relies on the MOOSE framework to provide the core functionality of solving multiphysics problems using the finite element method. The structure of the Solid Mechanics module is based on defining C++ classes that derive from classes in the MOOSE framework to provide functionality for solution of mechanics problems. By using the interfaces defined in MOOSE base classes for these classes, this module is able to rely on MOOSE to execute these models at the appropriate times during the simulation and use their results in the desired ways.

Data Design and Control

At a high level, the system is designed to process HIT input files to construct several objects that will constitute an FE simulation. Some of the objects in the simulation may in turn load other file-based resources to complete the simulation. Examples include meshes or data files. The system will then assemble systems of equations and solve them using the libraries of the Code Platform. The system can then output the solution in one or more supported output formats commonly used for visualization.

Human-Machine Interface Design

The Solid Mechanics module is a command-line driven program. All interaction with the Solid Mechanics module is ultimately done through the command line. This is typical for HPC applications that use the MPI interface for running on super computing clusters. Optional GUIs may be used to assist in creating input files and launching executables on the command line.

System Design Interface

All external system interaction is performed either through file I/O or through local API calls. Neither the Solid Mechanics module, nor the MOOSE framework, nor the other MOOSE modules are designed to interact with any external system directly through remote procedure calls. Any code to code coupling performed using the framework are done directly through API calls either in a static binary or after loading shared libraries.

Security Structure

The Solid Mechanics module does not require any elevated privileges to operate and does not run any stateful services, daemons or other network programs. Distributed runs rely on the MPI library.

Requirements Cross-Reference

solid_mechanics: Generalized Plane Strain Action
8.1.1The system shall support generalized plane strain with incremental strain for 1D meshes using the SolidMechanics/QuasiStatic Physics.
Specification(s): axisymmetric_gps_incremental
Design: Generalized Plane Strain Action
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.1.2The system shall support generalized plane strain with small strain for 1D meshes using the SolidMechanics/QuasiStatic Physics.
Specification(s): axisymmetric_gps_small
Design: Generalized Plane Strain Action
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.1.3The system shall support generalized plane strain with finite strain for 1D meshes using the SolidMechanics/QuasiStatic Physics.
Specification(s): axisymmetric_gps_finite
Design: Generalized Plane Strain Action
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.8The system shall support setting up a generalized plane strain problem through an action
Specification(s): generalized_plane_strain_squares
Design: Generalized Plane Strain Action
Issue(s): #7840
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.9The system shall support setting the out-of-plane pressure using a function for generalized plane strain problems
Specification(s): out_of_plane_pressure_function
Design: Generalized Plane Strain Action
Issue(s): #7840
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.10The system shall support setting the out-of-plane pressure using a material property for generalized plane strain problems
Specification(s): out_of_plane_pressure_material
Design: Generalized Plane Strain Action
Issue(s): #17250
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.11The system shall support listing all of the out-of-plane strain variables in the strain calculator
Specification(s): generalized_plane_strain_scalar_vector
Design: Generalized Plane Strain Action
Issue(s): #7840
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Axisymmetric 1D Incremental Strain
8.1.4The ComputeAxisymmetric1DIncrementalStrain class shall compute the elastic stress for a 1D axisymmetric small incremental strain formulation under a combination of applied tensile displacement and thermal expansion loading using the SolidMechanics/QuasiStatic Physics.
Specification(s): axisymmetric_plane_strain_incremental
Design: Compute Axisymmetric 1D Incremental Strain
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.1.7The ComputeAxisymmetric1DIncrementalStrain class shall, under generalized plane strain conditions, compute the elastic stress for a 1D axisymmetric small incremental strain formulation under a combination of applied tensile displacement and thermal expansion loading.
Specification(s): axisymm_gps_incremental
Design: Compute Axisymmetric 1D Incremental Strain
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Axisymmetric 1D Small Strain
8.1.5The ComputeAxisymmetric1DSmallStrain class shall compute the elastic stress for a 1D axisymmetric small total strain formulation under a combination of applied tensile displacement and thermal expansion loading using the SolidMechanics/QuasiStatic Physics.
Specification(s): axisymmetric_plane_strain_small
Design: Compute Axisymmetric 1D Small Strain
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.1.8The ComputeAxisymmetric1DSmallStrain class shall, under generalized plane strain conditions, compute the elastic stress for a 1D axisymmetric small total strain formulation under a combination of applied tensile displacement and thermal expansion loading.
Specification(s): axisymm_gps_small
Design: Compute Axisymmetric 1D Small Strain
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Axisymmetric 1D Finite Strain
8.1.6The ComputeAxisymmetric1DFiniteStrain class shall compute the elastic stress for a 1D axisymmetric incremental finite strain formulation under a combination of applied tensile displacement and thermal expansion loading using the SolidMechanics/QuasiStatic Physics.
Specification(s): axisymmetric_plane_strain_finite
Design: Compute Axisymmetric 1D Finite Strain
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.1.9The ComputeAxisymmetric1DFiniteStrain class shall, under generalized plane strain conditions, compute the elastic stress for a 1D axisymmetric incremental finite strain formulation under a combination of applied tensile displacement and thermal expansion loading.
Specification(s): axisymm_gps_finite
Design: Compute Axisymmetric 1D Finite Strain
Issue(s): #8045 #14606
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.1.10The StressDivergenceRZTensors class shall generate an error if used with Problem/rz_coord_axis set to anything other than Y
Specification(s): 1d_finite_rz_coord_axis_error
Design: Compute Axisymmetric 1D Finite Strain
Issue(s): #8045 #14606
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Compute R-Spherical Incremental Strain
8.2.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.21We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation. (non-AD reference)
Specification(s): rspherical_incremental_small_elastic-noad
Design: Compute R-Spherical Incremental Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Finite Strain Elastic Stress
8.2.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.1The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes.
Specification(s): elastic_patch
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.2The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.
Specification(s): elastic_patch_incremental_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.4The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.
Specification(s): elastic_patch_incremental_small_no_disp_mesh
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584 #12580
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.5The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.
Specification(s): elastic_patch_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.6The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when running on 2 processors in parallel.
Specification(s): elastic_patch_2Procs
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.7The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.
Specification(s): elastic_patch_2Procs_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.8The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular 20-noded quadratic hexes.
Specification(s): elastic_patch_quadratic
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #620
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.1The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.
Specification(s): new
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.2The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.
Specification(s): new_Bbar
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Volumetric Locking Correction
Issue(s): #8235 #4716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.5The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the QuasiStatic SolidMechanics Physics.
Specification(s): rotation_new
Design: Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.6The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the volumetric locking correction b-bar formulation.
Specification(s): rotation_new_Bbar
Design: Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #4716 #8235
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.7The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.
Specification(s): eigen_sol
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.8The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.
Specification(s): eigen_sol_Bbar
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Volumetric Locking Correction
Issue(s): #8235 #4716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.9The ComputeLinearElasticStress class shall generate an error if a user attempts to run a problem using ComputeLinearElasticStress with a finite strain formulation.
Specification(s): stress_errorcheck
Design: Compute Finite Strain Elastic Stress Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.50.1Finite strain methods in Tensor Mechanics should be able to adequately simulate a complex strain state simulation in 3D using an orhotropic filling with isotropic properties.
Specification(s): 3d_isotropic
Design: Compute Finite Strain Elastic Stress
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.50.2Finite strain methods in Tensor Mechanics should be able to adequately simulate a complex strain state simulation in 3D using an orhotropic filling with isotropic properties.
Specification(s): 3d_orthotropic_isotropic
Design: Compute Finite Strain Elastic Stress
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.50.3Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 90 degrees and retrieve the proper displacement after being solicited by a pressure boundary condition.
Specification(s): 3d_bar_orthotropic_90deg_rotation
Design: Compute Finite Strain Elastic Stress
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.50.4Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 90 degrees and retrieve the proper displacement after being solicited by a pressure boundary condition when automatic differentiation is used.
Specification(s): 3d_bar_orthotropic_90deg_rotation_ad
Design: Compute Finite Strain Elastic Stress
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.50.5Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 360 degrees and retrieve the proper displacement after being solicited by a pressure boundary condition.
Specification(s): 3d_bar_orthotropic_full_rotation
Design: Compute Finite Strain Elastic Stress
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.50.6Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 360 degrees and retrieve the proper displacement after being solicited by a pressure boundary condition when automatic differentiation is used.
Specification(s): 3d_bar_orthotropic_full_rotation_ad
Design: Compute Finite Strain Elastic Stress
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Solid Mechanics QuasiStatic Physics System
8.2.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.8The QuasiStatic SolidMechanics Physics shall calculate the elastic stress and strain response for a 3D pressurized hollow cylinder with a large strain incremental strain formulation.
Specification(s): 3D_RZ_finitestrain
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.1The QuasiStatic SolidMechanics Physics shall support changing the base name when creating a consistent strain calculator material and stress divergence kernel and shall generate different sets of outputs for different mesh subblocks with the appropriate base name.
Specification(s): two_block_base_name
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #13860
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.2The QuasiStatic SolidMechanics Physics shall create a consistent strain calculator material and stress divergence kernel and shall generate different sets of outputs for different mesh subblocks.
Specification(s): two_block_new
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.3The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks requesting different strain formulations.
Specification(s): two_block
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.4The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks requesting different strain formulations with the new kernel system.
Specification(s): two_block_lagrangian
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.5The QuasiStatic SolidMechanics Physics shall error if an input file does not specify block restrictions for the MasterAction in input files with more than one instance of the MasterAction block.
Specification(s): two_block.error_unrestricted
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.7.6The QuasiStatic SolidMechanics Physics shall error if an input file specifies overlapping block restrictions for the MasterAction in input files with more than one instance of the MasterAction block.
Specification(s): two_block.error_overlapping
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.7.7The QuasiStatic SolidMechanics Physics shall warn if global Master action parameters are supplied but no Master action subblock have been added.
Specification(s): no_block
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.7.8The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks using different coordinate systems.
Specification(s): two_coord
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.9The QuasiStatic SolidMechanics Physics shall error if an input file assigns the same QuasiStatic SolidMechanics Physics block to mesh blocks with different coordinate systems.
Specification(s): two_coord.error_different_coords
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.7.10The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console.
Specification(s): action_eigenstrain
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.11The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console.
Specification(s): action_multi_eigenstrain
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.12The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console.
Specification(s): action_multi_eigenstrain_same_conditions
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.13The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console.
Specification(s): ad_converter_action_multi_eigenstrain
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.14The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console.
Specification(s): reduced_eigenstrain_action
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.15The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console.
Specification(s): composite_eigenstrain
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.16The QuasiStatic SolidMechanics Physics shall determine the necessary orders and families to apply to material outputs.
Specification(s): material_output_order.empty
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.17The QuasiStatic SolidMechanics Physics shall apply a single given output order to all output variables.
Specification(s): material_output_order.single
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.18The QuasiStatic SolidMechanics Physics shall apply a single given output family to all output variables.
Specification(s): material_output_order.family_single
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): RunApp
8.7.19The QuasiStatic SolidMechanics Physics shall error if an the material outputs and or families do not match the number of material outputs.
Specification(s): material_output_order.error1
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.7.20The QuasiStatic SolidMechanics Physics shall determine the necessary orders and families to apply to material outputs.
Specification(s): material_output_first_lagrange_manual
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.21The QuasiStatic SolidMechanics Physics shall determine the necessary orders and families to apply to material outputs.
Specification(s): material_output_first_lagrange_automatic
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.7.22The QuasiStatic SolidMechanics Physics shall permit scalar quantity output from arbitrary tensors.
Specification(s): custom_output
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555 #15871
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.4The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.5The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere_incremental-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.6The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): finiteStrain_1DSphere_hollow-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.10.1The QuasiStatic SolidMechanics Physics shall create a consistent strain calculator material and stress divergence kernel and shall generate different sets of outputs for different mesh subblocks.
Specification(s): two_block_new
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.10.2The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks requesting different strain formulations.
Specification(s): two_block
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.10.3The QuasiStatic SolidMechanics Physics shall error if an input file does not specify block restrictions for the MasterAction in input files with more than one instance of the MasterAction block.
Specification(s): error_unrestricted
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.10.4The QuasiStatic SolidMechanics Physics shall error if an input file specifies overlapping block restrictions for the MasterAction in input files with more than one instance of the MasterAction block.
Specification(s): error_overlapping
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.10.5The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks using different coordinate systems.
Specification(s): two_coord
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.10.6The QuasiStatic SolidMechanics Physics shall error if an input file assigns the same QuasiStatic SolidMechanics Physics block to mesh blocks with different coordinate systems.
Specification(s): error_coord
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.10.7The Jacobian for the automatic differentiation in the two_block testproblem shall be perfect
Specification(s): two_block-jac
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.10.8The Jacobian for the automatic differentiation in the two_block testproblem shall be perfect (non action test case)
Specification(s): two_block_no_action-jac
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.10.9The Jacobian for the automatic differentiation in the two_block_new problem shall be perfect
Specification(s): two_block_new-jac
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.10.10The Jacobian for the automatic differentiation two_coord problem shall be perfect
Specification(s): two_coord-jac
Design: Solid Mechanics QuasiStatic Physics System
Issue(s): #7555
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.24.1The mechanics system shall be capable of accurately computing the elastic response of an anisotropic elastic material where 6 components of a symmetric elasticity tensor are output on an irregular patch of elements with total small strain assumptions
Specification(s): test
Design: Compute Linear Elastic Stress Compute Small Strain Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.1The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.
Specification(s): new
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.5The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the QuasiStatic SolidMechanics Physics.
Specification(s): rotation_new
Design: Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.7The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.
Specification(s): eigen_sol
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.9The ComputeLinearElasticStress class shall generate an error if a user attempts to run a problem using ComputeLinearElasticStress with a finite strain formulation.
Specification(s): stress_errorcheck
Design: Compute Finite Strain Elastic Stress Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.53.1The tensor mechanics action shall set up the mechanics kernels with the appropriate options to accumulate absolute values of the residual to a tag vector usable for relative convergence checks.
Specification(s): free_expansion_abs_ref
Design: Solid Mechanics QuasiStatic Physics System ReferenceResidualProblem
Issue(s): #24246
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Rank Two Spherical Component
8.2.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.2.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Incremental Strain Compute Finite Strain Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.4The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.5The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere_incremental-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.6The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): finiteStrain_1DSphere_hollow-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Compute Plane Small Strain
8.3.1The tensor mechanics strain calculators shall solve plane strain in the x-y plane for small strain
Specification(s): plane_strain_xy_small
Design: Compute Plane Small Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.4The tensor mechanics strain calculators shall solve plane strain in the x-z plane for small strain
Specification(s): plane_strain_xz_small
Design: Compute Plane Small Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.7The tensor mechanics strain calculators shall solve plane strain in the y-z plane for small strain
Specification(s): plane_strain_yz_small
Design: Compute Plane Small Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.1The ComputePlaneSmallStrain class shall compute the elastic stress and strain for a planar square geometry under tension using a total small plane strain formulation.
Specification(s): plane_strain
Design: Compute Plane Small Strain
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.2The ComputePlaneSmallStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a total small plane strain formulation.
Specification(s): plane_strain_Bbar
Design: Compute Plane Small Strain Volumetric Locking Correction
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.1The system shall support a traditional plane strain mechanics solution
Specification(s): plane_strain
Design: Compute Plane Small Strain
Issue(s): #5042
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.2The system shall support a traditional plane strain mechanics solution where the out-of-plane strain is prescribed
Specification(s): plane_strain_prescribed
Design: Compute Plane Small Strain
Issue(s): #5042
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.3The system shall support a generalized plane strain mechanics solution
Specification(s): generalized_plane_strain_small
Design: Compute Plane Small Strain
Issue(s): #5042
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.4The system shall support a generalized plane strain mechanics solution using the reference residual approach to check solution convergence of the field and scalar variables when the reference vector is constructed using absolute value vector tags.
Specification(s): generalized_plane_strain_ref_resid_absolute_value_vector_tags
Design: Compute Plane Small Strain
Issue(s): #5042
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.5The system shall support a generalized plane strain mechanics solution using the reference residual approach to check solution convergence of the field and scalar variables when the reference vector is constructed using unbalanced kernel contributions.
Specification(s): generalized_plane_strain_ref_resid_extra_vector_tags
Design: Compute Plane Small Strain
Issue(s): #5042
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Plane Incremental Strain
8.3.2The tensor mechanics strain calculators shall solve plane strain in the x-y plane for incremental strain
Specification(s): plane_strain_xy_incremental
Design: Compute Plane Incremental Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.5The tensor mechanics strain calculators shall solve plane strain in the x-z plane for incremental strain
Specification(s): plane_strain_xz_incremental
Design: Compute Plane Incremental Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.8The tensor mechanics strain calculators shall solve plane strain in the y-z plane for incremental strain
Specification(s): plane_strain_yz_incremental
Design: Compute Plane Incremental Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.6The system shall support a generalized plane strain mechanics solution with incremental strain
Specification(s): generalized_plane_strain_increment
Design: Compute Plane Incremental Strain
Issue(s): #5042
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Plane Finite Strain
8.3.3The tensor mechanics strain calculators shall solve plane strain in the x-y plane for finite strain
Specification(s): plane_strain_xy_finite
Design: Compute Plane Finite Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.6The tensor mechanics strain calculators shall solve plane strain in the x-z plane for finite strain
Specification(s): plane_strain_xz_finite
Design: Compute Plane Finite Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.9The tensor mechanics strain calculators shall solve plane strain in the y-z plane for finite strain
Specification(s): plane_strain_yz_finite
Design: Compute Plane Finite Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.3The ComputePlaneFiniteStrain class shall compute the elastic stress and strain for a planar square geometry under tension using a finite incremental plane strain formulation.
Specification(s): finite_planestrain
Design: Compute Plane Finite Strain
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.4The ComputePlaneFiniteStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a finite incremental plane strain formulation.
Specification(s): finite_planestrain_Bbar
Design: Compute Plane Finite Strain Volumetric Locking Correction
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.54.7The system shall support a generalized plane strain mechanics solution with finite strain
Specification(s): generalized_plane_strain_finite
Design: Compute Plane Finite Strain
Issue(s): #5042
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Generalized Plane Strain
8.3.10The tensor mechanics strain calculators shall solve generalized plane strain in the x-y plane for small strain
Specification(s): gps_xy_small
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.11The tensor mechanics strain calculators shall solve generalized plane strain in the x-y plane for incremental strain
Specification(s): gps_xy_incremental
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.12The tensor mechanics strain calculators shall solve generalized plane strain in the x-y plane for finite strain
Specification(s): gps_xy_finite
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.13The tensor mechanics strain calculators shall solve generalized plane strain in the x-z plane for small strain
Specification(s): gps_xz_small
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.14The tensor mechanics strain calculators shall solve generalized plane strain in the x-z plane for incremental strain
Specification(s): gps_xz_incremental
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.15The tensor mechanics strain calculators shall solve generalized plane strain in the x-z plane for finite strain
Specification(s): gps_xz_finite
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.16The tensor mechanics strain calculators shall solve generalized plane strain in the y-z plane for small strain
Specification(s): gps_yz_small
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.17The tensor mechanics strain calculators shall solve generalized plane strain in the y-z plane for incremental strain
Specification(s): gps_yz_incremental
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.3.18The tensor mechanics strain calculators shall solve generalized plane strain in the y-z plane for finite strain
Specification(s): gps_yz_finite
Design: Generalized Plane Strain
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Stress Divergence Tensors
8.3.19The Jacobian for plane strain in the x-y plane shall be correct
Specification(s): planestrain_jacobian_xy
Design: Stress Divergence Tensors
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.3.20The Jacobian for plane strain in the x-z plane shall be correct
Specification(s): planestrain_jacobian_xz
Design: Stress Divergence Tensors
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.3.21The Jacobian for plane strain in the y-z plane shall be correct
Specification(s): planestrain_jacobian_yz
Design: Stress Divergence Tensors
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.3.22The Jacobian for generalized plane strain in the x-y plane shall be correct
Specification(s): gps_jacobian_xy
Design: Stress Divergence Tensors
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.3.23The Jacobian for generalized plane strain in the x-z plane shall be correct
Specification(s): gps_jacobian_xz
Design: Stress Divergence Tensors
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.3.24The Jacobian for generalized plane strain in the y-z plane shall be correct
Specification(s): gps_jacobian_yz
Design: Stress Divergence Tensors
Issue(s): #11257
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Volumetric Locking Correction
8.4.2The ComputePlaneSmallStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a total small plane strain formulation.
Specification(s): plane_strain_Bbar
Design: Compute Plane Small Strain Volumetric Locking Correction
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.4The ComputePlaneFiniteStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a finite incremental plane strain formulation.
Specification(s): finite_planestrain_Bbar
Design: Compute Plane Finite Strain Volumetric Locking Correction
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.10The ComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.
Specification(s): axisym_resid_Bbar
Design: Compute Axisymmetric RZ Finite Strain Volumetric Locking Correction
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.11The volumetric locking correction option in ComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.
Specification(s): axisymmetric_vlc_centerline_pp
Design: Volumetric Locking Correction AxisymmetricCenterlineAverageValue
Issue(s): #12437 #10866
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.9.5The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.
Specification(s): axisym_resid_Bbar
Design: ADComputeAxisymmetricRZFiniteStrain Volumetric Locking Correction
Issue(s): #5142 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.9.6The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.
Specification(s): axisymmetric_vlc_centerline_pp
Design: Volumetric Locking Correction AxisymmetricCenterlineAverageValue
Issue(s): #12437 #10866
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.9.11The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction and shall produce perfect jacobians.
Specification(s): axisym_resid_Bbar-jac
Design: ADComputeAxisymmetricRZFiniteStrain Volumetric Locking Correction
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.9.12The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation and shall produce perfect jacobians.
Specification(s): axisymmetric_vlc_centerline_pp-jac
Design: Volumetric Locking Correction AxisymmetricCenterlineAverageValue
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.46.5The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.
Specification(s): elastic_patch_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.7The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.
Specification(s): elastic_patch_2Procs_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.2The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.
Specification(s): new_Bbar
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Volumetric Locking Correction
Issue(s): #8235 #4716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.3The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the QuasiStatic SolidMechanics Physics.
Specification(s): fake_plastic
Design: ComputeMultiPlasticityStress Volumetric Locking Correction
Issue(s): #9212 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.4The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the volumetric locking correction b-bar formulation.
Specification(s): fake_plastic_Bbar
Design: ComputeMultiPlasticityStress Volumetric Locking Correction
Issue(s): #9212 #8235
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.6The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the volumetric locking correction b-bar formulation.
Specification(s): rotation_new_Bbar
Design: Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #4716 #8235
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.8The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.
Specification(s): eigen_sol_Bbar
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Volumetric Locking Correction
Issue(s): #8235 #4716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.110.4The mechanics system shall correctly compute the jacobian for 3D problems using small strain and volumetric locking correction.
Specification(s): smallstrain_3D_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.5The mechanics system shall correctly compute the jacobian for 3D problems using incremental small strain and volumetric locking correction.
Specification(s): incrementalstrain_3D_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.6The mechanics system shall correctly compute the jacobian for 3D problems using finite strain and volumetric locking correction.
Specification(s): finitestrain_3D_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.10The mechanics system shall correctly compute the jacobian for RZ problems using small strain and volumetric locking correction.
Specification(s): smallstrain_RZ_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.11The mechanics system shall correctly compute the jacobian for RZ problems using incremental small strain and volumetric locking correction.
Specification(s): incrementalstrain_RZ_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.12The mechanics system shall correctly compute the jacobian for RZ problems using finite strain and volumetric locking correction.
Specification(s): finitestrain_RZ_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.16The mechanics system shall correctly compute the jacobian for planestrain problems using small strain and volumetric locking correction.
Specification(s): smallplanestrain_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.17The mechanics system shall correctly compute the jacobian for planestrain problems using incremental small strain and volumetric locking correction.
Specification(s): incrementalplanestrain_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.18The mechanics system shall correctly compute the jacobian for planestrain problems using finite strain and volumetric locking correction.
Specification(s): finiteplanestrain_Bbar
Design: Volumetric Locking Correction
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.121.2The ComputeDeformGradBasedStress class shall correctly compute the stress from lagrangian strain when volumetric locking correction is used.
Specification(s): elastic_Bbar
Design: ComputeDeformGradBasedStress Volumetric Locking Correction
Issue(s): #6604
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.121.4The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration when volumetric locking correction is used.
Specification(s): interface_Bbar
Design: ComputeVolumetricDeformGrad VolumeDeformGradCorrectedStress Volumetric Locking Correction
Issue(s): #6604
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.123.1The mechanics system shall correctly model the deformation of a 2D membrane with nearly incompressible material when volumetric locking correction is set to true.
Specification(s): vol_lock_2D
Design: Volumetric Locking Correction
Issue(s): #11220
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.123.2The mechanics system shall correctly model the locking behavior of a 2D membrane with nearly incompressible material when volumetric locking correction is set to false.
Specification(s): no_vol_lock_2D
Design: Volumetric Locking Correction
Issue(s): #11220
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Axisymmetric RZ Small Strain
8.4.5The ComputeAxisymmetricRZSmallStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small total axisymmetric strain formulation.
Specification(s): axisym_smallstrain
Design: Compute Axisymmetric RZ Small Strain
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.15We shall be able to reproduce small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation. (non-AD reference)
Specification(s): rz_small_elastic-noad
Design: Compute Axisymmetric RZ Small Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Axisymmetric RZ Incremental Strain
8.4.6The ComputeAxisymmetricRZIncrementalStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.
Specification(s): axisym_incremental_strain
Design: Compute Axisymmetric RZ Incremental Strain
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.12We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation. (non-AD reference)
Specification(s): rz_incremental_small_elastic-noad
Design: Compute Axisymmetric RZ Incremental Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Axisymmetric RZ Finite Strain
8.4.7The ComputeAxisymmetricRZFiniteStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.
Specification(s): axisym_finitestrain
Design: Compute Axisymmetric RZ Finite Strain
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.9The ComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension.
Specification(s): axisym_resid
Design: Compute Axisymmetric RZ Finite Strain
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.4.10The ComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.
Specification(s): axisym_resid_Bbar
Design: Compute Axisymmetric RZ Finite Strain Volumetric Locking Correction
Issue(s): #5142
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.9We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation. (non-AD reference)
Specification(s): rz_finite_elastic-noad
Design: Compute Axisymmetric RZ Finite Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: AxisymmetricCenterlineAverageValue
8.4.11The volumetric locking correction option in ComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.
Specification(s): axisymmetric_vlc_centerline_pp
Design: Volumetric Locking Correction AxisymmetricCenterlineAverageValue
Issue(s): #12437 #10866
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.9.6The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.
Specification(s): axisymmetric_vlc_centerline_pp
Design: Volumetric Locking Correction AxisymmetricCenterlineAverageValue
Issue(s): #12437 #10866
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.9.12The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation and shall produce perfect jacobians.
Specification(s): axisymmetric_vlc_centerline_pp-jac
Design: Volumetric Locking Correction AxisymmetricCenterlineAverageValue
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Legacy Kernel-Only Tensor Mechanics Action
8.5.1The Tensor Mechanics system shall support transformations of a rank two tensor into cylindircal coordinates.
Specification(s): test
Design: Legacy Kernel-Only Tensor Mechanics Action Cylindrical Rank Two Aux
Issue(s): #716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.5.2The Tensor Mechanics system including volumetric locking correction shall support transformations of a rank two tensor into cylindircal coordinates.
Specification(s): test_Bbar
Design: Legacy Kernel-Only Tensor Mechanics Action Cylindrical Rank Two Aux
Issue(s): #716
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Cylindrical Rank Two Aux
8.5.1The Tensor Mechanics system shall support transformations of a rank two tensor into cylindircal coordinates.
Specification(s): test
Design: Legacy Kernel-Only Tensor Mechanics Action Cylindrical Rank Two Aux
Issue(s): #716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.5.2The Tensor Mechanics system including volumetric locking correction shall support transformations of a rank two tensor into cylindircal coordinates.
Specification(s): test_Bbar
Design: Legacy Kernel-Only Tensor Mechanics Action Cylindrical Rank Two Aux
Issue(s): #716
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: AccumulateAux
8.6.1The system shall provide an aux kernel that accumulates the values of a given variable.
Specification(s): accumulate_aux
Design: AccumulateAux
Issue(s): #7091
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute R-Spherical Small Strain
8.8.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.4The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.5The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere_incremental-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.6The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): finiteStrain_1DSphere_hollow-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.12.24We shall be able to reproduce small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation. (non-AD reference)
Specification(s): rspherical_small_elastic-noad
Design: Compute R-Spherical Small Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Linear Elastic Stress
8.8.1The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.2The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
Specification(s): smallStrain_1DSphere_incremental
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.3The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.
Specification(s): finiteStrain_1DSphere_hollow
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #6256 #7555 #18876
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.8.4The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.5The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): smallStrain_1DSphere_incremental-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.8.6The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect
Specification(s): finiteStrain_1DSphere_hollow-jac
Design: Compute R-Spherical Small Strain Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System Rank Two Spherical Component
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.24.1The mechanics system shall be capable of accurately computing the elastic response of an anisotropic elastic material where 6 components of a symmetric elasticity tensor are output on an irregular patch of elements with total small strain assumptions
Specification(s): test
Design: Compute Linear Elastic Stress Compute Small Strain Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.3The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.
Specification(s): elastic_patch_total_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Small Strain Compute Linear Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.9The ComputeLinearElasticStress class shall generate an error if a user attempts to run a problem using ComputeLinearElasticStress with a finite strain formulation.
Specification(s): stress_errorcheck
Design: Compute Finite Strain Elastic Stress Compute Linear Elastic Stress Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: ADComputeAxisymmetricRZSmallStrain
8.9.1The ADComputeAxisymmetricRZSmallStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small total axisymmetric strain formulation.
Specification(s): axisym_smallstrain
Design: ADComputeAxisymmetricRZSmallStrain
Issue(s): #5142 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.9.7The ADComputeAxisymmetricRZSmallStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small total axisymmetric strain formulation and shall produce perfect jacobians.
Specification(s): axisym_smallstrain-jac
Design: ADComputeAxisymmetricRZSmallStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.12.16We shall be able to reproduce small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation.
Specification(s): rz_small_elastic
Design: ADComputeAxisymmetricRZSmallStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.17The Jacobian for the AD small strain elasticity problem in cylindrical coordinates shall be perfect
Specification(s): rz_small_elastic-jac
Design: ADComputeAxisymmetricRZSmallStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: ADComputeAxisymmetricRZIncrementalStrain
8.9.2The ADComputeAxisymmetricRZIncrementalStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.
Specification(s): axisym_incremental_strain
Design: ADComputeAxisymmetricRZIncrementalStrain
Issue(s): #5142 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.9.8The ADComputeAxisymmetricRZIncrementalStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation and shall produce perfect jacobians.
Specification(s): axisym_incremental_strain-jac
Design: ADComputeAxisymmetricRZIncrementalStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.12.13We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation.
Specification(s): rz_incremental_small_elastic
Design: ADComputeAxisymmetricRZIncrementalStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.14The Jacobian for the AD incremental small strain elasticity problem in cylindrical coordinates shall be perfect
Specification(s): rz_incremental_small_elastic-jac
Design: ADComputeAxisymmetricRZIncrementalStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: ADComputeAxisymmetricRZFiniteStrain
8.9.3The ADComputeAxisymmetricRZFiniteStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.
Specification(s): axisym_finitestrain
Design: ADComputeAxisymmetricRZFiniteStrain
Issue(s): #5142 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.9.4The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension.
Specification(s): axisym_resid
Design: ADComputeAxisymmetricRZFiniteStrain
Issue(s): #5142 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.9.5The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.
Specification(s): axisym_resid_Bbar
Design: ADComputeAxisymmetricRZFiniteStrain Volumetric Locking Correction
Issue(s): #5142 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.9.9The ADComputeAxisymmetricRZFiniteStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation and shall produce perfect jacobians.
Specification(s): axisym_finitestrain-jac
Design: ADComputeAxisymmetricRZFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.9.10The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension and shall produce perfect jacobians.
Specification(s): axisym_resid-jac
Design: ADComputeAxisymmetricRZFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.9.11The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction and shall produce perfect jacobians.
Specification(s): axisym_resid_Bbar-jac
Design: ADComputeAxisymmetricRZFiniteStrain Volumetric Locking Correction
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.12.10We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation.
Specification(s): rz_finite_elastic
Design: ADComputeAxisymmetricRZFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.11The Jacobian for the AD finite strain elasticity problem in cylindrical coordinates shall be perfect
Specification(s): rz_finite_elastic-jac
Design: ADComputeAxisymmetricRZFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Hill Creep Stress Update
8.11.1The system shall avoid regression on material time step and combined anisotropic creep computations
Specification(s): anis_mech_hill_tensor_creep_small_tiny_step_ts_limit_test
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.11.2The system shall be capable of reproducing verification results of creep strain ratios along the X direction.
Specification(s): ad_aniso_creep_x_3d
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.3The system shall be capable of reproducing verification results of creep strain ratios along the X direction using hand-coded Jacobians.
Specification(s): aniso_creep_x_3d
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.4The system shall reproduce the creep strain as those evaluated with residual and derivative computations used for isotropic elasticity.
Specification(s): ad_aniso_creep_x_3d_aniso_elasticity
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.5The system shall compute shear creep strain in an element subject to shear load in one direction.
Specification(s): ad_aniso_creep_x_3d_shear
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.6The system shall compute shear creep strain in an element subject to shear load in two directions.
Specification(s): ad_aniso_creep_xy_3d_shear
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.7The system shall compute creep strains in an element with anisotropic elasticity and subject to biaxial tensile load.
Specification(s): ad_aniso_creep_xy_3d_aniso_elasticity
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.8The system shall be capable of reproducing verification results of creep strain ratios along the X direction using hand-coded Jacobians when no transformation is used to rotate the Hill tensor for small deformation.
Specification(s): aniso_creep_x_3d_no_trafo
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.9The system shall be capable of reproducing verification results of creep strain ratios along the Y direction.
Specification(s): ad_aniso_creep_y_3d
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.10The system shall be capable of reproducing verification results of creep strain ratios along the Z direction.
Specification(s): ad_aniso_creep_z_3d
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.11The system shall be capable of reproducing isotropic creep with the right anisotropic creep parameters: Baseline
Specification(s): ad_aniso_iso_iso
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.12The system shall provide a perfect Jacobian while calculating large deformation creep.
Specification(s): jac_ad
Design: Hill Creep Stress Update
Issue(s): #17456
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.11.13The system shall provide a reasonable Jacobian while calculating large deformation creep using the elasticity tensor as the tangent operator.
Specification(s): jac
Design: Hill Creep Stress Update
Issue(s): #21824
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.11.14The system shall be capable of reproducing isotropic creep with the right anisotropic creep parameters.
Specification(s): ad_aniso_iso_aniso
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.15The system shall be capable of enforcing a time step such that the creep rate integration error is controled by the user with the aid of a soft terminator when regular (non-AD) objects are used.
Specification(s): aniso_creep_integration_error
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.16The system shall be capable of enforcing a time step such that the creep rate integration error is controled by the user with the aid of a soft terminator.
Specification(s): ad_aniso_creep_integration_error
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.17The system shall be capable of running Hill materials with constant coefficients and coefficients that are function of temperature to capture material texture. This test performs a reference run with constant coefficients
Specification(s): ad_aniso_creep_temperature_coefficients
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.11.18The system shall be capable of running Hill materials with constant coefficients and coefficients that are function of temperature to capture material texture. This test performs a run using a constant temperature function.
Specification(s): ad_aniso_creep_temperature_coefficients_function
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.11.19The system shall be capable of running anisotropic Hill creep with temperature-dependent Hill coefficients and generating correct output.
Specification(s): ad_aniso_creep_temperature_coefficients_function_variation
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.11.20The system shall be capable of using large deformation rotation to update the orientation of Hill parameters even when there is no rigid body rotation. This test also serves as a reference to verify the updates to the Hill parameters when there is significant rigid body motion
Specification(s): 3d_bar_orthotropic_90deg_rotation_ad_creep_z_no_rotation
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.21The system shall be capable of using large deformation rotation to update the orientation of Hill parameters when there is 90-degree rigid body orientation change about the Z axis. The creep strains have to be very similar to the output when there is no rigid body motion (Note: The mere constraints enforcing rigid body rotation induce numerical errors). In this case using Hill constants.
Specification(s): 3d_bar_orthotropic_90deg_rotation_ad_creep_z
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.22The system shall be capable of using large deformation rotation to update the orientation of Hill parameters even when there is no rigid body rotation. This test also serves as a reference to verify the updates to the Hill parameters when there is significant rigid body motion
Specification(s): 3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.23The system shall be capable of not using large deformation rotation to define Hill anisotropic parameters.
Specification(s): 3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation_no_transformation
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.11.24The system shall be capable of using large deformation rotation to update the orientation of Hill parameters when there is 90-degree rigid body orientation change about the X axis. The creep strains have to be very similar to the output when there is no rigid body motion (Note: The mere constraints enforcing rigid body rotation induce numerical errors). In this case using Hill constants.
Specification(s): 3d_bar_orthotropic_90deg_rotation_ad_creep_x
Design: Hill Creep Stress Update
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Finite Strain in Cartesian System
8.12.1We shall be able to reproduce finite strain elasticity results of the hand-coded simulation using automatic differentiation. (non-AD reference)
Specification(s): finite_elastic-noad
Design: Compute Finite Strain in Cartesian System
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.1The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.
Specification(s): new
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.2The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.
Specification(s): new_Bbar
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Volumetric Locking Correction
Issue(s): #8235 #4716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.7The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.
Specification(s): eigen_sol
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.8The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.
Specification(s): eigen_sol_Bbar
Design: Compute Finite Strain Elastic Stress Compute Finite Strain in Cartesian System Volumetric Locking Correction
Issue(s): #8235 #4716
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.51.1Finite strain methods in Tensor Mechanics should be able to adequately simulate a bar bending simulation in 2D
Specification(s): bending
Design: Compute Finite Strain in Cartesian System
Issue(s): #7228
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.51.2Finite strain methods in Tensor Mechanics should be able to adequately simulate a bar bending simulation in 2D using a volumetric locking correction
Specification(s): bending_Bbar
Design: Compute Finite Strain in Cartesian System
Issue(s): #7228
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.51.3Finite strain methods in Tensor Mechanics should be able to adequately simulate a tensile test simulation in 3D
Specification(s): 3d_bar
Design: Compute Finite Strain in Cartesian System
Issue(s): #7228
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.51.4Finite strain methods in Tensor Mechanics should be able to adequately simulate a tensile test simulation in 3D using a volumetric locking correction
Specification(s): 3d_bar_Bbar
Design: Compute Finite Strain in Cartesian System
Issue(s): #7228
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.124.3The system shall cut the timestep through a mooseException when the loading conditions deform the element enough to produce a negative number under a square root term in the Rashid approximation for the rotation tensor
Specification(s): except3
Design: Compute Finite Strain in Cartesian System
Issue(s): #19067
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: ADComputeFiniteStrain
8.12.2We shall be able to reproduce finite strain elasticity results of the hand-coded simulation using automatic differentiation.
Specification(s): finite_elastic
Design: ADComputeFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.3The Jacobian for the AD finite strain elasticity problem shall be perfect
Specification(s): finite_elastic-jac
Design: ADComputeFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.13.1Finite strain methods in Tensor Mechanics should be able to adequately simulate a bar bending simulation in 2D using AD and match non-AD methods
Specification(s): bending
Design: ADComputeFiniteStrain
Issue(s): #7228 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.13.2Finite strain methods in Tensor Mechanics should be able to adequately simulate a bar bending simulation in 2D using a volumetric locking correction using AD and match non-AD methods
Specification(s): bending_Bbar
Design: ADComputeFiniteStrain
Issue(s): #7228 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.13.3Finite strain methods in Tensor Mechanics should be able to adequately simulate a tensile test simulation in 3D using AD and match non-AD methods
Specification(s): 3d_bar
Design: ADComputeFiniteStrain
Issue(s): #7228 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.13.4Finite strain methods in Tensor Mechanics should be able to adequately simulate a tensile test simulation in 3D using a volumetric locking correction using AD and match non-AD methods
Specification(s): 3d_bar_Bbar
Design: ADComputeFiniteStrain
Issue(s): #7228 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.13.5Finite strain methods in Tensor Mechanics should be able to adequately simulate a bar bending simulation in 2D using AD and calculate perfect Jacobians
Specification(s): bending-jac
Design: ADComputeFiniteStrain
Issue(s): #12650 #13260
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.13.6Finite strain methods in Tensor Mechanics should be able to adequately simulate a bar bending simulation in 2D using a volumetric locking correction using AD and calculate perfect Jacobians
Specification(s): bending_Bbar-jac
Design: ADComputeFiniteStrain
Issue(s): #12650 #13260
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.13.7Finite strain methods in Tensor Mechanics should be able to adequately simulate a tensile test simulation in 3D using AD and calculate perfect Jacobians
Specification(s): 3d_bar-jac
Design: ADComputeFiniteStrain
Issue(s): #12650 #13260
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.13.8Finite strain methods in Tensor Mechanics should be able to adequately simulate a tensile test simulation in 3D using a volumetric locking correction using AD and calculate perfect Jacobians
Specification(s): 3d_bar_Bbar-jac
Design: ADComputeFiniteStrain
Issue(s): #12650 #13260
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.13.9Finite strain methods in Tensor Mechanics, using the auto differentiation capabilities, shall cut the timestep through a mooseException when the loading conditions deform the elements so much as to produce a negative number under the square root term in the Rashid approximation for the rotation tensor calcuation
Specification(s): bending_exception
Design: ADComputeFiniteStrain
Issue(s): #19067
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Compute Incremental Strain
8.12.4We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation using automatic differentiation. (non-AD reference)
Specification(s): incremental_small_elastic-noad
Design: Compute Incremental Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.2The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.
Specification(s): elastic_patch_incremental_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.4The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.
Specification(s): elastic_patch_incremental_small_no_disp_mesh
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584 #12580
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ADComputeIncrementalStrain
8.12.5We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation using automatic differentiation.
Specification(s): incremental_small_elastic
Design: ADComputeIncrementalStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.6The Jacobian for the AD incremental small strain elasticity problem shall be perfect
Specification(s): incremental_small_elastic-jac
Design: ADComputeIncrementalStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: ADComputeGreenLagrangeStrain
8.12.7The system shall provide an AD enabled Green-Lagrange strain calculator
Specification(s): green-lagrange
Design: ADComputeGreenLagrangeStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.8The Jacobian for the Green-Lagrange strain calculator shall be perfect
Specification(s): green-lagrange-jac
Design: ADComputeGreenLagrangeStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Compute R-Spherical Finite Strain
8.12.18We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation. (non-AD reference)
Specification(s): rspherical_finite_elastic-noad
Design: Compute R-Spherical Finite Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ADComputeRSphericalFiniteStrain
8.12.19We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation.
Specification(s): rspherical_finite_elastic
Design: ADComputeRSphericalFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.20The Jacobian for the AD finite strain elasticity problem in spherical coordinates shall be perfect
Specification(s): rspherical_finite_elastic-jac
Design: ADComputeRSphericalFiniteStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: ADComputeRSphericalIncrementalStrain
8.12.22We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation.
Specification(s): rspherical_incremental_small_elastic
Design: ADComputeRSphericalIncrementalStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.23The Jacobian for the AD incremental small strain elasticity in spherical coordinates problem shall be perfect
Specification(s): rspherical_incremental_small_elastic-jac
Design: ADComputeRSphericalIncrementalStrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Compute R-Spherical Small Strain
8.12.25We shall be able to reproduce small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation.
Specification(s): rspherical_small_elastic
Design: Compute R-Spherical Small Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.12.26The Jacobian for the AD small strain elasticity problem in spherical coordinates shall be perfect
Specification(s): rspherical_small_elastic-jac
Design: Compute R-Spherical Small Strain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Compute Isotropic Elasticity Tensor
8.14.1The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the lambda and shear modulus for an isotropic material using AD formulations.
Specification(s): lambda_shear
Design: Compute Isotropic Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.14.2The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the Young's modulus and Poisson's ratio for an isotropic material using AD formulations.
Specification(s): youngs_poissons
Design: Compute Isotropic Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.14.3The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from their bulk modulus and shear modulus for an isotropic material using AD formulations.
Specification(s): bulk_shear
Design: Compute Isotropic Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.14.4The ComputeElasticityTensor class shall correctly compute the elasticity tensor for an isotropic axisymmetric problem.
Specification(s): axisymmetric_rz
Design: Compute Isotropic Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.14.5The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the lambda and shear modulus for an isotropic material using AD formulations and produce a perfect Jacobian.
Specification(s): lambda_shear-jac
Design: Compute Isotropic Elasticity Tensor
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.14.6The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the Young's modulus and Poisson's ratio for an isotropic material using AD formulations and produce a perfect Jacobian.
Specification(s): youngs_poissons-jac
Design: Compute Isotropic Elasticity Tensor
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.14.7The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from their bulk modulus and shear modulus for an isotropic material using AD formulations and produce a perfect Jacobian.
Specification(s): bulk_shear-jac
Design: Compute Isotropic Elasticity Tensor
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.14.8The ComputeElasticityTensor class shall correctly compute the elasticity tensor for an isotropic axisymmetric problem and produce a perfect Jacobian.
Specification(s): axisymmetric_rz-jac
Design: Compute Isotropic Elasticity Tensor
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.32.1The system shall generate an error if a number of elastic constants other than two is supplied for an isotropic elasticity tensor
Specification(s): num_constants
Design: Compute Isotropic Elasticity Tensor
Issue(s): #9438
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.32.2The system shall generate an error if a non-positive Youngs modulus is supplied for an isotropic elasticity tensor
Specification(s): youngs_modulus
Design: Compute Isotropic Elasticity Tensor
Issue(s): #9438
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.32.3The system shall generate an error if a non-positive bulk modulus is supplied for an isotropic elasticity tensor
Specification(s): bulk_modulus
Design: Compute Isotropic Elasticity Tensor
Issue(s): #9438
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.32.4The system shall generate an error if a Poissons ratio outside the range from -1 to 0.5 is supplied for an isotropic elasticity tensor
Specification(s): poissons_ratio
Design: Compute Isotropic Elasticity Tensor
Issue(s): #9438
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.32.5The system shall generate an error if a non-positive shear modulus is supplied for an isotropic elasticity tensor
Specification(s): shear_modulus
Design: Compute Isotropic Elasticity Tensor
Issue(s): #9438
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.46.1The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes.
Specification(s): elastic_patch
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.2The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.
Specification(s): elastic_patch_incremental_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.3The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.
Specification(s): elastic_patch_total_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Small Strain Compute Linear Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.4The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.
Specification(s): elastic_patch_incremental_small_no_disp_mesh
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584 #12580
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.5The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.
Specification(s): elastic_patch_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.6The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when running on 2 processors in parallel.
Specification(s): elastic_patch_2Procs
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.7The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.
Specification(s): elastic_patch_2Procs_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.8The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular 20-noded quadratic hexes.
Specification(s): elastic_patch_quadratic
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #620
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.67.1The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the lambda and shear modulus for an isotropic material.
Specification(s): lambda_shear
Design: Compute Isotropic Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.67.2The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the Young's modulus and Poisson's ratio for an isotropic material.
Specification(s): youngs_poissons
Design: Compute Isotropic Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.67.3The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from their bulk modulus and shear modulus for an isotropic material.
Specification(s): bulk_shear
Design: Compute Isotropic Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ADComputeLinearElasticStress
8.15.1We shall be able to reproduce linear elastic stress results of the hand-coded simulation using automatic differentiation.
Specification(s): linear_elastic_material
Design: ADComputeLinearElasticStress
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.15.2The Jacobian for the AD linear elastic stress problem shall be perfect
Specification(s): linear_elastic_material-jac
Design: ADComputeLinearElasticStress
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.15.3We shall be able to introduce extra stresses into the stress calculators using automatic differentiation.
Specification(s): extra_stresses
Design: ADComputeLinearElasticStress
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.15.4The Jacobian for the AD linear elastic stress problem shall be perfect
Specification(s): extra_stresses-jac
Design: ADComputeLinearElasticStress
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.15.7We shall be able to reproduce small strain with specified tensors results of the hand-coded simulation using automatic differentiation.
Specification(s): tensor
Design: ADComputeLinearElasticStress
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.15.8The Jacobian for the AD small strain with specified tensors problem shall be perfect
Specification(s): tensor-jac
Design: ADComputeLinearElasticStress
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Compute Eigenstrain
8.15.5We shall be able to reproduce eigenstrain results of the hand-coded simulation using automatic differentiation.
Specification(s): applied_strain
Design: Compute Eigenstrain
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.15.6The Jacobian for the AD eigenstrain problem shall be perfect
Specification(s): applied_strain-jac
Design: Compute Eigenstrain
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.15.9We shall be able to reproduce thermal eigenstrain results of the hand-coded simulation using automatic differentiation.
Specification(s): thermal_expansion
Design: Compute Eigenstrain
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.15.10The Jacobian for the AD thermal eigenstrain problem shall be perfect
Specification(s): thermal_expansion-jac
Design: Compute Eigenstrain
Issue(s): #13099
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Power Law Creep Stress Update
8.16.1The AD multiple inelastic stress calculator shall provide a correct stress for a single power law creep model (reference computation)
Specification(s): powerlaw_ten
Design: Power Law Creep Stress Update
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.1The PowerLawCreepStressUpdate, called through the ADComputeMultipleInelasticStress, shall compute a creep strain based on an extrenal loading.
Specification(s): creep
Design: Power Law Creep Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.2The Jacobian for the AD regular creep problem shall be perfect
Specification(s): creep-jac
Design: Power Law Creep Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.92.2
The system shall gracefully correct for out of bounds guess from the radial return mapping algorithm
1. from the high bound.
2. from the low bound.
Specification(s): bounds/high, bounds/low
Design: Power Law Creep Stress Update
Issue(s): #9659 #20290
Collection(s): FUNCTIONAL
Type(s): RunApp
8.92.3
The system shall provide a power law creep mechanical constitutive model not using AD
1. that works with a finite strain formulation.
2. that works with a coupled plasticty model.
3. that shall be restartable.
4. that shall be restartable with a response that matches the original run.
5. that works with a small strain formulation.
Specification(s): nonad/power_law_creep, nonad/cp_power_law_creep, nonad/restart1, nonad/power_law_creep_restart2, nonad/smallstrain
Design: Power Law Creep Stress Update
Issue(s): #8642
Collection(s): FUNCTIONAL
Type(s): ExodiffRunApp
8.92.4
The system shall provide a power law creep mechanical constitutive model using AD
1. that works with a finite strain formulation.
2. that shall be restartable.
3. that shall be restartable with a response that matches the original run.
4. that works with a small strain formulation.
5. calculate a perfect Jacobian
6. calculate a perfect Jacobian with the small strain formulation
Specification(s): ad/power_law_creep, ad/restart1, ad/power_law_creep_restart2, ad/smallstrain, ad/power_law_creep-jac, ad/small_strain-jac
Design: Power Law Creep Stress Update
Issue(s): #8642
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTesterExodiffRunApp

solid_mechanics: ADComputeMultipleInelasticStress
8.16.2The AD multiple inelastic stress calculator shall provide a correct stress for a single power law creep model and an additional zero creep power law model
Specification(s): powerlaw_zero
Design: ADComputeMultipleInelasticStress
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.16.3The AD multiple inelastic stress calculator shall provide a correct stress for the linear combination of two power law creep models
Specification(s): powerlaw_sum
Design: ADComputeMultipleInelasticStress
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.16.4The AD multiple inelastic stress calculator shall provide a correct stress when cycling through two identical power law creep models
Specification(s): powerlaw_cycle
Design: ADComputeMultipleInelasticStress
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.16.5The AD multiple inelastic stress calculator shall provide a correct jacobian for a single power law creep model
Specification(s): powerlaw_ten_jacobian
Design: ADComputeMultipleInelasticStress
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.16.6The AD multiple inelastic stress calculator shall provide a correct jacobian for a single power law creep model and an additional zero creep power law model
Specification(s): powerlaw_zero_jacobian
Design: ADComputeMultipleInelasticStress
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.16.7The AD multiple inelastic stress calculator shall provide a correct jacobian for the linear combination of two power law creep models
Specification(s): powerlaw_sum_jacobian
Design: ADComputeMultipleInelasticStress
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.16.8The AD multiple inelastic stress calculator shall provide a correct jacobian when cycling through two identical power law creep models
Specification(s): powerlaw_cycle_jacobian
Design: ADComputeMultipleInelasticStress
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.1The PowerLawCreepStressUpdate, called through the ADComputeMultipleInelasticStress, shall compute a creep strain based on an extrenal loading.
Specification(s): creep
Design: Power Law Creep Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.2The Jacobian for the AD regular creep problem shall be perfect
Specification(s): creep-jac
Design: Power Law Creep Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.3The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.
Specification(s): exact_spherical
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.4The Jacobian for the AD exact spherical problem shall be perfect
Specification(s): exact_spherical-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.5The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.
Specification(s): exact_cylindrical
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.6The Jacobian for the AD exact cylindrical problem shall be perfect
Specification(s): exact_cylindrical-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.7The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with LPS spherical formulation that increases the porosity due to an external strain.
Specification(s): lps_single
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.8The Jacobian for the AD lps single problem shall be perfect
Specification(s): lps_single-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.9The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and the same stress exponential that is close to combining the models into a single ADViscoplasticityStressUpdate instance.
Specification(s): lps_single_split
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.10The Jacobian for the AD lps single split problem shall be perfect
Specification(s): lps_single_split-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.11The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and two different stress exponents that increases the porosity due to an external strain.
Specification(s): lps_dual
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.12The Jacobian for the AD lps dual problem shall be perfect
Specification(s): lps_dual-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.13The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with GTN formulation that increases the porosity due to an external strain.
Specification(s): gtn_single
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.14The Jacobian for the AD gtn single problem shall be perfect
Specification(s): gtn_single-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.15
The system shall handle a negative calculated porosity computed from a strain tensor
1. by setting the porosity to zero.
2. by setting the porosity to the initial condition.
3. by throwing an exception.
Specification(s): negative/zero, negative/initial, negative/exception
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunExceptionCSVDiff

solid_mechanics: Pressure Action System
8.17.1The Pressure boundary condition action shall create the objects needed to apply automatic differentiation pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure and match non-AD methods.
Specification(s): 3D
Design: Pressure Action System
Issue(s): #4781 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.17.2The Pressure boundary condition action shall create the objects needed to apply automatic differentiation pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure using the volumetric locking correction b-bar formulation and match non-AD methods.
Specification(s): 3D_Bbar
Design: Pressure Action System
Issue(s): #4781 #8235 #13260
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.17.3The Pressure boundary condition action shall create the objects needed to apply automatic differentiation pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure and calculate a perfect Jacobian.
Specification(s): 3D-jac
Design: Pressure Action System
Issue(s): #4781 #13260
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.17.4The Pressure boundary condition action shall create the objects needed to apply automatic differentiation pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure using the volumetric locking correction b-bar formulation and calculate a perfect Jacobian.
Specification(s): 3D_Bbar-jac
Design: Pressure Action System
Issue(s): #4781 #8235 #13260
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.94.1The Pressure boundary condition action shall create the objects needed to apply pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure.
Specification(s): 3D
Design: Pressure Action System
Issue(s): #4781
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.94.2The Pressure boundary condition action shall create the objects needed to apply pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure using the volumetric locking correction b-bar formulation.
Specification(s): 3D_Bbar
Design: Pressure Action System
Issue(s): #4781 #8235
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Radial Return Stress Update
8.18.1The return mapping algorithm shall use automatic differentiation to compute the derivative of the yield function with respect to the internal variable, and the solution should be the same as existing hand coded derivative.
Specification(s): reference
Design: Radial Return Stress Update
Issue(s): #20407
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.14The system shall return an error if the user requests substepping for a radial return inelastic model that does not implement it yet.
Specification(s): isotropic_plasticity_substepping_error
Design: Radial Return Stress Update
Issue(s): #14757
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Compute Small Strain
8.19.1We shall be able to run a simple linear small-strain problem using a hand-coded Jacobian
Specification(s): linear-hand-coded
Design: Compute Small Strain
Issue(s): #5658 #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.19.4The Jacobian for the hand-coded problem shall be perfect
Specification(s): linear-hand-coded-jac
Design: Compute Small Strain
Issue(s): #5658 #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.24.1The mechanics system shall be capable of accurately computing the elastic response of an anisotropic elastic material where 6 components of a symmetric elasticity tensor are output on an irregular patch of elements with total small strain assumptions
Specification(s): test
Design: Compute Linear Elastic Stress Compute Small Strain Solid Mechanics QuasiStatic Physics System
Issue(s): #4716 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.3The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.
Specification(s): elastic_patch_total_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Small Strain Compute Linear Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ADComputeSmallStrain
8.19.2We shall be able to reproduce the results of the hand-coded simulation using automatic differentiation in the production stress divergence kernel
Specification(s): linear-ad
Design: ADComputeSmallStrain
Issue(s): #5658 #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.19.3We shall be able to reproduce the results of the hand-coded simulation using automatic differentiation with reversed stress and strain materials
Specification(s): linear-ad-reverse
Design: ADComputeSmallStrain
Issue(s): #5658 #12650
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.19.5The Jacobian for the automatic differentiation problem shall be perfect
Specification(s): linear-ad-jac
Design: ADComputeSmallStrain
Issue(s): #5658 #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.19.6The Jacobian for the automatic differentiation problem with reversed stress and strain materials shall be perfect
Specification(s): linear-ad-jac-reverse
Design: ADComputeSmallStrain
Issue(s): #5658 #12650
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: AD Compute Smeared Cracking Stress
8.20.1The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in cartesian coordinates using AD and match non-AD methods.
Specification(s): cracking
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.2The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in rz coordinates using AD and match non-AD methods.
Specification(s): cracking_rz
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.3The MOOSE SolidMechanics module shall simulate cracking while the cracking strength is prescribed by an elemental AuxVariable using AD and match non-AD methods.
Specification(s): cracking_function
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.4The MOOSE SolidMechanics module shall simulate exponential stress release using AD and match non-AD methods.
Specification(s): exponential
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.5The MOOSE SolidMechanics module shall simulate exponential stress relase while using the rz coordinate system using AD and match non-AD methods.
Specification(s): rz_exponential
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.6The MOOSE SolidMechanics module shall demonstrate softening using the power law for smeared cracking using AD and match non-AD methods.
Specification(s): power
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.7The MOOSE SolidMechanics module shall demonstrate the prescribed softening laws in three directions, power law (x), exponential (y), and abrupt (z) using AD and match non-AD methods.
Specification(s): multiple_softening
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.8The MOOSE SolidMechanics module shall simulate smeared cracking in the x y and z directions using AD and match non-AD methods.
Specification(s): xyz
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.9The MOOSE SolidMechanics module shall simulate smeared cracking under plane stress conditions using AD and match non-AD methods.
Specification(s): plane_stress
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.10The MOOSE SolidMechanics module shall demonstrate that the smeared cracking model correctly handles finite rotation of cracked elements using AD and match non-AD methods.
Specification(s): cracking_rotation
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.11The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in x using AD and match non-AD methods.
Specification(s): cracking_rotation_pres_dir_x
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.12The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in z using AD and match non-AD methods.
Specification(s): cracking_rotation_pres_dir_z
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.13The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where two cracks are prescribed in x and z using AD and match non-AD methods.
Specification(s): cracking_rotation_pres_dir_xz
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.20.14The MOOSE SolidMechanics module shall compute accurate AD Jacobian of system with multiple softening laws.
Specification(s): ad_multiple_softening_jacobian
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.20.15The ComputeSmearedCrackingStress model shall generate a warning if 'cracked_elasticity_type' is not specified
Specification(s): cracking_err_diagonal
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.20.16The ComputeSmearedCrackingStress model shall generate an error if an invalid number of softening models is specified
Specification(s): cracking_err_softening
Design: AD Compute Smeared Cracking Stress
Issue(s): #6815 #9227 #15311
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: ComputeMeanThermalExpansionFunctionEigenstrain
8.21.1
The system shall compute an eigenstrain due to thermal expansion using a function that describes a constant mean and instantaneous thermal expansion using the AD formulation
1. and the finite strain formulation
2. and the small strain formulation
Specification(s): constant/finite, constant/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.21.2
The system shall compute an eigenstrain due to thermal expansion using a function that describes a mean and instantaneous thermal expansion with a linear relationship to temperature using the AD formulation
1. and the finite strain formulation
2. and the small strain formulation
Specification(s): linear/finite, linear/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.21.3
The system shall compute an eigenstrain due and allow a smooth transition from negative to positive strain across the reference temperature and compare favorably to hand calculations
1. using a mean thermal expansion coefficient
2. using a complex mean thermal expansion coefficient
3. using a complex mean thermal expansion coefficient and compute a perfect jacobian
4. using a instantaneous thermal expansion coefficient
5. using a complex instantaneous thermal expansion coefficient
6. using a complex instantaneous thermal expansion coefficient and compute a perfect jacobian
7. using a dilatation thermal expansion coefficient
Specification(s): individual/mean, individual/mean_complex, individual/mean_complex_jac, individual/instantaneous, individual/instantaneous_complex, individual/instantaneous_complex_jac, individual/dilatation
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain ComputeDilatationThermalExpansionFunctionEigenstrain
Issue(s): #13634 #14595
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTesterCSVDiff
8.112.1
The system shall compute an eigenstrain due to thermal expansion using a function that describes a constant mean and instantaneous thermal expansion
1. using finite strain formulation
2. using small strain formulation
Specification(s): constant/finite, constant/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #13634
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.112.2
The system shall compute an eigenstrain due to thermal expansion using a function that describes a mean and instantaneous thermal expansion with a linear relationship to temperature
1. using finite strain formulation
2. using small strain formulation
Specification(s): linear/finite, linear/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #13634
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.112.3
The system shall compute an eigenstrain due and allow a smooth transition from negative to positive strain across the reference temperature and compare favorably to hand calculations
1. using a mean thermal expansion coefficient
2. using a mean thermal expansion coefficient with a scaling factor for sensitivity studies
3. using a instantaneous thermal expansion coefficient
4. using a dilatation thermal expansion coefficient
Specification(s): individual/mean, individual/mean_scaling, individual/instantaneous, individual/dilatation
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain ComputeDilatationThermalExpansionFunctionEigenstrain
Issue(s): #13634 #14595 #21412
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeInstantaneousThermalExpansionFunctionEigenstrain
8.21.1
The system shall compute an eigenstrain due to thermal expansion using a function that describes a constant mean and instantaneous thermal expansion using the AD formulation
1. and the finite strain formulation
2. and the small strain formulation
Specification(s): constant/finite, constant/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.21.2
The system shall compute an eigenstrain due to thermal expansion using a function that describes a mean and instantaneous thermal expansion with a linear relationship to temperature using the AD formulation
1. and the finite strain formulation
2. and the small strain formulation
Specification(s): linear/finite, linear/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #12650
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.21.3
The system shall compute an eigenstrain due and allow a smooth transition from negative to positive strain across the reference temperature and compare favorably to hand calculations
1. using a mean thermal expansion coefficient
2. using a complex mean thermal expansion coefficient
3. using a complex mean thermal expansion coefficient and compute a perfect jacobian
4. using a instantaneous thermal expansion coefficient
5. using a complex instantaneous thermal expansion coefficient
6. using a complex instantaneous thermal expansion coefficient and compute a perfect jacobian
7. using a dilatation thermal expansion coefficient
Specification(s): individual/mean, individual/mean_complex, individual/mean_complex_jac, individual/instantaneous, individual/instantaneous_complex, individual/instantaneous_complex_jac, individual/dilatation
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain ComputeDilatationThermalExpansionFunctionEigenstrain
Issue(s): #13634 #14595
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTesterCSVDiff
8.112.1
The system shall compute an eigenstrain due to thermal expansion using a function that describes a constant mean and instantaneous thermal expansion
1. using finite strain formulation
2. using small strain formulation
Specification(s): constant/finite, constant/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #13634
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.112.2
The system shall compute an eigenstrain due to thermal expansion using a function that describes a mean and instantaneous thermal expansion with a linear relationship to temperature
1. using finite strain formulation
2. using small strain formulation
Specification(s): linear/finite, linear/small_const
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain
Issue(s): #13634
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.112.3
The system shall compute an eigenstrain due and allow a smooth transition from negative to positive strain across the reference temperature and compare favorably to hand calculations
1. using a mean thermal expansion coefficient
2. using a mean thermal expansion coefficient with a scaling factor for sensitivity studies
3. using a instantaneous thermal expansion coefficient
4. using a dilatation thermal expansion coefficient
Specification(s): individual/mean, individual/mean_scaling, individual/instantaneous, individual/dilatation
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain ComputeDilatationThermalExpansionFunctionEigenstrain
Issue(s): #13634 #14595 #21412
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeDilatationThermalExpansionFunctionEigenstrain
8.21.3
The system shall compute an eigenstrain due and allow a smooth transition from negative to positive strain across the reference temperature and compare favorably to hand calculations
1. using a mean thermal expansion coefficient
2. using a complex mean thermal expansion coefficient
3. using a complex mean thermal expansion coefficient and compute a perfect jacobian
4. using a instantaneous thermal expansion coefficient
5. using a complex instantaneous thermal expansion coefficient
6. using a complex instantaneous thermal expansion coefficient and compute a perfect jacobian
7. using a dilatation thermal expansion coefficient
Specification(s): individual/mean, individual/mean_complex, individual/mean_complex_jac, individual/instantaneous, individual/instantaneous_complex, individual/instantaneous_complex_jac, individual/dilatation
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain ComputeDilatationThermalExpansionFunctionEigenstrain
Issue(s): #13634 #14595
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTesterCSVDiff
8.112.3
The system shall compute an eigenstrain due and allow a smooth transition from negative to positive strain across the reference temperature and compare favorably to hand calculations
1. using a mean thermal expansion coefficient
2. using a mean thermal expansion coefficient with a scaling factor for sensitivity studies
3. using a instantaneous thermal expansion coefficient
4. using a dilatation thermal expansion coefficient
Specification(s): individual/mean, individual/mean_scaling, individual/instantaneous, individual/dilatation
Design: ComputeMeanThermalExpansionFunctionEigenstrain ComputeInstantaneousThermalExpansionFunctionEigenstrain ComputeDilatationThermalExpansionFunctionEigenstrain
Issue(s): #13634 #14595 #21412
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: AD Viscoplasticity Stress Update
8.22.3The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.
Specification(s): exact_spherical
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.4The Jacobian for the AD exact spherical problem shall be perfect
Specification(s): exact_spherical-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.5The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.
Specification(s): exact_cylindrical
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.6The Jacobian for the AD exact cylindrical problem shall be perfect
Specification(s): exact_cylindrical-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.7The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with LPS spherical formulation that increases the porosity due to an external strain.
Specification(s): lps_single
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.8The Jacobian for the AD lps single problem shall be perfect
Specification(s): lps_single-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.9The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and the same stress exponential that is close to combining the models into a single ADViscoplasticityStressUpdate instance.
Specification(s): lps_single_split
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.10The Jacobian for the AD lps single split problem shall be perfect
Specification(s): lps_single_split-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.11The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and two different stress exponents that increases the porosity due to an external strain.
Specification(s): lps_dual
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.12The Jacobian for the AD lps dual problem shall be perfect
Specification(s): lps_dual-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.13The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with GTN formulation that increases the porosity due to an external strain.
Specification(s): gtn_single
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.22.14The Jacobian for the AD gtn single problem shall be perfect
Specification(s): gtn_single-jac
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.22.15
The system shall handle a negative calculated porosity computed from a strain tensor
1. by setting the porosity to zero.
2. by setting the porosity to the initial condition.
3. by throwing an exception.
Specification(s): negative/zero, negative/initial, negative/exception
Design: AD Viscoplasticity Stress Update ADComputeMultipleInelasticStress
Issue(s): #13494
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunExceptionCSVDiff

solid_mechanics: SolidMechanicsPlasticOrthotropic
8.23.1Anisotropic plasticity and anisotropic elastoplasticity must give almost identical results if elastic behavior is isotropic – plastic anisotropy
Specification(s): ad_aniso_plasticity_x_one_ref
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.2Anisotropic plasticity and anisotropic elastoplasticity must give almost identical results if elastic behavior is isotropic – elastoplastic anisotropy
Specification(s): ad_aniso_plasticity_x_one
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.3The system shall be able to solve anisotropic plasticity and anisotropic elastoplasticity problems with elastoplastic anisotropy
Specification(s): ad_aniso_plasticity_x_one_light
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): RunApp
8.23.4Uniaxial tensile test run in x direction with anisotropic elasticity and linear strain hardening with automatic differentiation
Specification(s): ad_uniaxial_x_linear
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.5Uniaxial tensile test run in y direction with anisotropic elasticity and linear strain hardening with automatic differentiation
Specification(s): ad_uniaxial_y_linear
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.6Uniaxial tensile test run in x direction with anisotropic elasticity and non-linear strain hardening with automatic differentiation
Specification(s): ad_uniaxial_x_non_linear
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.7Compute hoop plastic strain in a cylinder and compare it for two elements located separately in hoop direction
Specification(s): 3D_hoop_strain_comparison
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.8Compute hoop plastic strain in a cylinder oriented along the x axis and compare it for two elements located separately in hoop direction for coarsely meshed model
Specification(s): 3D_hoop_strain_comparison_coarse_xaxis
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.9Compute hoop plastic strain in a cylinder oriented along the y axis and compare it for two elements located separately in hoop direction for coarsely meshed model
Specification(s): 3D_hoop_strain_comparison_coarse_yaxis
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.23.10Compute hoop plastic strain in a cylinder oriented along the z axis and compare it for two elements located separately in hoop direction for coarsely meshed model
Specification(s): 3D_hoop_strain_comparison_coarse_zaxis
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.25.1Anisotropic plasticity must yield same results as finite strain elasticity if yield condition is never met
Specification(s): anis_plasticity_test
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.25.2Anisotropic plasticity must yield same results as finite strain elasticity if yield condition is never met –elasticity
Specification(s): anis_elasticity_test
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.25.3Anisotropic plasticity with isotropic elasticity must reproduce simplified verification problem along x axis
Specification(s): ad_aniso_plasticity_x
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.25.4Anisotropic plasticity with hill tensor rotation must produce simplified verification problem along x axis
Specification(s): ad_aniso_plasticity_x_rotate
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.25.5Anisotropic plasticity with isotropic elasticity must reproduce simplified verification problem along y axis
Specification(s): ad_aniso_plasticity_y
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #16016
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.87.1The system shall be capable of simulating materials that exhibit orthotropic plasticity with constant hardening and linear strain applied in the x and y directions.
Specification(s): test
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #3832
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.87.2The system shall be capable of simulating materials that exhibit orthotropic plasticity with power rule hardening and linear strain applied in the x direction.
Specification(s): power_rule
Design: SolidMechanicsPlasticOrthotropic
Issue(s): #3832
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Rank Two Scalar Aux
8.26.1The system shall compute the VonMises value of a RankTwoTensor
Specification(s): ranktwoscalaraux
Design: Rank Two Scalar Aux
Issue(s): #4774
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.26.2The system shall allow RankTwoScalarAux to output principal stresses
Specification(s): principalstress
Design: Rank Two Scalar Aux
Issue(s): #5516
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.122.1The system shall correctly compute an eigenstrain tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain.
Specification(s): volumetric_eigenstrain
Design: Compute Volumetric Eigenstrain Rank Two Scalar Aux
Issue(s): #8615 #11743
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.122.2The system shall correctly compute an eigenstrain using AD tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain.
Specification(s): ad_volumetric_eigenstrain
Design: AD Compute Volumetric Eigenstrain Rank Two Scalar Aux
Issue(s): #8615 #11743 #26880
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.122.3The volumetric strain computed using RankTwoScalarAux for a unit cube with imposed displacements shall be identical to that obtained by imposing an eigenstrain that causes the same deformation of that model.
Specification(s): volumetric_mechanical
Design: Compute Volumetric Eigenstrain Rank Two Scalar Aux
Issue(s): #8615 #11743
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ElasticEnergyAux
8.26.3The system shall compute the local elastic energy
Specification(s): tensorelasticenergyaux
Design: ElasticEnergyAux
Issue(s): #13635
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.1The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes.
Specification(s): elastic_patch
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.2The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.
Specification(s): elastic_patch_incremental_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.3The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.
Specification(s): elastic_patch_total_small
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Small Strain Compute Linear Elastic Stress
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.4The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.
Specification(s): elastic_patch_incremental_small_no_disp_mesh
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Incremental Strain Compute Finite Strain Elastic Stress
Issue(s): #12584 #12580
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.5The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.
Specification(s): elastic_patch_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.6The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when running on 2 processors in parallel.
Specification(s): elastic_patch_2Procs
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.7The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.
Specification(s): elastic_patch_2Procs_Bbar
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress Volumetric Locking Correction
Issue(s): #458
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.46.8The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular 20-noded quadratic hexes.
Specification(s): elastic_patch_quadratic
Design: ElasticEnergyAux Compute Isotropic Elasticity Tensor Compute Finite Strain Elastic Stress
Issue(s): #620
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Line Element Action System
8.27.1The LineElementAction class shall correctly create the objects required for a mechanics simulation using beam or truss elements.
Specification(s): 2_block_action
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.2The LineElementAction class shall correctly set the common parameters in the action subblocks.
Specification(s): 2_block_common_action
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.3The LineElementAction class shall produce an error when the displacement variables are not provided by the user.
Specification(s): beam_action_test1
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.4The LineElementAction class shall produce an error if the user provided inputs for strain_type, rotation_type and use_displaced_mesh parameters are not compatible.
Specification(s): beam_action_test2
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.5The LineElementAction class shall produce an error if the number of variables listed in the save_in parameter differs from the number of displacement variables.
Specification(s): beam_action_test3
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.6The LineElementAction class shall produce an error if the number of variables listed in the diag_save_in parameter differs from the number of displacement variables.
Specification(s): beam_action_test4
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.7The LineElementAction class shall produce an error if the names for the rotational degrees of freedom are not provided by the user.
Specification(s): beam_action_test5
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.8The LineElementAction class shall produce an error if the number of rotational variables provided as input differs from the number of displacement variables.
Specification(s): beam_action_test6
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.9The LineElementAction class shall produce an error if the moment of inertia, area and orientation of the beam are not provided as input.
Specification(s): beam_action_test7
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.10The LineElementAction class shall produce an error if translational and rotational velocities and accelerations are not provided as input for dynamic simulations using beam elements.
Specification(s): beam_action_test8
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.11The LineElementAction class shall produce an error if the number of translational and rotational velocities and accelerations differs from the number of displacement variables.
Specification(s): beam_action_test9
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.12The LineElementAction class shall produce an error if Newmark time integration parameters (beta and gamma) are not provided as input for dynamic simulations using beam elements.
Specification(s): beam_action_test10
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.13The LineElementAction class shall produce an error if density is not provided as input for dynamic beam simulations using beams elements with consistent mass/inertia matrix.
Specification(s): beam_action_test11
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.14The LineElementAction class shall produce an error if nodal mass is not provided as input for dynamic beam simulations using beam elements with nodal mass matrix.
Specification(s): beam_action_test12
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.15The LineElementAction class shall produce an error if nodal inertia is not provided as input for dynamic beam simulations using beam elements with nodal inertia matrix.
Specification(s): beam_action_test13
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.16The LineElementAction class shall produce an error if multiple subblocks specify properties for the same mesh block.
Specification(s): beam_action_test14
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.17The LineElementAction class shall produce an error if an action subblock is mesh block restricted while another is not.
Specification(s): beam_action_test15
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.18The LineElementAction class shall produce an error if dynamic_nodal_translational_inertia is set to true in the common action block but the subblocks do not have the parameters required for a dynamic beam simulation using beam elements.
Specification(s): beam_action_test16
Design: Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.30The LineElementAction shall create the translational and rotational velocities and accelerations required for a dynamic simulation using beam elements.
Specification(s): add_dynamic_variables_action
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.33The LineElementAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and a consistent mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): dyn_euler_rayleigh_hht_action
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.34The LineElmentAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and nodal mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): dyn_euler_added_mass_inertia_damping_action
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.51The LineElementAction class shall produce an error if add_dynamic_variables option is set to false while dynamic_consistent_inertia, dynamic_nodal_rotational_inertia or dynamic_nodal_translational_inertia options are set to true.
Specification(s): error_16
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: C0 Timoshenko Beam Element
8.27.19The mechanics system shall accurately predict the displacement of a beam element with a frictionless contact constraint.
Specification(s): frictionless_constraint
Design: C0 Timoshenko Beam Element
Issue(s): #14873
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.27.20The mechanics system shall accurately predict the displacement of a beam element with a glued contact constraint.
Specification(s): glued_constraint
Design: C0 Timoshenko Beam Element
Issue(s): #14873
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.27.21The mechanics system shall accurately predict the displacement of a beam element with a frictional contact constraint.
Specification(s): frictional_constraint
Design: C0 Timoshenko Beam Element
Issue(s): #14873
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.27.22The mechanics system shall correctly predict the natural frequencies of an Euler-Bernoulli beam modeled using beam elements with consistent mass/inertia.
Specification(s): dyn_euler
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.23The mechanics system shall correctly predict the natural frequencies of a Timoshenko beam modeled using beam elements with consistent mass/inertia.
Specification(s): dyn_timoshenko
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.24The mechanics system shall correctly predict the natural frequencies of an Euler-Bernoulli beam modeled using beam elements in the presence of Rayleigh damping and numerical damping introduced by Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): dyn_euler_rayleigh_hht
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.25The mechanics system shall correctly predict the natural frequencies of an Euler-Bernoulli beam modeled using beam elements in the presence of Rayleigh damping and numerical damping introduced by Hilber-Hughes-Taylor (HHT) time integration when using the velocity and acceleration computed using the Newmark-Beta time integrator.
Specification(s): dyn_euler_rayleigh_hht_ti
Design: C0 Timoshenko Beam Element
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.26The mechanics system shall correctly predict the natural frequencies of a massless Euler-Bernoulli beam modeled using beam elements with a nodal masses placed at the ends.
Specification(s): dyn_euler_added_mass
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.27The mechanics system shall correctly predict the natural frequencies of a massless Euler-Bernoulli beam modeled using beam elements with added nodal masses when the location and values of the masses are provided using a csv file.
Specification(s): dyn_euler_added_mass_file
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.28The mechanics system shall correctly model the response of a beam modeled using beam elements when gravitational force (proportional to nodal mass) is applied to the beam.
Specification(s): dyn_euler_added_mass_gravity
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.29The mechanics system shall correctly model the response of a beam modeled using beam elements under gravitational force when the nodal mass distribution is provided using a csv file.
Specification(s): dyn_euler_added_mass_gravity_2
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.30The LineElementAction shall create the translational and rotational velocities and accelerations required for a dynamic simulation using beam elements.
Specification(s): add_dynamic_variables_action
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.31The mechanics system shall correctly model the response of a beam modeled using beam elements in the presence of nodal mass, nodal inertia and Rayleigh damping.
Specification(s): dyn_euler_added_mass_inertia_damping
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.32The mechanics system shall correctly model the response of a beam modeled using beam elements in the presence of nodal mass, nodal inertia and Rayleigh damping when using the velocity and accelerations computed by the Newmark-Beta time integrator.
Specification(s): dyn_euler_added_mass_inertia_damping_ti
Design: C0 Timoshenko Beam Element
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.33The LineElementAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and a consistent mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): dyn_euler_rayleigh_hht_action
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.34The LineElmentAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and nodal mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): dyn_euler_added_mass_inertia_damping_action
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.35The mechanics system shall correctly predict the natural frequency of a cantilever beam modeled using beam elements with a mass at the free end.
Specification(s): dyn_euler_added_mass2
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.27.36The InertialForceBeam class shall produce an error if the number of variables provided for rotations differs from that provided for displacements.
Specification(s): error_1
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.37The NodalRotatioanlInertia class shall produce an error if the number of rotational velocities and accelerations provided as input differ from the number of rotations.
Specification(s): error_2
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.38The NodalRotationalInertia class shall produce an error if the user provided nodal inertia is not positive definite.
Specification(s): error_3
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.39The NodalRotatioanlInertia class shall produce an error if the user provided x and y orientations are not unit vectors.
Specification(s): error_4
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.40The NodalRotatioanlInertia class shall produce an error if the user provided x and y orientations are not perpendicular to each other.
Specification(s): error_5
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.41The NodalRotatioanlInertia class shall produce an error if only x or y orientation is provided as input by the user.
Specification(s): error_6
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.42The InertialForceBeam class shall produce an error if the number of translational and rotational velocities and accelerations provided as input differ from the number of displacement variables.
Specification(s): error_7
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.43The NodalTranslationalInertia class shall produce an error if nodal mass is provided as input both as a constant value and also using a csv file.
Specification(s): error_8
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.44The NodalTranslationalInertia class shall produce an error if nodal mass is not provided as input either as a constant value or using a csv file.
Specification(s): error_9
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.45The NodalTranslationalInertia class shall produce an error if the number of columns in the nodal mass file is not 4.
Specification(s): error_10
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.46The NodalTranslationalInertia class shall produce an error if all the nodal positions provided in the nodal mass file cannot be found in the given boundary or mesh block.
Specification(s): error_11
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.47The NodalGravity class shall produce an error if nodal mass is provided as input both as a constant value and also using a csv file.
Specification(s): error_12
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.48The NodalGravity class shall produce an error if nodal mass is not provided as input either as a constant value or using a csv file.
Specification(s): error_13
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.49The NodalGravity class shall produce an error if the number of columns in the nodal mass file is not 4.
Specification(s): error_14
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.50The NodalGravity class shall produce an error if all the nodal positions provided in the nodal mass file cannot be found in the given boundary or mesh block.
Specification(s): error_15
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.51The LineElementAction class shall produce an error if add_dynamic_variables option is set to false while dynamic_consistent_inertia, dynamic_nodal_rotational_inertia or dynamic_nodal_translational_inertia options are set to true.
Specification(s): error_16
Design: C0 Timoshenko Beam Element Line Element Action System
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.52The NodalTranslationalInertia class shall produce an error if nodal mass is provided as input both as constant value and also using a csv file.
Specification(s): error_17
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.56The mechanics system shall accurately predict the static bending response of a Timoshenko beam modeled using beam elements under small deformations in the y direction.
Specification(s): timoshenko_small_strain_y
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.57The mechanics system shall accurately predict the static bending response of a Timoshenko beam modeled using beam elements under small deformations in the z direction.
Specification(s): timoshenko_small_strain_z
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.58The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under small deformations in the y direction.
Specification(s): euler_small_strain_y
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.59The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under small deformations in the z direction.
Specification(s): euler_small_strain_z
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.60The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under finite deformations in the y direction.
Specification(s): euler_finite_rot_y
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.61The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under finite deformations in the z direction.
Specification(s): euler_finite_rot_z
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.62The LineElementAction class shall accurately create the objects required to model the static bending response of an Euler-Bernoulli beam modeled using beam elements under small deformations.
Specification(s): euler_small_y_with_action
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.63The LineElementAction class shall accurately create the objects required to model the static bending response of an Euler-Bernoulli beam modeled using beam elements under finite deformations.
Specification(s): euler_finite_y_with_action
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.64The mechanics system shall accurately predict the axial displacement of an Euler-Bernoulli pipe modeled using beam elements.
Specification(s): euler_pipe_axial_disp
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.27.65The mechanics system shall accurately predict the axial forces on an Euler-Bernoulli pipe modeled using beam elements.
Specification(s): euler_pipe_axial_force
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): CSVDiff
Verification: Beams
8.27.66The mechanics system shall accurately predict the bending response of an Euler-Bernoulli pipe modeled using beam elements.
Specification(s): euler_pipe_bend
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.27.67The ComputeIncrementalBeamStrain class shall produce an error if the number of supplied displacements and rotations do not match.
Specification(s): error_displacements1
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.68The StressDivergenceBeam class shall produce an error if the number of supplied displacements and rotations do not match.
Specification(s): error_displacements2
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.69The ComputeIncrementalBeamStrain class shall produce an error if large strain calculation is requested for asymmetric beam configurations with non-zero first or third moments of area.
Specification(s): error_large_strain
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.70The ComputeIncrementalBeamStrain class shall produce an error if the y orientation provided is not perpendicular to the beam axis.
Specification(s): error_y_orientation
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.27.71The mechanics system shall accurately predict the torsional response of a beam modeled using beam elements with auto-calculated polar moment of inertia.
Specification(s): torsion_1
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
Verification: Beams
8.27.72The mechanics system shall accurately predict the torsional response of a beam modeled using beam elements with user provided polar moment of inertia.
Specification(s): torison_2
Design: C0 Timoshenko Beam Element
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.73
The mechanics system shall accurately predict the static bending response of an Euler beam modeled using beam elements under small deformation when the beam is
1. oriented along the global Z axis.
2. oriented on the YZ plane at a 45 deg. angle.
3. oriented on the YZ plane at a 45 deg. angle and has in-plane loading.
4. oriented on the YZ plane at a 45 deg. angle and has in-plane loading with non-symmetric cross section geometry.
5. oriented on the YZ plane at a 45 deg. angle and has in-plane loading and the cross section geometry is non-symmetric.
6. oriented along the global Y axis.
7. oriented on the XZ plane at a 45 deg. angle.
8. oriented on the XZ plane at a 45 deg. angle, and the external loading takes place on the same plane.
9. oriented on the XY plane at a 45 deg. angle.
10. oriented on the XY plane at a 45 deg. angle, and the external loading takes place on the same plane.
Specification(s): euler_small_strain/orientation_z, euler_small_strain/orientation_yz, euler_small_strain/orientation_yz_force_yz, euler_small_strain/orientation_yz_force_yz_cross_section, euler_small_strain/orientation_yz_cross_section, euler_small_strain/orientation_y, euler_small_strain/orientation_xz, euler_small_strain/orientation_xz_force_xz, euler_small_strain/orientation_xy, euler_small_strain/orientation_xy_force_xy
Design: C0 Timoshenko Beam Element
Issue(s): #14772
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.27.74
The mechanics system shall accurately predict the static bending response of an Euler beam modeled using beam elements under small deformations when the beam is
1. subjected to simply supported BCs and distributed loading.
2. subjected to combined bending and torsion loading.
Specification(s): verification_tests/ansys_vm2, verification_tests/ansys_vm12
Design: C0 Timoshenko Beam Element
Issue(s): #14772
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Thermal Expansion Eigenstrain Beam
8.27.53The ComputeThermalExpansionEigenstrainBeam class shall correctly calculate eigenstrains due to changes in temperature.
Specification(s): thermal_eigenstrain
Design: Compute Thermal Expansion Eigenstrain Beam
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Eigenstrain Beam From Variable
8.27.54The ComputeEigenstrainBeamFromVariable class shall correctly transfer eigenstrains from auxvariables into eigenstrain material property.
Specification(s): eigenstrain_from_var
Design: Compute Eigenstrain Beam From Variable
Issue(s): #10313
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.27.55The ComputeEigenstrainBeamFromVariable class shall report an error if less than 3 displacement or rotational eigenstrains are provided by the user.
Specification(s): eigenstrain_from_var_test1
Design: Compute Eigenstrain Beam From Variable
Issue(s): #10313
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: CappedWeakPlaneStressUpdate
8.30.1The CappedWeakPlaneStressUpdate model shall generate an error if the friction angle is negative
Specification(s): except1
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.30.2The CappedWeakPlaneStressUpdate model shall generate an error if the dilation angle is negative
Specification(s): except2
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.30.3The CappedWeakPlaneStressUpdate model shall generate an error if the friction angle is less than the dilation angle
Specification(s): except3
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.30.4The CappedWeakPlaneStressUpdate model shall generate an error if the cohesion is negative
Specification(s): except4
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.30.5The CappedWeakPlaneStressUpdate model shall generate an error if the sum of the tensile and compressive strength is less than smoothing_tol
Specification(s): except5
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.30.6The CappedWeakPlaneStressUpdate model shall generate an error if the normal vector has zero length
Specification(s): except6
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.30.7The CappedWeakPlaneStressUpdate model shall correctly compute stresses in the elastic regime
Specification(s): small1
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.8The CappedWeakPlaneStressUpdate model shall correctly represent tensile failure with the Lame coefficient lambda=0
Specification(s): small2
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.9The CappedWeakPlaneStressUpdate model shall correctly represent tensile failure with the Lame coefficient lambda=4
Specification(s): small3
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.10The CappedWeakPlaneStressUpdate model shall correctly represent compression failure
Specification(s): small4
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.11The CappedWeakPlaneStressUpdate model shall correctly represent shear failure
Specification(s): small5
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.12The CappedWeakPlaneStressUpdate model shall correctly represent both tensile and shear failure
Specification(s): small6
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.13The CappedWeakPlaneStressUpdate model shall correctly represent tensile behavior with hardening
Specification(s): small7
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.14The CappedWeakPlaneStressUpdate model shall correctly represent compression behavior with hardening
Specification(s): small8
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.15The CappedWeakPlaneStressUpdate model shall correctly represent shear behavior with hardening
Specification(s): small9
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.16The CappedWeakPlaneStressUpdate model shall correctly represent hardening under combined tension and shear
Specification(s): small10
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.17The CappedWeakPlaneStressUpdate model shall correctly represent hardening under combined tension and shear with an initial stress
Specification(s): small11
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.18The CappedWeakPlaneStressUpdate model shall correctly represent the behavior of a column of elements that is pulled, then pushed
Specification(s): pull_push
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.30.19The CappedWeakPlaneStressUpdate model shall correctly represent the behavior of a column of elements that is pulled, then pushed, with tensile hardening
Specification(s): pull_push_h
Design: CappedWeakPlaneStressUpdate
Issue(s): #7784
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.30.20The CappedWeakPlaneStressUpdate model shall correctly represent the behavior of a beam with its ends fully clamped
Specification(s): cwp_beam
Design: CappedWeakPlaneStressUpdate
Issue(s): #7960
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.30.21The CappedWeakPlaneStressUpdate model shall correctly represent the tensile failure of a single layer of elements in 1 nonlinear step
Specification(s): pull_and_shear_1step
Design: CappedWeakPlaneStressUpdate
Issue(s): #7960
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.30.22The CappedWeakPlaneStressUpdate model shall correctly represent a dynamic problem with plasticity in which a column of material is pulled in tension
Specification(s): pull_and_shear
Design: CappedWeakPlaneStressUpdate
Issue(s): #7960
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.30.23The CappedWeakPlaneStressUpdate model shall correctly represent a dynamic problem with plasticity in which a column of material is pushed in compression
Specification(s): push_and_shear
Design: CappedWeakPlaneStressUpdate
Issue(s): #7960
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.30.24The system shall permit exceptions to be thrown from material models with stateful properties without reading/writing to/from uninitialized memory
Specification(s): throw_test
Design: CappedWeakPlaneStressUpdate
Issue(s): #7960
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: CappedWeakInclinedPlaneStressUpdate
8.30.25The CappedWeakInclinedPlaneStressUpdate model shall correctly represent tensile failure with a specified normal=(1,0,0)
Specification(s): small_inclined2
Design: CappedWeakInclinedPlaneStressUpdate
Issue(s): #8303
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.26The CappedWeakPlaneStressUpdate model shall correctly represent tensile failure with a specified normal=(0,1,0)
Specification(s): small_inclined3
Design: CappedWeakInclinedPlaneStressUpdate
Issue(s): #8303
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.27The CappedWeakPlaneStressUpdate model shall correctly represent shear failure with a specified normal=(1,0,0)
Specification(s): small_inclined5
Design: CappedWeakInclinedPlaneStressUpdate
Issue(s): #8303
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: CappedWeakPlaneCosseratStressUpdate
8.30.28The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a first set of loading conditions
Specification(s): small_cosserat1
Design: CappedWeakPlaneCosseratStressUpdate
Issue(s): #8431
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.29The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a second set of loading conditions
Specification(s): small_cosserat2
Design: CappedWeakPlaneCosseratStressUpdate
Issue(s): #8431
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.30The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a third set of loading conditions
Specification(s): small_cosserat3
Design: CappedWeakPlaneCosseratStressUpdate
Issue(s): #8431
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.30.31The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a fourth set of loading conditions
Specification(s): small_cosserat4
Design: CappedWeakPlaneCosseratStressUpdate
Issue(s): #8431
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: CentralDifference
8.31.1The NewmarkBeta timeintegrator shall correctly calculate the response of a 1D mesh.
Specification(s): implicit
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.2The CentralDifference timeintegrator shall correctly calculate the response of a 1D mesh when the the consistent mass matrix option is used.
Specification(s): explicit
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.3The NewmarkBeta timeintegrator shall correctly calculate the response of a 2D mesh.
Specification(s): implicit
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.4The CentralDifference timeintegrator shall correctly calculate the response of a 2D mesh when the the consistent mass matrix option is used.
Specification(s): explicit
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.5The NewmarkBeta timeintegrator shall correctly calculate the response of a 3D mesh.
Specification(s): implicit
Design: CentralDifference
Issue(s): #13964 #9726 #22997
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.6The CentralDifference timeintegrator shall correctly calculate the response of a 3D mesh when the the consistent mass matrix option is used.
Specification(s): explicit
Design: CentralDifference
Issue(s): #13964 #9726 #22997
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.7The central difference time integrator time step can be increased by selecting density scaling.
Specification(s): explicit_mass_scaling
Design: CentralDifference
Issue(s): #13964 #9726 #22997
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.31.8The system shall include central difference time integration that correctly calculates the response of a 1D mesh with nodal masses equal to those of a corresponding lumped mass system.
Specification(s): explicit_nodalmass
Design: CentralDifference
Issue(s): #13964 #9726 #16163
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.9The system shall include Newmark-beta time integration that correctly calculate the response of a 1D mesh with nodal masses equal to those of a corresponding lumped mass system.
Specification(s): implicit_nodalmass
Design: CentralDifference
Issue(s): #13964 #9726 #16163
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.10The system shall include a central difference time integration that when used with the lumped mass shall correctly calculate the response of a 1D mesh and produce results that are identical to those calculated using equivalent nodal masses.
Specification(s): explicit_lumped
Design: CentralDifference
Issue(s): #13964 #9726 #16163
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.11The system shall include central difference time integration that when used with the constant mass option shall correctly calculate the response of a 1D mesh and produce results that are identical to those calculated using equivalent nodal masses.
Specification(s): explicit_constant_mass
Design: CentralDifference
Issue(s): #13964 #9726 #16163
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.12The system shall include central difference time integration that correctly calculates the response of a 2D mesh with nodal masses equal to those of a corresponding lumped mass system.
Specification(s): explicit_nodalmass
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.13The system shall include Newmark-beta time integration that correctly calculates the response of a 2D mesh with nodal masses equal to those of a corresponding lumped mass system.
Specification(s): implicit_nodalmass
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.14The system syall include central difference time integration that when used with the lumped mass option shall correctly calculate the response of a 2D mesh and produce results that are identical to those calculated using equivalent nodal masses.
Specification(s): explicit_lumped
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.15The system syall include central difference time integration that when used with the constant mass option shall correctly calculate the response of a 2D mesh and produce results that are identical to those calculated using equivalent nodal masses.
Specification(s): explicit_constant_mass
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.16The system shall include central difference time integration that correctly calculates the response of a 3D mesh with nodal masses equal to those of a corresponding lumped mass system.
Specification(s): explicit_nodalmass
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.17The system shall include Newmar-beta time integration that correctly calculates the response of a 3D mesh with nodal masses equal to those of a corresponding lumped mass system.
Specification(s): implicit_nodalmass
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.18The system shall include central difference time integration that when used with the lumped mass option shall correctly calculate the response of a 3D mesh and produce results that are identical to those calculated using equivalent nodal masses.
Specification(s): explicit_lumped
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.31.19The system shall include central difference time integration that when used with the constant mass option shall correctly calculate the response of a 3D mesh and produce results that are identical to those calculated using equivalent nodal masses.
Specification(s): explicit_constant_mass
Design: CentralDifference
Issue(s): #13964 #9726
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: PureElasticTractionSeparation
8.33.1
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
2. The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
3. The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material
4. The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material
5. The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries
6. The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction
7. The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction
8. The system shall use the common block generate output and additional outputs for all CZM blocks
9. The system shall add additional outputs requested within each block
10. The system shall be able to use different output orders on different blocks
11. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.
12. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
13. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
14. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
15. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
16. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
17. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material.
18. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material.
Specification(s): czm_framework/jacobian_small_strain, czm_framework/jacobian_total_lagrangian, czm_framework/small_strain_incremental, czm_framework/total_lagrangian_incremental, czm_framework/multiple_action_and_materials, czm_framework/multiple_action_different_strain, czm_framework/czm_multiple_action_overlapping_boundary, czm_framework/multiple_action_common_outputs, czm_framework/czm_multiple_action_additional_outputs_on_different_block, czm_framework/multiple_action_differnt_outputs_orders_on_different_block, czm_framework/action_3D_small_strain_normal, czm_framework/action_2D_small_strain_normal, czm_framework/action_1D_small_strain_normal, czm_framework/action_3D_total_lagrangian_normal, czm_framework/action_2D_total_lagrangian_normal, czm_framework/action_1D_total_lagrangian_normal, czm_framework/czm_incremental_stretch_rotate_total_lagrangian, czm_framework/czm_total_stretch_rotate_total_lagrangian
Design: PureElasticTractionSeparation CZMComputeDisplacementJumpSmallStrain CZMComputeGlobalTractionSmallStrain CZM InterfaceKernelSmallStrain CZMComputeDisplacementJumpTotalLagrangian CZMComputeGlobalTractionTotalLagrangian CZMInterfaceKernelTotalLagrangian
Issue(s): #11546 #14527 #17156 #18611
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): ExodiffRunExceptionCSVDiff

solid_mechanics: CZMComputeDisplacementJumpSmallStrain
8.33.1
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
2. The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
3. The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material
4. The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material
5. The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries
6. The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction
7. The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction
8. The system shall use the common block generate output and additional outputs for all CZM blocks
9. The system shall add additional outputs requested within each block
10. The system shall be able to use different output orders on different blocks
11. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.
12. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
13. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
14. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
15. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
16. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
17. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material.
18. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material.
Specification(s): czm_framework/jacobian_small_strain, czm_framework/jacobian_total_lagrangian, czm_framework/small_strain_incremental, czm_framework/total_lagrangian_incremental, czm_framework/multiple_action_and_materials, czm_framework/multiple_action_different_strain, czm_framework/czm_multiple_action_overlapping_boundary, czm_framework/multiple_action_common_outputs, czm_framework/czm_multiple_action_additional_outputs_on_different_block, czm_framework/multiple_action_differnt_outputs_orders_on_different_block, czm_framework/action_3D_small_strain_normal, czm_framework/action_2D_small_strain_normal, czm_framework/action_1D_small_strain_normal, czm_framework/action_3D_total_lagrangian_normal, czm_framework/action_2D_total_lagrangian_normal, czm_framework/action_1D_total_lagrangian_normal, czm_framework/czm_incremental_stretch_rotate_total_lagrangian, czm_framework/czm_total_stretch_rotate_total_lagrangian
Design: PureElasticTractionSeparation CZMComputeDisplacementJumpSmallStrain CZMComputeGlobalTractionSmallStrain CZM InterfaceKernelSmallStrain CZMComputeDisplacementJumpTotalLagrangian CZMComputeGlobalTractionTotalLagrangian CZMInterfaceKernelTotalLagrangian
Issue(s): #11546 #14527 #17156 #18611
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): ExodiffRunExceptionCSVDiff

solid_mechanics: CZMComputeGlobalTractionSmallStrain
8.33.1
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
2. The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
3. The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material
4. The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material
5. The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries
6. The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction
7. The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction
8. The system shall use the common block generate output and additional outputs for all CZM blocks
9. The system shall add additional outputs requested within each block
10. The system shall be able to use different output orders on different blocks
11. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.
12. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
13. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
14. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
15. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
16. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
17. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material.
18. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material.
Specification(s): czm_framework/jacobian_small_strain, czm_framework/jacobian_total_lagrangian, czm_framework/small_strain_incremental, czm_framework/total_lagrangian_incremental, czm_framework/multiple_action_and_materials, czm_framework/multiple_action_different_strain, czm_framework/czm_multiple_action_overlapping_boundary, czm_framework/multiple_action_common_outputs, czm_framework/czm_multiple_action_additional_outputs_on_different_block, czm_framework/multiple_action_differnt_outputs_orders_on_different_block, czm_framework/action_3D_small_strain_normal, czm_framework/action_2D_small_strain_normal, czm_framework/action_1D_small_strain_normal, czm_framework/action_3D_total_lagrangian_normal, czm_framework/action_2D_total_lagrangian_normal, czm_framework/action_1D_total_lagrangian_normal, czm_framework/czm_incremental_stretch_rotate_total_lagrangian, czm_framework/czm_total_stretch_rotate_total_lagrangian
Design: PureElasticTractionSeparation CZMComputeDisplacementJumpSmallStrain CZMComputeGlobalTractionSmallStrain CZM InterfaceKernelSmallStrain CZMComputeDisplacementJumpTotalLagrangian CZMComputeGlobalTractionTotalLagrangian CZMInterfaceKernelTotalLagrangian
Issue(s): #11546 #14527 #17156 #18611
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): ExodiffRunExceptionCSVDiff

solid_mechanics: CZM InterfaceKernelSmallStrain
8.33.1
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
2. The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
3. The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material
4. The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material
5. The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries
6. The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction
7. The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction
8. The system shall use the common block generate output and additional outputs for all CZM blocks
9. The system shall add additional outputs requested within each block
10. The system shall be able to use different output orders on different blocks
11. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.
12. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
13. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
14. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
15. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
16. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
17. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material.
18. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material.
Specification(s): czm_framework/jacobian_small_strain, czm_framework/jacobian_total_lagrangian, czm_framework/small_strain_incremental, czm_framework/total_lagrangian_incremental, czm_framework/multiple_action_and_materials, czm_framework/multiple_action_different_strain, czm_framework/czm_multiple_action_overlapping_boundary, czm_framework/multiple_action_common_outputs, czm_framework/czm_multiple_action_additional_outputs_on_different_block, czm_framework/multiple_action_differnt_outputs_orders_on_different_block, czm_framework/action_3D_small_strain_normal, czm_framework/action_2D_small_strain_normal, czm_framework/action_1D_small_strain_normal, czm_framework/action_3D_total_lagrangian_normal, czm_framework/action_2D_total_lagrangian_normal, czm_framework/action_1D_total_lagrangian_normal, czm_framework/czm_incremental_stretch_rotate_total_lagrangian, czm_framework/czm_total_stretch_rotate_total_lagrangian
Design: PureElasticTractionSeparation CZMComputeDisplacementJumpSmallStrain CZMComputeGlobalTractionSmallStrain CZM InterfaceKernelSmallStrain CZMComputeDisplacementJumpTotalLagrangian CZMComputeGlobalTractionTotalLagrangian CZMInterfaceKernelTotalLagrangian
Issue(s): #11546 #14527 #17156 #18611
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): ExodiffRunExceptionCSVDiff

solid_mechanics: CZMComputeDisplacementJumpTotalLagrangian
8.33.1
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
2. The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
3. The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material
4. The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material
5. The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries
6. The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction
7. The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction
8. The system shall use the common block generate output and additional outputs for all CZM blocks
9. The system shall add additional outputs requested within each block
10. The system shall be able to use different output orders on different blocks
11. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.
12. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
13. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
14. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
15. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
16. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
17. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material.
18. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material.
Specification(s): czm_framework/jacobian_small_strain, czm_framework/jacobian_total_lagrangian, czm_framework/small_strain_incremental, czm_framework/total_lagrangian_incremental, czm_framework/multiple_action_and_materials, czm_framework/multiple_action_different_strain, czm_framework/czm_multiple_action_overlapping_boundary, czm_framework/multiple_action_common_outputs, czm_framework/czm_multiple_action_additional_outputs_on_different_block, czm_framework/multiple_action_differnt_outputs_orders_on_different_block, czm_framework/action_3D_small_strain_normal, czm_framework/action_2D_small_strain_normal, czm_framework/action_1D_small_strain_normal, czm_framework/action_3D_total_lagrangian_normal, czm_framework/action_2D_total_lagrangian_normal, czm_framework/action_1D_total_lagrangian_normal, czm_framework/czm_incremental_stretch_rotate_total_lagrangian, czm_framework/czm_total_stretch_rotate_total_lagrangian
Design: PureElasticTractionSeparation CZMComputeDisplacementJumpSmallStrain CZMComputeGlobalTractionSmallStrain CZM InterfaceKernelSmallStrain CZMComputeDisplacementJumpTotalLagrangian CZMComputeGlobalTractionTotalLagrangian CZMInterfaceKernelTotalLagrangian
Issue(s): #11546 #14527 #17156 #18611
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): ExodiffRunExceptionCSVDiff

solid_mechanics: CZMComputeGlobalTractionTotalLagrangian
8.33.1
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
2. The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
3. The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material
4. The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material
5. The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries
6. The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction
7. The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction
8. The system shall use the common block generate output and additional outputs for all CZM blocks
9. The system shall add additional outputs requested within each block
10. The system shall be able to use different output orders on different blocks
11. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.
12. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
13. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
14. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
15. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
16. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
17. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material.
18. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material.
Specification(s): czm_framework/jacobian_small_strain, czm_framework/jacobian_total_lagrangian, czm_framework/small_strain_incremental, czm_framework/total_lagrangian_incremental, czm_framework/multiple_action_and_materials, czm_framework/multiple_action_different_strain, czm_framework/czm_multiple_action_overlapping_boundary, czm_framework/multiple_action_common_outputs, czm_framework/czm_multiple_action_additional_outputs_on_different_block, czm_framework/multiple_action_differnt_outputs_orders_on_different_block, czm_framework/action_3D_small_strain_normal, czm_framework/action_2D_small_strain_normal, czm_framework/action_1D_small_strain_normal, czm_framework/action_3D_total_lagrangian_normal, czm_framework/action_2D_total_lagrangian_normal, czm_framework/action_1D_total_lagrangian_normal, czm_framework/czm_incremental_stretch_rotate_total_lagrangian, czm_framework/czm_total_stretch_rotate_total_lagrangian
Design: PureElasticTractionSeparation CZMComputeDisplacementJumpSmallStrain CZMComputeGlobalTractionSmallStrain CZM InterfaceKernelSmallStrain CZMComputeDisplacementJumpTotalLagrangian CZMComputeGlobalTractionTotalLagrangian CZMInterfaceKernelTotalLagrangian
Issue(s): #11546 #14527 #17156 #18611
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): ExodiffRunExceptionCSVDiff

solid_mechanics: CZMInterfaceKernelTotalLagrangian
8.33.1
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
2. The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian
3. The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material
4. The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material
5. The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries
6. The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction
7. The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction
8. The system shall use the common block generate output and additional outputs for all CZM blocks
9. The system shall add additional outputs requested within each block
10. The system shall be able to use different output orders on different blocks
11. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.
12. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
13. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.
14. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
15. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
16. The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.
17. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material.
18. The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material.
Specification(s): czm_framework/jacobian_small_strain, czm_framework/jacobian_total_lagrangian, czm_framework/small_strain_incremental, czm_framework/total_lagrangian_incremental, czm_framework/multiple_action_and_materials, czm_framework/multiple_action_different_strain, czm_framework/czm_multiple_action_overlapping_boundary, czm_framework/multiple_action_common_outputs, czm_framework/czm_multiple_action_additional_outputs_on_different_block, czm_framework/multiple_action_differnt_outputs_orders_on_different_block, czm_framework/action_3D_small_strain_normal, czm_framework/action_2D_small_strain_normal, czm_framework/action_1D_small_strain_normal, czm_framework/action_3D_total_lagrangian_normal, czm_framework/action_2D_total_lagrangian_normal, czm_framework/action_1D_total_lagrangian_normal, czm_framework/czm_incremental_stretch_rotate_total_lagrangian, czm_framework/czm_total_stretch_rotate_total_lagrangian
Design: PureElasticTractionSeparation CZMComputeDisplacementJumpSmallStrain CZMComputeGlobalTractionSmallStrain CZM InterfaceKernelSmallStrain CZMComputeDisplacementJumpTotalLagrangian CZMComputeGlobalTractionTotalLagrangian CZMInterfaceKernelTotalLagrangian
Issue(s): #11546 #14527 #17156 #18611
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): ExodiffRunExceptionCSVDiff

solid_mechanics: Bilinear mixed mode traction separation law
8.33.2
The system shall be able to model decohesion of composites using cohesive zone model
1. under mode I loading.
2. under mode I loading with scaled normal strength.
3. under mode II loading.
4. under mode I loading by lagging the seperation state.
5. under mode I loading with power law propagation criterion.
Specification(s): bilinear_mixed_mode/normal, bilinear_mixed_mode/scale_strength_normal, bilinear_mixed_mode/shear, bilinear_mixed_mode/normal_lag, bilinear_mixed_mode/normal_power_law
Design: Bilinear mixed mode traction separation law
Issue(s): #18611 #18763
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: SalehaniIrani 3D Coupled Traction separation law
8.33.3
The system shall be able to use the small strain and total lagrangian cohesive zone model formulation, demonstrate an exact jacobian, and use the parent action to simplify input an doutput and provide the correct results
1. The system shall converge quadratically when using the handcoded Jacobian of the 3DC traction separation model
2. The 3DC traction separation shall produce only a normal traction when a normal displacement jump is applied.
3. The 3DC traction separation shall produce only a shear traction y when a only a displacement jump along y is applied.
4. The 3DC traction separation shall produce only a shear traction z when a only a displacement jump along z is applied.
Specification(s): material_3DC/jacobian, material_3DC/normal_load, material_3DC/shear_load_y, material_3DC/shear_load_z
Design: SalehaniIrani 3D Coupled Traction separation law
Issue(s): #11546 #14527 #17156
Collection(s): FUNCTIONAL
Type(s): ExodiffCSVDiff

solid_mechanics: ADPureElasticTractionSeparation
8.33.4
The system shall be able to use the small strain cohesive zone model formulation using automatic differentiation
1. The solution obtained using AD CZM shall match
2. the non-AD solution
Specification(s): AD_CZM_small/AD_solution, AD_CZM_small/non_AD_solution
Design: ADPureElasticTractionSeparation
Issue(s): #23855
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.33.5
The system shall be able to use the total lagrangian cohesive zone model formulation using automatic differentiation
1. The solution obtained using AD CZM shall match
2. the non-AD solution
Specification(s): AD_CZM_large/AD_solution, AD_CZM_large/non_AD_solution
Design: ADPureElasticTractionSeparation
Issue(s): #23855
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Multiple Inelastic Stress
8.34.1MOOSE tensor mechanics module shall solve a combined creep and plasticity 1-d bar problem.
Specification(s): combined
Design: Compute Multiple Inelastic Stress
Issue(s): #6873 #8651
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.34.2MOOSE tensor mechanics module shall solve a combined creep and plasticity 1-d bar problem with a non-zero start time.
Specification(s): combined_start_time
Design: Compute Multiple Inelastic Stress
Issue(s): #6873 #8651
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.34.3MOOSE tensor mechanics module shall solve a combined creep and plasticity 3D cube problem with a time-varying pressure BC.
Specification(s): stress_prescribed
Design: Compute Multiple Inelastic Stress
Issue(s): #6873 #8651
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.34.4MOOSE tensor mechanics module shall solve a combined creep and plasticity 3D cube problem with a constant displacement BC and stress relaxation.
Specification(s): stress_relaxation
Design: Compute Multiple Inelastic Stress
Issue(s): #6873 #8651
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.34.5MOOSE tensor mechanics module shall solve a combined creep and plasticity 1-d bar problem with the creep and plasticity models tightly coupled.
Specification(s): creepWithPlasticity
Design: Compute Multiple Inelastic Stress
Issue(s): #6873 #8651
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.1The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation.
Specification(s): isotropic_plasticity_incremental
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.2The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation while prescribing a base name for the isotropic plasticity material properties.
Specification(s): isotropic_plasticity_incremental_base_name
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.3The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation and using the b-bar element volume correction.
Specification(s): isotropic_plasticity_incremental_Bbar
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.4The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation.
Specification(s): isotropic_plasticity_finite
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.5The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation and using the b-bar element volume correction.
Specification(s): isotropic_plasticity_finite_Bbar
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.12The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213.
Specification(s): affine_plasticity
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.99.1The system shall calculate the effect of damage on the stress of a elastic material.
Specification(s): scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.2The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation.
Specification(s): ad_scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.3The system shall calculate damaged stress based on old damage index.
Specification(s): scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.4The system shall calculate damaged stress based on old damage index when using automatic differentiation.
Specification(s): ad_scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.5The system shall report an error when damage index is greater than 1.
Specification(s): scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.6The system shall report an error when damage index is greater than 1 also when using automatic differentiation.
Specification(s): ad_scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.7The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress
Specification(s): scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.8The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation
Specification(s): ad_scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.9The system shall calculate the maximum value of the damage index comparing different damage models.
Specification(s): combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.10The system shall calculate the effective damage index from different damage models.
Specification(s): combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.11The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model
Specification(s): combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.12The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models.
Specification(s): combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.13The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.14The system shall calculate the effective damage index from different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.15The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.16The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.17The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation.
Specification(s): scalar_damage_material_inelastic
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.18The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation.
Specification(s): scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.19The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation.
Specification(s): ad_scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.20The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object.
Specification(s): multiple_inelastic_bad_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #20722
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.21The system shall calculate the effect of damage on the stress of a nonlocal damage model.
Specification(s): nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.22The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation.
Specification(s): ad_nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Coupled Pressure BC
8.35.1The system shall allow to apply a pressure boundary condition from a variable
Specification(s): coupled_pressure
Design: Coupled Pressure BC
Issue(s): #11558
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: CrackFrontNonlocalStress
8.36.1The system shall compute the average stress at each crack point in a 3D domain.
Specification(s): crack_front_stress
Design: CrackFrontNonlocalStress
Issue(s): #27659
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Crack Front Definition
8.37.1The system shall report crack front data for a curved crack front to the console.
Specification(s): screen_output_test
Design: Crack Front Definition
Issue(s): #3275
Collection(s): FUNCTIONAL
Type(s): RunApp

solid_mechanics: Recompute Iterations on the Effective Plastic Strain Increment
8.38.1The system shall compute the proper stress update using the radial return isotropic power law creep model.
Specification(s): ten
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.38.2The system shall compute the proper stress update using multiple radial return isotropic power law creep models where one of the models returns zero.
Specification(s): zero
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.38.3The system shall compute the sum of multiple stress updates using multiple radial return isotropic power law creep models.
Specification(s): sum
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.38.4The system shall support the cycling of multiple creep models when computing stress updates.
Specification(s): cycle
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.38.5The system shall produce the correct Jacobians for radial return isotropic power law creep models.
Specification(s): ten_jacobian
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): AnalyzeJacobian
8.38.6The system shall produce the correct Jacobians for radial return isotropic power law creep models when one of the models returns zero.
Specification(s): zero_jacobian
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): AnalyzeJacobian
8.38.7The system shall produce the correct Jacobians for summed radial return isotropic power law creep models.
Specification(s): sum_jacobian
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): AnalyzeJacobian
8.38.8The systam shall produce the correct Jacobians for cyclic creep model evaluation.
Specification(s): cycle_jacobian
Design: Recompute Iterations on the Effective Plastic Strain Increment
Issue(s): #13232
Collection(s): FUNCTIONAL
Type(s): AnalyzeJacobian

solid_mechanics: Critical Time Step Postprocessor
8.39.1
The system shall correctly compute the critical time step for a solid with:
1. uniform properties and
2. variable properties.
Specification(s): crit_time_solid/uniform, crit_time_solid/variable
Design: Critical Time Step Postprocessor
Issue(s): #13975
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.39.2The system shall correctly compute the critical time step for a beam.
Specification(s): timoshenko_smallstrain_critstep
Design: Critical Time Step Postprocessor
Issue(s): #13975
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.39.3The system shall produce an error if the input elasticity tensor is non-isotropic.
Specification(s): except1
Design: Critical Time Step Postprocessor
Issue(s): #13975
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: AverageSectionValueSampler
8.40.1The system shall compute the average of the nodal displacements of a cross section defined by the user via a nodal vector.
Specification(s): test_one_step
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.40.2The system shall compute the average of the nodal displacements of a cross section defined by the user via a nodal vector at automatically determined positions.
Specification(s): test_one_step_auto_positions
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.40.3The system shall compute the average of the nodal displacements of a cross section at automatically located points that are updated with mesh adaptivity.
Specification(s): test_adapt
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.40.4The system shall compute the average of the nodal displacements of a cross section at automatically located points that are updated with mesh adaptivity.
Specification(s): test_adapt_err
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.40.5The system shall generate an error if the user defines an empty set of positions in AverageSectionValueSampler.
Specification(s): test_one_step_empty_positions_err
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.40.6The system shall generate an error if the user specifies a nonexistent variable in AverageSectionValueSampler.
Specification(s): test_one_step_nonexistent_variable
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.40.7The system shall compute the average of the nodal displacements of a cross section defined by the user via a nodal vector at multiple steps.
Specification(s): test_one_step_heavy
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.40.8The system shall compute the average of the nodal displacements of a cross section defined by the user via two nodal vector and two reference points for two respective ducts.
Specification(s): test_one_step_two_ducts
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.40.9The system shall compute the average of the nodal displacements of a cross section with mechanically and thermally induced deformation.
Specification(s): test_therm_exp
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.40.10The system shall compute the average of the nodal displacements of a cross section with mechanically and thermally induced deformation with a symmetry plane not aligned with a Cartesian coordinate, and match a reference solution without the symmetry plane.
Specification(s): test_therm_exp_symm
Design: AverageSectionValueSampler
Issue(s): #26165
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Crystal Plasticity Thermal Eigenstrain
8.41.1The system shall produce correct thermal deformation gradient values with changing temperature
Specification(s): thermal_eigenstrain
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.3The system shall produce correct deformation gradient values for the total and individual eigenstrains
Specification(s): multiple_eigenstrains
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.4The system shall produce correct thermal deformation gradient values with changing temperature under a 011 loading orientation
Specification(s): thermal_eigenstrain_011orientation
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.5The system shall produce correct thermal deformation gradient values with changing temperature for an anisotropic HCP crystal lattice
Specification(s): hcp_thermal_eigenstrain
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Multiple Crystal Plasticity Stress
8.41.1The system shall produce correct thermal deformation gradient values with changing temperature
Specification(s): thermal_eigenstrain
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.2The system shall produce correct thermal deformation gradient values when the simulation is restarted
Specification(s): thermal_eigenstrain_restart
Design: Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.3The system shall produce correct deformation gradient values for the total and individual eigenstrains
Specification(s): multiple_eigenstrains
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.4The system shall produce correct thermal deformation gradient values with changing temperature under a 011 loading orientation
Specification(s): thermal_eigenstrain_011orientation
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.5The system shall produce correct thermal deformation gradient values with changing temperature for an anisotropic HCP crystal lattice
Specification(s): hcp_thermal_eigenstrain
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.6The system shall produce a positive isotropic eigenstrain in response to an increasing number density and shall demonstrate an applied shear stress on the slip systems with a z-component in response to the BCs on displacement in the z-direction.
Specification(s): volumetric_eigenstrain_increase
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.7The system shall continue the isotropic eigenstrain response calculation upon simulation restart.
Specification(s): volumetric_eigenstrain_increase_restart
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.8The system shall produce a negative isotropic eigenstrain in response to an decreasing average radius and shall demonstrate an applied stress on the slip systems with a z-component in response to the BC constraints on displacement of the crystal in the z-direction.
Specification(s): hcp_volumetric_eigenstrain_decrease
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.9The system shall produce an isotropic eigenstrain in response to parabolic evolution of both the void number density and average radius, and shall induce plastic deformation in the crystal plasticity reponse through the state dependance of the deformation gradient that final strain state of the FCC crystal is not zero.
Specification(s): volumetric_eigenstrain_parabolic
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.16
Upon simulation restart, the HCP crystal plasticity capability shall:
1. continue to evolve the forest dislocation densities on basal <a> slip planes.
2. continue to compute the slip system strength and resolved applied shear stress for the prismatic<a> and pyramidal<c+a> slip systems.
Specification(s): restart_capabilities/update_method_hcp_basal_active_restart, restart_capabilities/update_method_hcp_aprismatic_capyramidal_restart
Design: Crystal Plasticity HCP Dislocation Slip Beyerlein Update Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.17
The HCP crystal plasticity capability shall:
1. compute the Schmid tensors and resulting resolved applied shear stress for a non-physical representative set of basal, prismatic, and pyramidal slip systems;
2. ensure that the provided lattice parameters match the expectation a = b != c for HCP crystals;
3. ensure that eight indices are given for the Miller-Bravais notation for HCP slip systems;
4. ensure that the Miller-Bravais basal plane indices sum to zero.
5. ensure that the Miller-Bravais indices for the slip direction in the basal plane sum to zero.
6. provide warning messages about constitutive model and slip increment convergence issues when the corresponding input file parameter is set to true.
7. provide warning messages about constitutive model stress convergence issues with the appropriate input file parameter setting.
Specification(s): base_class_hcp/update_method_hcp_representative_slip_systems, base_class_hcp/update_method_hcp_representative_equal_lattice_parameters, base_class_hcp/update_method_hcp_representative_incorrect_index_numbers, base_class_hcp/update_method_hcp_representative_incorrect_basal_plane, base_class_hcp/update_method_hcp_representative_incorrect_basal_slip_direction, base_class_hcp/update_method_hcp_convergence_issue_flag, base_class_hcp/update_method_hcp_stress_convergence_issue_flag
Design: Compute Multiple Crystal Plasticity Stress
Issue(s): #18846
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunExceptionCSVDiff
8.41.18
The crystal plasticity HCP system shall:
1. calculate the Schmid tensor for a set of HCP twin systems given in Miller-Bravais indices and shall calculate a twin volume fraction when using the FCC Kalidindi twinning model with a modified input file.
2. compute a plastic velocity gradient that accounts for deformation contributions from both slip and twinning in an HCP crystal.
Specification(s): coupling_demonstration/modified_kalidindi_for_hcp, coupling_demonstration/demonstration_combined_hcp_slip_twins
Design: Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update CrystalPlasticityTwinningKalidindiUpdate
Issue(s): #18846
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.19The crystal plasticity system shall compute the plastic velocity gradient from both slip and twinning in anHCP crystal upon simulation restart.
Specification(s): demonstration_combined_hcp_slip_twins_restart
Design: Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update CrystalPlasticityTwinningKalidindiUpdate
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.32The system shall provide a StressUpdate material-based extensible crystal plasticity system
Specification(s): update_model_test
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.33The system shall provide a StressUpdate material-based extensible crystal plasticity framework that shall continue the state-dependent calculation upon restart
Specification(s): update_model_test_restart
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.34The material-based crystal plasticity model shall compute the lagrangian stress, PK2 stress, and slip for an orientation not aligned with the Cartesian coordinate system.
Specification(s): update_model_011orientation
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.35A constitutive failure shall trigger an exception leading to a cut time step rather than a failed solve using the stress-update based crystal plasticity implementation
Specification(s): exception
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.36The crystal plasticity system shall provide a substepping capability for improved convergence using the stress-update based crystal plasticity implementation
Specification(s): substep
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.40The system shall apply correct boundary condition after timestep being cut during substepping using the stress-update based crystal plasticity implementation
Specification(s): use_substep_dt
Design: Compute Multiple Crystal Plasticity Stress
Issue(s): #17340
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.41The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (111).
Specification(s): update_euler_angle_111_orientation
Design: Compute Updated Euler Angle Compute Multiple Crystal Plasticity Stress
Issue(s): #19473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.42The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (112).
Specification(s): update_euler_angle_112_orientation
Design: Compute Updated Euler Angle Compute Multiple Crystal Plasticity Stress
Issue(s): #19473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.43The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (123).
Specification(s): update_euler_angle_123_orientation
Design: Compute Updated Euler Angle Compute Multiple Crystal Plasticity Stress
Issue(s): #19473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.44The system shall allow multiple crystal plasticity models to be used in a polycrystalline simulation through the use of the base_name input parameter.
Specification(s): bicrystal_test
Design: Compute Multiple Crystal Plasticity Stress
Issue(s): #21036
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.45The system shall allow multiple crystal plasticity models to be used in a polycrystalline simulation with the restart capability.
Specification(s): bicrystal_test_restart
Design: Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.52
Upon simulation restart, the crystal plasticity capability shall:
1. continue to compute the plastic shear due to twinning after a simulation restart.
2. continue to calculate plastic shear due to both dislocation slip and twinning when loaded under tension in a 111 orientation in a simulation restart.
Specification(s): restart_capabilities/only_twinning_fcc_restart, restart_capabilities/combined_twinning_slip_111tension_restart
Design: CrystalPlasticityTwinningKalidindiUpdate CrystalPlasticityKalidindiUpdate Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Crystal Plasticity HCP Dislocation Slip Beyerlein Update
8.41.5The system shall produce correct thermal deformation gradient values with changing temperature for an anisotropic HCP crystal lattice
Specification(s): hcp_thermal_eigenstrain
Design: Compute Crystal Plasticity Thermal Eigenstrain Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update
Issue(s): #17734
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.8The system shall produce a negative isotropic eigenstrain in response to an decreasing average radius and shall demonstrate an applied stress on the slip systems with a z-component in response to the BC constraints on displacement of the crystal in the z-direction.
Specification(s): hcp_volumetric_eigenstrain_decrease
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.15
The model for HCP crystal plasticity, using the Beyerlein and Tome (2008) constitutive model, shall:
1. compute the slip system strength and resolved applied shear stress for the prismatic<a> and pyramidal<c+a> slip systems when loaded along the c-axis;
2. evolve the forest dislocation and substructure densities on prismatic<a> slip planes when loaded in an appropriate orientation;
3. evolve the forest dislocation densities on pyramidal <c+a> slip planes and the substructure density when the crystal is loaded in an appropriate orientation.
4. evolve the forest dislocation densities on basal <a> slip planes when the crystal is loaded in an appropriate orientation.
5. prevent the calculation of a negative substructure density increment.
6. prevent the calculation of a negative total forest density.
7. ensure the user specifies a number of the slip systems per mode which is equal to the number of modes;
8. ensure the user specifies an equal total number of slip systems and the sum of the different slip mode systems;
9. ensure the user specifies a number of burgers vectors per mode that is equal to the number of modes;
10. ensure the user specifies a number of slip generation coefficient per mode that is equal to the number of modes;
11. ensure the user specifies a size of slip activation energy per mode that is equal to the specified number of modes;
12. ensure the user specifies a size of slip energy proportionality factor per mode that is equal to the specified number of modes;
13. ensure the user specifies a size of effective shear modulus per mode that is equal to the specified number of modes;
14. ensure the user specifies a size of substructure generation rate coefficient per mode that is equal to the specified number of modes;
15. ensure the user specifies a size of Hall-Petch like coefficient per mode that is equal to the specified number of modes;
16. ensure the user specifies a size of lattice friction values per mode that is equal to the specified number of modes;
Specification(s): constitutive_model/update_method_hcp_aprismatic_capyramidal, constitutive_model/update_method_hcp_aprismatic_active, constitutive_model/update_method_hcp_capyramidal_active, constitutive_model/update_method_hcp_basal_active, constitutive_model/update_method_hcp_no_substructure, constitutive_model/update_method_hcp_no_negative_aprismatic, constitutive_model/update_method_hcp_size_slip_modes, constitutive_model/update_method_hcp_sum_slip_modes_vs_systems, constitutive_model/update_method_hcp_size_burgers_vectors, constitutive_model/update_method_hcp_size_slip_generation, constitutive_model/update_method_hcp_size_activation_energy, constitutive_model/update_method_hcp_size_proportionality_factor, constitutive_model/update_method_hcp_size_shear_modulus, constitutive_model/update_method_hcp_size_substructure_rate, constitutive_model/update_method_hcp_size_hall_petch, constitutive_model/update_method_hcp_size_lattice_friction
Design: Crystal Plasticity HCP Dislocation Slip Beyerlein Update
Issue(s): #18846
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunExceptionCSVDiff
8.41.16
Upon simulation restart, the HCP crystal plasticity capability shall:
1. continue to evolve the forest dislocation densities on basal <a> slip planes.
2. continue to compute the slip system strength and resolved applied shear stress for the prismatic<a> and pyramidal<c+a> slip systems.
Specification(s): restart_capabilities/update_method_hcp_basal_active_restart, restart_capabilities/update_method_hcp_aprismatic_capyramidal_restart
Design: Crystal Plasticity HCP Dislocation Slip Beyerlein Update Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.18
The crystal plasticity HCP system shall:
1. calculate the Schmid tensor for a set of HCP twin systems given in Miller-Bravais indices and shall calculate a twin volume fraction when using the FCC Kalidindi twinning model with a modified input file.
2. compute a plastic velocity gradient that accounts for deformation contributions from both slip and twinning in an HCP crystal.
Specification(s): coupling_demonstration/modified_kalidindi_for_hcp, coupling_demonstration/demonstration_combined_hcp_slip_twins
Design: Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update CrystalPlasticityTwinningKalidindiUpdate
Issue(s): #18846
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.19The crystal plasticity system shall compute the plastic velocity gradient from both slip and twinning in anHCP crystal upon simulation restart.
Specification(s): demonstration_combined_hcp_slip_twins_restart
Design: Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update CrystalPlasticityTwinningKalidindiUpdate
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Crystal Plasticity Volumetric Eigenstrain
8.41.6The system shall produce a positive isotropic eigenstrain in response to an increasing number density and shall demonstrate an applied shear stress on the slip systems with a z-component in response to the BCs on displacement in the z-direction.
Specification(s): volumetric_eigenstrain_increase
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.7The system shall continue the isotropic eigenstrain response calculation upon simulation restart.
Specification(s): volumetric_eigenstrain_increase_restart
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.8The system shall produce a negative isotropic eigenstrain in response to an decreasing average radius and shall demonstrate an applied stress on the slip systems with a z-component in response to the BC constraints on displacement of the crystal in the z-direction.
Specification(s): hcp_volumetric_eigenstrain_decrease
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.9The system shall produce an isotropic eigenstrain in response to parabolic evolution of both the void number density and average radius, and shall induce plastic deformation in the crystal plasticity reponse through the state dependance of the deformation gradient that final strain state of the FCC crystal is not zero.
Specification(s): volumetric_eigenstrain_parabolic
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.10The system shall not attempt to calculate the volumetric eigenstrain from a negative number density of voids.
Specification(s): volumetric_eigenstrain_density_check
Design: Compute Crystal Plasticity Volumetric Eigenstrain
Issue(s): #25932
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.41.11The system shall not attempt to calculate the volumetric eigenstrain from a negative average radius value.
Specification(s): volumetric_eigenstrain_radius_check
Design: Compute Crystal Plasticity Volumetric Eigenstrain
Issue(s): #25932
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: CrystalPlasticityKalidindiUpdate
8.41.6The system shall produce a positive isotropic eigenstrain in response to an increasing number density and shall demonstrate an applied shear stress on the slip systems with a z-component in response to the BCs on displacement in the z-direction.
Specification(s): volumetric_eigenstrain_increase
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.9The system shall produce an isotropic eigenstrain in response to parabolic evolution of both the void number density and average radius, and shall induce plastic deformation in the crystal plasticity reponse through the state dependance of the deformation gradient that final strain state of the FCC crystal is not zero.
Specification(s): volumetric_eigenstrain_parabolic
Design: Compute Crystal Plasticity Volumetric Eigenstrain Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #25932
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.32The system shall provide a StressUpdate material-based extensible crystal plasticity system
Specification(s): update_model_test
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.33The system shall provide a StressUpdate material-based extensible crystal plasticity framework that shall continue the state-dependent calculation upon restart
Specification(s): update_model_test_restart
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.34The material-based crystal plasticity model shall compute the lagrangian stress, PK2 stress, and slip for an orientation not aligned with the Cartesian coordinate system.
Specification(s): update_model_011orientation
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.35A constitutive failure shall trigger an exception leading to a cut time step rather than a failed solve using the stress-update based crystal plasticity implementation
Specification(s): exception
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.36The crystal plasticity system shall provide a substepping capability for improved convergence using the stress-update based crystal plasticity implementation
Specification(s): substep
Design: Compute Multiple Crystal Plasticity Stress CrystalPlasticityKalidindiUpdate
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.37The crystal plasticity system shall implement a line search capability for accelerated internal Newton solves using the stress-update based crystal plasticity implementation
Specification(s): linesearch
Design: CrystalPlasticityKalidindiUpdate
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.51
When combined with a dislocation slip constitutive model in a simulation of an FCC material, the Kalidindi (2001) twin propagation model shall:
1. compute plastic shear due to both slip and twin propagation when loaded under tension in a 111 orientation.
2. compute a near-zero twin volume fraction when loaded under compression in a 111 orientation.
3. compute a near-zero volume fraction of twins for all twin system when a 100 oriented crystal is loaded under tension.
4. compute both dislocation glide and twin propagation in a 100 oriented crystal loaded under compression.
Specification(s): combined_twinning_slip_models/combined_twinning_slip_111tension, combined_twinning_slip_models/combined_twinning_slip_111compression, combined_twinning_slip_models/combined_twinning_slip_100tension, combined_twinning_slip_models/combined_twinning_slip_100compression
Design: CrystalPlasticityTwinningKalidindiUpdate CrystalPlasticityKalidindiUpdate
Issue(s): #18846
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.52
Upon simulation restart, the crystal plasticity capability shall:
1. continue to compute the plastic shear due to twinning after a simulation restart.
2. continue to calculate plastic shear due to both dislocation slip and twinning when loaded under tension in a 111 orientation in a simulation restart.
Specification(s): restart_capabilities/only_twinning_fcc_restart, restart_capabilities/combined_twinning_slip_111tension_restart
Design: CrystalPlasticityTwinningKalidindiUpdate CrystalPlasticityKalidindiUpdate Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Elasticity Tensor CP
8.41.12The crystal plasticity models should be able to utilize Euler angle values supplied through AuxVariables.
Specification(s): euler_angle_auxvar
Design: Compute Elasticity Tensor CP
Issue(s): #19497
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.13An error will be thrown when trying to set Euler angles information from a text file and AuxVariables at the same time.
Specification(s): euler_angle_auxvar_conflict
Design: Compute Elasticity Tensor CP
Issue(s): #19497
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.41.14An error will be thrown when trying to set Euler angles information with less than three components.
Specification(s): euler_angle_components
Design: Compute Elasticity Tensor CP
Issue(s): #19497
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.41.38The crystal plasticity rotations shall correctly rotate the elasticity tensors at each material point using the stress-update based crystal plasticity implementation
Specification(s): orthotropic_rotation_Cijkl
Design: Compute Elasticity Tensor CP
Issue(s): #10629
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.46The system shall produce the initial Euler angles phi1=0, psi=54.7356103, and phi2=45 when supplied with the associated rotation matrix and shall calculate a relatively higher 2nd Piola Kirchoff stress in agreement with the low Schmid factor for this loading orientation.
Specification(s): rotation_matrix_update_euler_angle_111_orientation
Design: Compute Elasticity Tensor CP Compute Updated Euler Angle
Issue(s): #23451
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.47The system shall produce the initial Euler angles of phi1=45, psi=90, and phi2=45, which shall quickly update as the crystal rotates, when supplied with the associated rotation matrix. The system shall calculate a relatively low 2nd Piola Kirchoff stress in the z-direction in agreement with the high Schmid factor for this loading orientation
Specification(s): rotation_matrix_update_euler_angle_011_orientation
Design: Compute Elasticity Tensor CP Compute Updated Euler Angle
Issue(s): #23451
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.48The system shall produce the initial Euler angles of phi1=90, psi=30, and phi2=35, when supplied with the associated rotation matrix, and the updated Euler angles values as the crystal under goes rotation during deformation.
Specification(s): rotation_matrix_update_euler_angle_112_orientation
Design: Compute Elasticity Tensor CP Compute Updated Euler Angle
Issue(s): #23451
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.49The system shall not allow specification of both the rotation matrix and the Bunge Euler angles within the same input file.
Specification(s): rotation_matrix_and_euler_angles_error
Design: Compute Elasticity Tensor CP
Issue(s): #23451
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.41.61The crystal plasticity rotations shall correctly rotate the elasticity tensors at each material point
Specification(s): orthotropic_rotation_Cijkl
Design: Compute Elasticity Tensor CP
Issue(s): #10629
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: CrystalPlasticityTwinningKalidindiUpdate
8.41.18
The crystal plasticity HCP system shall:
1. calculate the Schmid tensor for a set of HCP twin systems given in Miller-Bravais indices and shall calculate a twin volume fraction when using the FCC Kalidindi twinning model with a modified input file.
2. compute a plastic velocity gradient that accounts for deformation contributions from both slip and twinning in an HCP crystal.
Specification(s): coupling_demonstration/modified_kalidindi_for_hcp, coupling_demonstration/demonstration_combined_hcp_slip_twins
Design: Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update CrystalPlasticityTwinningKalidindiUpdate
Issue(s): #18846
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.19The crystal plasticity system shall compute the plastic velocity gradient from both slip and twinning in anHCP crystal upon simulation restart.
Specification(s): demonstration_combined_hcp_slip_twins_restart
Design: Compute Multiple Crystal Plasticity Stress Crystal Plasticity HCP Dislocation Slip Beyerlein Update CrystalPlasticityTwinningKalidindiUpdate
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.50
The crystal plasticity model for twin propagation in FCC materials, using the Kalidindi (2001) constiutive model, shall:
1. compute the plastic shear due to twinning as a function of the applied shear stress and resistance to twin propagation, the corresponding twin volume fraction per twin system, and the total value of the twin volume fraction across all twin systems.
2. compute a non-zero twin volume fraction, and associate plastic shear increment, for only postive applied shear stress values.
3. calculate the coplanar twin propogation resistance contribution as a function of the twin volume fractions on coplanar systems alone.
4. calculate the contribution to twin propagation resistance from non-coplanar systems as a function of only the twin volume fraction on non-coplanar twin systems.
5. set the plastic shear increments due to twinning to zero once the total twin volume fraction limit is reached.
6. prevent the accumulation of a total twin volume fraction above the user-defined limit.
7. prevent the calculation of a plastic shear increment in excess of the user-defined tolerance value.
Specification(s): constiutive_model/only_twinning_fcc, constiutive_model/check_direction_twin_propagation, constiutive_model/coplanar_twin_hardening, constiutive_model/non_coplanar_twin_hardening, constiutive_model/upper_twin_fraction_limit, constiutive_model/upper_twin_fraction_limit_error, constiutive_model/strain_increment_upper_limit
Design: CrystalPlasticityTwinningKalidindiUpdate
Issue(s): #18846
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunExceptionCSVDiff
8.41.51
When combined with a dislocation slip constitutive model in a simulation of an FCC material, the Kalidindi (2001) twin propagation model shall:
1. compute plastic shear due to both slip and twin propagation when loaded under tension in a 111 orientation.
2. compute a near-zero twin volume fraction when loaded under compression in a 111 orientation.
3. compute a near-zero volume fraction of twins for all twin system when a 100 oriented crystal is loaded under tension.
4. compute both dislocation glide and twin propagation in a 100 oriented crystal loaded under compression.
Specification(s): combined_twinning_slip_models/combined_twinning_slip_111tension, combined_twinning_slip_models/combined_twinning_slip_111compression, combined_twinning_slip_models/combined_twinning_slip_100tension, combined_twinning_slip_models/combined_twinning_slip_100compression
Design: CrystalPlasticityTwinningKalidindiUpdate CrystalPlasticityKalidindiUpdate
Issue(s): #18846
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.52
Upon simulation restart, the crystal plasticity capability shall:
1. continue to compute the plastic shear due to twinning after a simulation restart.
2. continue to calculate plastic shear due to both dislocation slip and twinning when loaded under tension in a 111 orientation in a simulation restart.
Specification(s): restart_capabilities/only_twinning_fcc_restart, restart_capabilities/combined_twinning_slip_111tension_restart
Design: CrystalPlasticityTwinningKalidindiUpdate CrystalPlasticityKalidindiUpdate Compute Multiple Crystal Plasticity Stress
Issue(s): #26458
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Finite Strain Crystal Plasticity Slip Rate Residual
8.41.20The system shall compute the stress and strain response of a single crystal using the Kalidindi constitutive equation for hardening as a function of slip rate on each slip system.
Specification(s): test_one_elem
Design: Finite Strain Crystal Plasticity Slip Rate Residual
Issue(s): #5683 #6973
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.21The system shall compute the stress and strain response of a single crystal using the Kalidindi constitutive equation for hardening as a function of slip rate on each slip system with the substepping capability that reduces the intermediate time step size to aid with convergence within the crystal plasticity hardening model.
Specification(s): test_substep
Design: Finite Strain Crystal Plasticity Slip Rate Residual
Issue(s): #5082 #5683
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.22The system shall compute the stress and strain response of a single crystal using the Kalidindi constitutive equation for hardening as a function of slip rate on each slip system with the bisection line search method within the crystal plasticity hardening model to aid with convergence.
Specification(s): test_with_linesearch
Design: Finite Strain Crystal Plasticity Slip Rate Residual
Issue(s): #5683 #6973
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Solid Mechanics Module
8.41.23This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.24This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test_fileread
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.25This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test_user_object
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.26This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test_save_euler
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.27This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test_read_slip_prop
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.28This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test_cutback
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.29This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test_substep
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.30This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): test_linesearch
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.31This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.
Specification(s): orthotropic_rotation
Design: Solid Mechanics Module
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Introduction
8.41.39The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in the stress-update based crystal plasticity implementation
Specification(s): patch_recovery
Design: Introduction
Issue(s): #18721
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.63The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in a crystal plasticity finite strain application.
Specification(s): patch_recovery
Design: Introduction
Issue(s): #18721
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.85.1The SolidMechanics module shall be able to construct nodal variables from material properties that are defined at quadrature points.
Specification(s): nodal_patch_recovery
Design: Introduction
Issue(s): #15748 #12036
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.105.1The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in a small strain application.
Specification(s): patch_small_strain
Design: Introduction
Issue(s): #11880
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.105.2The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in a finite strain application.
Specification(s): patch_finite_strain
Design: Introduction
Issue(s): #18721
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.105.3In areas of high concentration gradients, the Zienkiewicz-Zhu implementation shall recover the specified material property.
Specification(s): stress_concentration
Design: Introduction
Issue(s): #11880
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Updated Euler Angle
8.41.41The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (111).
Specification(s): update_euler_angle_111_orientation
Design: Compute Updated Euler Angle Compute Multiple Crystal Plasticity Stress
Issue(s): #19473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.42The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (112).
Specification(s): update_euler_angle_112_orientation
Design: Compute Updated Euler Angle Compute Multiple Crystal Plasticity Stress
Issue(s): #19473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.43The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (123).
Specification(s): update_euler_angle_123_orientation
Design: Compute Updated Euler Angle Compute Multiple Crystal Plasticity Stress
Issue(s): #19473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.46The system shall produce the initial Euler angles phi1=0, psi=54.7356103, and phi2=45 when supplied with the associated rotation matrix and shall calculate a relatively higher 2nd Piola Kirchoff stress in agreement with the low Schmid factor for this loading orientation.
Specification(s): rotation_matrix_update_euler_angle_111_orientation
Design: Compute Elasticity Tensor CP Compute Updated Euler Angle
Issue(s): #23451
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.47The system shall produce the initial Euler angles of phi1=45, psi=90, and phi2=45, which shall quickly update as the crystal rotates, when supplied with the associated rotation matrix. The system shall calculate a relatively low 2nd Piola Kirchoff stress in the z-direction in agreement with the high Schmid factor for this loading orientation
Specification(s): rotation_matrix_update_euler_angle_011_orientation
Design: Compute Elasticity Tensor CP Compute Updated Euler Angle
Issue(s): #23451
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.48The system shall produce the initial Euler angles of phi1=90, psi=30, and phi2=35, when supplied with the associated rotation matrix, and the updated Euler angles values as the crystal under goes rotation during deformation.
Specification(s): rotation_matrix_update_euler_angle_112_orientation
Design: Compute Elasticity Tensor CP Compute Updated Euler Angle
Issue(s): #23451
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: UserObject based Crystal Plasticity System
8.41.53The system shall provide a plug-in based extensible crystal plasticity system
Specification(s): test
Design: UserObject based Crystal Plasticity System
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.54The material-based crystal plasticity model shall compute the lagrangian stress, PK2 stress, and slip for an orientation not aligned with the Cartesian coordinate system.
Specification(s): user_object_011orientation
Design: UserObject based Crystal Plasticity System
Issue(s): #16064
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.41.55A constitutive failure shall trigger an exception leading to a cut time step rather than a failed solve
Specification(s): exception
Design: UserObject based Crystal Plasticity System
Issue(s): #10133
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.56The crystal plasticity system shall provide a function to read slip system parameters from files
Specification(s): fileread
Design: UserObject based Crystal Plasticity System
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.57The crystal plasticity system shall use pluggable user objects to dtermine the plasticity state variable evolution
Specification(s): user_object
Design: UserObject based Crystal Plasticity System
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.58The crystal plasticity system shall make local Euler angles at material points available for output
Specification(s): save_euler
Design: UserObject based Crystal Plasticity System
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.59The crystal plasticity system shall provide a substepping capability for improved convergence
Specification(s): substep
Design: UserObject based Crystal Plasticity System
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.60The crystal plasticity system shall implement a line search capability for accellerated internal Newton solves
Specification(s): linesearch
Design: UserObject based Crystal Plasticity System
Issue(s): #6097
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.41.65The system shall apply correct boundary condition after timestep being cut during substepping
Specification(s): use_substep_dt
Design: UserObject based Crystal Plasticity System
Issue(s): #17340
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Crystal Plasticity State Var Rate Component Voce
8.41.62The crystal plasticity system shall provide a plugin user object implementing the Voce hardening law
Specification(s): user_object_Voce_BCC
Design: Crystal Plasticity State Var Rate Component Voce
Issue(s): #11307
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: PropertyReadFile
8.41.64The system shall provide an object to read values from a file and map them onto a mesh besed on mesh block IDs
Specification(s): prop_block_read
Design: PropertyReadFile
Issue(s): #4066
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.48.1The system shall provide an object to read values from a file and map them onto a mesh based on mesh element IDs
Specification(s): test_elem
Design: PropertyReadFile
Issue(s): #4066
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.48.2The system shall provide an object to read values from a file and map them onto a mesh based on grain IDs determined by a random Voronoi tessellation
Specification(s): test_grain
Design: PropertyReadFile
Issue(s): #4066
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: DomainIntegral System
8.42.1The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D.
Specification(s): test_jthermal
Design: DomainIntegral System
Issue(s): #3807 #10232
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.42.2The domain integral action shall compute all of the fracture domain integrals including the C integral for problems in 2D.
Specification(s): c_integral_2d
Design: DomainIntegral System
Issue(s): #3807 #10232
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.42.3The domain integral action shall compute all of the fracture domain integrals including the interaction integral for problems in 2D.
Specification(s): test_iithermal
Design: DomainIntegral System
Issue(s): #7527 #9966
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.42.4The domain integral action shall compute the stress intensity factor using the interaction integral approach for a problem dominated by thermal strains using an approach that integrates eigenstrain gradients in a general manner.
Specification(s): test_iithermal_generic
Design: DomainIntegral System
Issue(s): #26452
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.42.5The interaction integral shall account for the contributions of the gradients of arbitrary eigenstrains in 2D
Specification(s): test_ii_arb_eig_grad
Design: DomainIntegral System
Issue(s): #18804
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.42.6The DomainIntegralAction shall generate an error if a user specifies the eigenstrain gradient and also request the J integral
Specification(s): test_ii_arb_eig_grad_err_jint
Design: DomainIntegral System
Issue(s): #18804
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.42.7The DomainIntegralAction shall generate an error if a user specifies the temperature and also provides the eigenstrain_gradient
Specification(s): test_ii_arb_eig_grad_err_temp
Design: DomainIntegral System
Issue(s): #18804
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.42.8The interaction integral shall account for the contributions of body forces in 2D
Specification(s): test_ii_bf
Design: DomainIntegral System
Issue(s): #18804
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.42.9The DomainIntegralAction shall generate an error if a user specifies the body force and also request the J integral
Specification(s): test_ii_bf_err_jint
Design: DomainIntegral System
Issue(s): #18804
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.42.10The domain integral action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane for 2D.
Specification(s): test_iithermal_rot
Design: DomainIntegral System
Issue(s): #7527 #9966
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.42.11The domain integral action shall compute all of the fracture domain integrals including the C(t) integral for problems in 2D.
Specification(s): interaction_integral_2d_c
Design: DomainIntegral System
Issue(s): #7527 #9966
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.42.12The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the instantaneous thermal expansion function eigenstrain.
Specification(s): test_jthermal_ctefunc
Design: DomainIntegral System
Issue(s): #3807 #10232
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.42.13The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the mean thermal expansion function eigenstrain.
Specification(s): test_jthermal_mean_ctefunc
Design: DomainIntegral System
Issue(s): #3807 #10232
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.42.14The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the instantaneous thermal expansion function eigenstrain.
Specification(s): test_jthermal_inst_ctefunc
Design: DomainIntegral System
Issue(s): #3807 #10232
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.1The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 2D.
Specification(s): ii_2d
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.2The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems for all planes in 2D.
Specification(s): ii_2d_rot
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.3The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3d evaluated as 2D.
Specification(s): ii_3d_as_2d
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.4The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D.
Specification(s): ii_3d
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.5The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D while supressing the output of q function values.
Specification(s): ii_3d_noq
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.6The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D at specified points.
Specification(s): ii_3d_points
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.7The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane in 3D.
Specification(s): ii_3d_rot
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.63.8The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 2D while outputting q vlaues.
Specification(s): ii_2d_chk_q
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.63.9The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane 2D while outputting q values.
Specification(s): ii_2d_rot_chk_q
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.63.10The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D evaluated as 2D.
Specification(s): ii_3d_as_2d_chk_q
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.63.11The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D while outputting q values.
Specification(s): ii_3d_chk_q
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.63.12The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D for specified points, while outputting q values.
Specification(s): ii_3d_points_chk_q
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.63.13The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane in 3D while outputting q values.
Specification(s): ii_3d_rot_chk_q
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.64.1The system shall compute mixed-mode fracture integrals that match values of K fields applied at the boundary of a 3D disk cut on one side by a slit
Specification(s): test
Design: DomainIntegral System
Issue(s): #3705
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.1The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D.
Specification(s): j_2d
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.2The domain integral action shall compute the fracture domain integrals including the J integral for problems in which the fracture domains of interest represent a subset of all the domains in the system.
Specification(s): j_2d_block_restrict
Design: DomainIntegral System
Issue(s): #24795
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.3The domain integral action shall error out if the blocks selected do not have the adequate material objects.
Specification(s): j_2d_block_restrict_error
Design: DomainIntegral System
Issue(s): #24795
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.69.4The domain integral action shall suppress the vector postprocessor output and stop generating a csv file for each integration ring at each time step.
Specification(s): j_2d_output_vpp
Design: DomainIntegral System
Issue(s): #25162
Collection(s): FUNCTIONAL
Type(s): CheckFiles
8.69.5The domain integral action shall suppress the vector postprocessor output while the postprocessor outputs are not affected.
Specification(s): j_2d_output_pp
Design: DomainIntegral System
Issue(s): #25162
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.6The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using small strain.
Specification(s): j_2d_small_strain
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.7The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D at specified points.
Specification(s): j_2d_points
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.8The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D given a mouth direction.
Specification(s): j_2d_mouth_dir
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.9The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the topology type q function.
Specification(s): j_2d_topo_q
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.10The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D evaluated as a 2D problem.
Specification(s): j_3d_as_2d
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.11The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D evaluated as a 2D problem using the topology type q function.
Specification(s): j_3d_as_2d_topo_q
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.12The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D.
Specification(s): j_3d
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.13The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with the q function turned off.
Specification(s): j_3d_noq
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.14The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with specified points.
Specification(s): j_3d_points
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.15The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D given a crack mouth direction.
Specification(s): j_3d_mouth_dir
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.16The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D given a crack mouth direction and end direction vector.
Specification(s): j_3d_mouth_dir_end_dir_vec
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.17The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with a topology type q function.
Specification(s): j_3d_topo_q
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.18The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D evaluated as a 2D problem using the topology type q function.
Specification(s): j_3d_as_2d_topo_q_outq
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.19The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D given a crack mouth direction.
Specification(s): j_3d_mouth_dir_outq
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.20The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D while supressing the output of the q function values.
Specification(s): j_2d_noq
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.69.21The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D while outputting the q function values.
Specification(s): j_2d_chk_q
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.69.22The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D with the topology type q function and outputting the values.
Specification(s): j_2d_topo_chk_q
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.69.23The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D while supressing the output of the q values.
Specification(s): j_3d_chk_q
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.69.24The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with the topology type q function and outputting the values.
Specification(s): j_3d_topo_chk_q
Design: DomainIntegral System
Issue(s): #2814
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.70.1The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks.
Specification(s): j_ellip
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.2The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks using the crack mouth specification.
Specification(s): J_ellip_cm
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.3The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks using the crack mouth specification computing the system Jacobian via automatic differentiation.
Specification(s): J_ellip_cm_ad
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.4The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks with crack face pressure.
Specification(s): j_ellip_cfp
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.5The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks with crack face pressure and crack mouth boundary specified.
Specification(s): J_ellip_cm_cfp
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.6The Domain Integral Action shall compute all of the fracture domain integrals including the C integral for surface breaking elliptical cracks.
Specification(s): c_int_surfbreak_ellip_crack_sym_mm
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.7The Domain Integral Action shall compute all of the fracture domain integrals including the C integral for surface breaking elliptical cracks using automatic differentiation.
Specification(s): c_int_surfbreak_ellip_crack_sym_mm_ad
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.8The Domain Integral Action shall compute stress intensity factors from the interaction integral for a crack perpendicular to a bi-material interface, treating the interface as a functionally-graded material.
Specification(s): j_int_fgm_sif
Design: DomainIntegral System
Issue(s): #23313
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.9The Domain Integral shall error out if the user input does not consistently define the required material properties to consider extra interaction integral terms for functionally graded materials.
Specification(s): j_int_fgm_sif_error
Design: DomainIntegral System
Issue(s): #2717
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.70.10The Domain Integral Action shall compute stress intensity factors from the interaction integral, with an added term stemming for spatially varying properties, that accounts for the crack perpendicularity to the property grading and yield verified results.
Specification(s): fgm_5
Design: DomainIntegral System
Issue(s): #23313
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.70.11The Domain Integral Action shall compute verified stress intensity factors from the interaction integral for axisymmetric geometries and circumferential cracks.
Specification(s): axisymmetric_solution_tran
Design: DomainIntegral System
Issue(s): #23631
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.107.1The Domain Integral Action shall compute all of the fracture domain integrals including the T stress for cracks in an infinite plate.
Specification(s): t_stress_crack_infinite_plate_2d
Design: DomainIntegral System
Issue(s): #4276
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.107.2The Domain Integral Action shall compute all of the fracture domain integrals including the T stress for an elliptical crack in 3D.
Specification(s): t_stress_ellip_crack_3d
Design: DomainIntegral System
Issue(s): #4276
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.107.3The Domain Integral Action shall compute all of the fracture domain integrals including the T stress for an elliptical crack in 3D using automatic differentiation objects.
Specification(s): ad_t_stress_ellip_crack_3d
Design: DomainIntegral System
Issue(s): #4276
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Dynamics
8.44.1The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary.
Specification(s): acceleration_bc
Design: Dynamics PresetAcceleration
Issue(s): #7642
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.2The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary when the Newmark-Beta time integrator is used to calculate the velocity and acceleration.
Specification(s): acceleration_bc_ti
Design: Dynamics PresetAcceleration
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.4The PresetDisplacement class shall accurately prescribe the displacement at the given boundary.
Specification(s): displacement_bc
Design: Dynamics PresetDisplacement
Issue(s): #7642
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.5The PresetDisplacement class shall accurately prescribe the displacement at the given boundary using the velocity and and acceleration computed using the Newmark-Beta time integrator.
Specification(s): displacement_bc_ti
Design: Dynamics PresetDisplacement
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.6The mechanics system shall accurately conduct a static analysis in a small number of time steps to equilibrate the system under gravity before starting the dynamic analysis.
Specification(s): displacement_bc_gravity
Design: Dynamics
Issue(s): #7642
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.7The mechanics system shall accurately predict the dynamic response of a linear elastic system with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): hht
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.8The mechanics system shall accurately predict the dynamic response of a linear elastic system with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when using the velocity and acceleration computed using the Newmark-Beta time integrator.
Specification(s): hht_ti
Design: Dynamics
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.9The mechanics system shall accurately predict the dynamic response of a linear elastic system with a constant Rayleigh damping.
Specification(s): newmark
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.10The mechanics system shall accurately predict the dynamic response of a linear elastic system with Rayleigh damping provided as a material property.
Specification(s): newmark_material
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.11The mechanics system shall accurately predict the dynamic response of a linear elastic system using Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): hht
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.12The mechanics system shall accurately predict the dynamic response of a linear elastic system using Hilber-Hughes-Taylor (HHT) time integration when using the dynamic tensor mechanics action.
Specification(s): hht_action
Design: Dynamics
Issue(s): #18388
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.13The mechanics system shall accurately predict the dynamic response of a linear elastic system using Newmark time integration.
Specification(s): newmark
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.14The mechanics system shall accurately predict the dynamic response of a linear elastic system using Newmark time integration and the dynamic tensor mechanics action.
Specification(s): newmark_action
Design: Dynamics
Issue(s): #18388
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.15The mechanics system shall accurately predict the dynamic response of a linear elastic system using Hilber-Hughes-Taylor (HHT) time integration when velocity and acceleration of the system are calculated using the Newmark-Beta time integrator.
Specification(s): hht_ti
Design: Dynamics
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.16The dynamic tensor mechanics action shall support automatic differentiation using the Newmark-Beta time integrator.
Specification(s): ad_newmark_action
Design: Dynamics
Issue(s): #18687
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.20The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): hht
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.21The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with no numerical or structural damping.
Specification(s): newmark
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.22The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration.
Specification(s): rayleigh_hht
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.23The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when automatic differentiation is used.
Specification(s): rayleigh_hht_ad
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.24The mechanics system shall correctly compute the Jacobian for 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when automatic differentiation is used.
Specification(s): rayleigh_hht_ad_jac
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.44.25The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when using the velocity and acceleration computed using the Newmark-Beta time integrator.
Specification(s): rayleigh_hht_ti
Design: Dynamics
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.26The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with Rayleigh damping.
Specification(s): rayleigh_newmark
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.27The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with Rayleigh damping when using the dynamic tensor mechanics parent action.
Specification(s): rayleigh_newmark_action
Design: Dynamics
Issue(s): #5559
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: PresetAcceleration
8.44.1The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary.
Specification(s): acceleration_bc
Design: Dynamics PresetAcceleration
Issue(s): #7642
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.2The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary when the Newmark-Beta time integrator is used to calculate the velocity and acceleration.
Specification(s): acceleration_bc_ti
Design: Dynamics PresetAcceleration
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: LinearNodalConstraint
8.44.3The LinearNodalConstraint class shall constrain the secondary nodes to move as a linear combination of the primary nodes.
Specification(s): linear_nodal_constraint
Design: LinearNodalConstraint
Issue(s): #5783
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: PresetDisplacement
8.44.4The PresetDisplacement class shall accurately prescribe the displacement at the given boundary.
Specification(s): displacement_bc
Design: Dynamics PresetDisplacement
Issue(s): #7642
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.5The PresetDisplacement class shall accurately prescribe the displacement at the given boundary using the velocity and and acceleration computed using the Newmark-Beta time integrator.
Specification(s): displacement_bc_ti
Design: Dynamics PresetDisplacement
Issue(s): #12185
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: DirectCentralDifference
8.44.17The solid mechanics app shall support a form of central difference time integration that uses a direct calculation of the acceleration from the residual forces to perform a solution update.
Specification(s): direct_central_difference
Design: DirectCentralDifference
Issue(s): #27833
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.18The solid mechanics app shall support a form of central difference time integration that uses a direct calculation of the acceleration from the residual forces to perform a solution update. The direct central difference method should properly use a time step averaging method to handle non-constant time steps.
Specification(s): direct_central_difference_varied_dt
Design: DirectCentralDifference
Issue(s): #27833
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.44.19The solid mechanics app shall support dirichlet boundary conditions for direct central difference time integration that correctly enforce constant and function boundary conditions
Specification(s): direct_central_difference_multiVarBC
Design: DirectCentralDifference
Issue(s): #27833
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Composite Elasticity Tensor
8.47.1The system shall provide a method for assembling an elasticity tensor from multiple tensor contributions weighted by material properties.
Specification(s): composite
Design: Composite Elasticity Tensor
Issue(s): #5850
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Elasticity Tensor
8.47.2The system shall provide a method for rotating a tensor using a rotation matrix.
Specification(s): rotation_matrix_one_rotation
Design: Compute Elasticity Tensor
Issue(s): #16340
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.47.3The system shall provide a method for rotating a tensor using a rotation matrix requiring more than one rotation.
Specification(s): rotation_matrix_two_rotations
Design: Compute Elasticity Tensor
Issue(s): #16340
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.67.4The ComputeElasticityTensor class shall correctly compute the elasticity tensor for an isotropic axisymmetric problem.
Specification(s): axisymmetric_rz
Design: Compute Elasticity Tensor
Issue(s): #4783
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ComputeMultiPlasticityStress
8.49.3The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the QuasiStatic SolidMechanics Physics.
Specification(s): fake_plastic
Design: ComputeMultiPlasticityStress Volumetric Locking Correction
Issue(s): #9212 #7555
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.49.4The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the volumetric locking correction b-bar formulation.
Specification(s): fake_plastic_Bbar
Design: ComputeMultiPlasticityStress Volumetric Locking Correction
Issue(s): #9212 #8235
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Stress Divergence
8.52.1The system shall track a changing global stress state when a model undergoes rigid body rotation
Specification(s): rotation_test
Design: Stress Divergence
Issue(s): #8422
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.52.2The system shall compute a uniform stress state given a uniform strain state with finite strains
Specification(s): patch_test
Design: Stress Divergence
Issue(s): #12584
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ReferenceResidualProblem
8.53.1The tensor mechanics action shall set up the mechanics kernels with the appropriate options to accumulate absolute values of the residual to a tag vector usable for relative convergence checks.
Specification(s): free_expansion_abs_ref
Design: Solid Mechanics QuasiStatic Physics System ReferenceResidualProblem
Issue(s): #24246
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Global Strain
8.55.1The globalstrain system shall correctly compute the volume change due to applied stress while still maintaining periodicity in 2D.
Specification(s): test
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.55.2The globalstrain system shall correctly compute the volume change under uniaxial stress while still maintaining periodicity in all the directions in 3D.
Specification(s): uniaxial
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.55.3The globalstrain system shall correctly compute the volume change under hydrostratic stress while still maintaining periodicity in all the directions in 3D.
Specification(s): hydrostat
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.55.4The globalstrain system shall correctly compute the shear deformation due to applied stress while still maintaining periodicity in all the directions in 3D.
Specification(s): shear
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.55.5The globalstrain system shall correctly compute the deformation behavior in 2D with applied displacement boundary condition in one direction while still maintaining periodicity in the other.
Specification(s): direction
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.55.6The globalstrain system shall correctly compute the deformation behavior in 3D with applied displacement boundary condition in one direction while still maintaining periodicity in the others.
Specification(s): disp
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.55.7The globalstrain system shall correctly compute the deformation behavior in 3D with pressure boundary condition in one direction while still maintaining periodicity in the others.
Specification(s): pressure_3D
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.55.8The 'GlobalStrainAction' should set all the objects reqiured for the globalstrain system to correctly compute the deformation behavior maintaining strain periodicity.
Specification(s): action_check
Design: Global Strain
Issue(s): #11314
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Gravity
8.56.1The tensor mechanics module shall have the capability of applying a body force term in the stress divergence equilibrium equation that accounts for the force of gravity on a solid object due to its own weight.
Specification(s): gravity_test
Design: Gravity
Issue(s): #4781
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ADGravity
8.56.2The tensor mechanics module shall be able to reproduce gravity test results of the hand-coded jacobian using automatic differentiation.
Specification(s): ad_gravity_test
Design: ADGravity
Issue(s): #13100
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.56.3The Jacobian for the AD gravity problem shall be perfect
Specification(s): ad_gravity_test-jac
Design: ADGravity
Issue(s): #13100
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: MaterialVectorBodyForce
8.56.4The system shall provide a way to apply a vector valued body force density to a volume
Specification(s): material_vector_body_force
Design: MaterialVectorBodyForce
Issue(s): #13100
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: KineticEnergyAux
8.56.5The system shall provide a way to compute the system total kinetic energy through the use of auxiliary kernels and postprocessors. This test verifies that a body falls at the right acceleration under the action of gravity and that the computed kinetic energy matches the analytical expression.
Specification(s): block-gravity-kinetic-energy
Design: KineticEnergyAux
Issue(s): #19671
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: AsymptoticExpansionHomogenizationKernel
8.57.1The system shall compute homogenized elastic constants using the asymptotic expansion homogenization approach and match values for the so-called long fiber problem
Specification(s): longFiber
Design: AsymptoticExpansionHomogenizationKernel
Issue(s): #6750
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.57.2The system shall compute homogenized elastic constants using the asymptotic expansion homogenization approach and match values for the so-called short fiber problem
Specification(s): shortFiber
Design: AsymptoticExpansionHomogenizationKernel
Issue(s): #6750
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Volume Weighted Weibull
8.59.1VolumeWeightedWeibull shall generate a randomly distributed field that approximates the analytic expression for the Weibull distribution when the mesh is uniform and the reference volume is set equal to the element size
Specification(s): test
Design: Volume Weighted Weibull
Issue(s): #10221
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.59.2VolumeWeightedWeibull shall generate a randomly distributed field that approaches the analytic expression for the Weibull distribution when the mesh is uniform and the reference volume is set equal to the element size as the mesh density is increased
Specification(s): test_finer
Design: Volume Weighted Weibull
Issue(s): #10221
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.59.3VolumeWeightedWeibull shall generate a randomly distributed field that approximates the analytic expression for the Weibull distribution when the mesh is uniform, the reference volume is set to a value different from the element size, and the median is adjusted to account for the different reference volume
Specification(s): test_ref_vol
Design: Volume Weighted Weibull
Issue(s): #10221
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: PenaltyInclinedNoDisplacementBC
8.60.1The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 2D model using a penalty method.
Specification(s): 2D
Design: PenaltyInclinedNoDisplacementBC InclinedNoDisplacementBC Action
Issue(s): #13128
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.60.2The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 3D model using a penalty method.
Specification(s): 3D
Design: PenaltyInclinedNoDisplacementBC InclinedNoDisplacementBC Action
Issue(s): #13128
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.60.3The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions while using automatic differentiation.
Specification(s): ad
Design: PenaltyInclinedNoDisplacementBC InclinedNoDisplacementBC Action
Issue(s): #24910
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: InclinedNoDisplacementBC Action
8.60.1The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 2D model using a penalty method.
Specification(s): 2D
Design: PenaltyInclinedNoDisplacementBC InclinedNoDisplacementBC Action
Issue(s): #13128
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.60.2The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 3D model using a penalty method.
Specification(s): 3D
Design: PenaltyInclinedNoDisplacementBC InclinedNoDisplacementBC Action
Issue(s): #13128
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.60.3The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions while using automatic differentiation.
Specification(s): ad
Design: PenaltyInclinedNoDisplacementBC InclinedNoDisplacementBC Action
Issue(s): #24910
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Inertial Torque
8.61.1The tensor mechanics module computes residual for a simplesituation correctly
Specification(s): residual
Design: Inertial Torque
Issue(s): #13634
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.61.2The tensor mechanics module computes the ith component ofinertial torque where the only degree of freedom in y
Specification(s): simple
Design: Inertial Torque
Issue(s): #13634
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeEigenstrainFromInitialStress
8.62.1SolidMechanics shall allow users to specify initial stresses, but shall error-out with appropriate message if the user does not supply the correct number of functions to define the initial stress tensor
Specification(s): except01
Design: ComputeEigenstrainFromInitialStress
Issue(s): #9749
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.62.2SolidMechanics shall allow users to specify initial stresses, but shall error-out with appropriate message if the user does not supply the correct number of AuxVariables to define the initial stress tensor
Specification(s): except02
Design: ComputeEigenstrainFromInitialStress
Issue(s): #13087
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.62.3SolidMechanics shall allow users to specify initial stresses using Functions
Specification(s): gravity
Design: ComputeEigenstrainFromInitialStress
Issue(s): #9749
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.62.4SolidMechanics shall allow users to specify initial stresses using AuxVariables
Specification(s): gravity_with_aux
Design: ComputeEigenstrainFromInitialStress
Issue(s): #13087
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.62.5SolidMechanics shall allow users to specify initial stresses for problems with Cosserat mechanics
Specification(s): gravity_cosserat
Design: ComputeEigenstrainFromInitialStress
Issue(s): #9749
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.62.6SolidMechanics shall allow users to specify initial stresses for problems with plasticity, and if the initial stresses are inadmissible, the return-map algorithm will be applied, perhaps incrementally, to bring the initial stresses back to the admissible region
Specification(s): mc_tensile
Design: ComputeEigenstrainFromInitialStress
Issue(s): #9749
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ElementJacobianDamper
8.72.1The module shall be able to apply a damper on the displaced mesh to limit the element Jacobian change over nonlinear iterations.
Specification(s): damper_exodus
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.72.2The element Jacobian damper shall be able to apply a partial nonlinear update.
Specification(s): damper_verify
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): RunApp
8.72.3The module shall be able to apply a damper on the undisplaced mesh to limit the element Jacobian change over nonlinear iterations.
Specification(s): ref_damper
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.72.4The module shall be able to apply a damper on certain blocks of the undisplaced mesh to limit the element Jacobian change over nonlinear iterations.
Specification(s): ref_damper_block_restricted
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ReferenceElementJacobianDamper
8.72.1The module shall be able to apply a damper on the displaced mesh to limit the element Jacobian change over nonlinear iterations.
Specification(s): damper_exodus
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.72.2The element Jacobian damper shall be able to apply a partial nonlinear update.
Specification(s): damper_verify
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): RunApp
8.72.3The module shall be able to apply a damper on the undisplaced mesh to limit the element Jacobian change over nonlinear iterations.
Specification(s): ref_damper
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.72.4The module shall be able to apply a damper on certain blocks of the undisplaced mesh to limit the element Jacobian change over nonlinear iterations.
Specification(s): ref_damper_block_restricted
Design: ElementJacobianDamper ReferenceElementJacobianDamper
Issue(s): #21397
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Tensor Mechanics Master Action
8.73.1Can run second order problem without stabilization
Specification(s): without_correction
Design: Tensor Mechanics Master Action
Issue(s): #20281
Collection(s): FUNCTIONAL
Type(s): RunApp
8.73.2Cannot run second order problem with stabilization
Specification(s): with_correction
Design: Tensor Mechanics Master Action
Issue(s): #20281
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.73.3Homogenization system can be block restricted
Specification(s): homogenization_block_restriction
Design: Tensor Mechanics Master Action
Issue(s): #21716
Collection(s): FUNCTIONAL
Type(s): RunApp
8.73.4Action produces identical results for small deformations/without stabilization in axisymmetric RZ coordinates
Specification(s): action_small_unstabilized
Design: Tensor Mechanics Master Action
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.5Action produces identical results for small deformations/with stabilization in axisymmetric RZ coordinates
Specification(s): action_small_stabilized
Design: Tensor Mechanics Master Action
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.6Action produces identical results for large deformations/without stabilization in axisymmetric RZ coordinates
Specification(s): action_large_unstabilized
Design: Tensor Mechanics Master Action
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.7Action produces identical results for large deformations/with stabilization in axisymmetric RZ coordinates
Specification(s): action_large_stabilized
Design: Tensor Mechanics Master Action
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.23Action produces identical results for large deformations/with stabilization
Specification(s): action_large_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.24Action produces identical results for large deformations/no stabilization
Specification(s): action_large_no_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.25Action produces identical results for small deformations/with stabilization
Specification(s): action_small_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.26Action produces identical results for small deformations/no stabilization
Specification(s): action_small_no_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.27Action produces identical results for 1D Cartesian problem
Specification(s): action_1D
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.69Action produces identical results for a 3D, large deformation problem with mixed constraints compared to a case where the components are specified manually.
Specification(s): compare_3d
Design: Tensor Mechanics Master Action
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.70Action produces identical results for a 2D, small deformation problem with mixed constraints compared to a case where the components are specific manually.
Specification(s): compare_2d
Design: Tensor Mechanics Master Action
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.128Action produces identical results for large deformations/with stabilization
Specification(s): action_large_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.129Action produces identical results for large deformations/no stabilization
Specification(s): action_large_no_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.130Action produces identical results for small deformations/with stabilization
Specification(s): action_small_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.131Action produces identical results for small deformations/no stabilization
Specification(s): action_small_no_stab
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.132Action produces identical results for 1D Cartesian problem
Specification(s): action_1D
Design: Tensor Mechanics Master Action
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.188Action produces identical results for small deformations/without stabilization in axisymmetric RZ coordinates
Specification(s): action_small_unstabilized
Design: Tensor Mechanics Master Action
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.189Action produces identical results for large deformations/without stabilization in axisymmetric RZ coordinates
Specification(s): action_large_unstabilized
Design: Tensor Mechanics Master Action
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: TotalLagrangianStressDivergenceAxisymmetricCylindrical
8.73.8Small strain solution in 2D axisymmetric RZ coordinates matches analytical solution
Specification(s): small
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.9Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates
Specification(s): dirichlet_small_unstabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.10Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates
Specification(s): dirichlet_small_stabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.11Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates
Specification(s): dirichlet_large_unstabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.12Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates
Specification(s): dirichlet_large_stabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.13Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates
Specification(s): neumann_small_unstabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.14Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates
Specification(s): neumann_small_stabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.15Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates
Specification(s): neumann_large_unstabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.16Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates
Specification(s): neumann_large_stabilized
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.17Small strain uniaxial patch test in 2D axisymmetric RZ coordinates passes
Specification(s): small
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.18Large strain uniaxial patch test in 2D axisymmetric RZ coordinates passes
Specification(s): large
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.19Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_small_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.20Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_large_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.21Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_small_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.22Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_large_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.199Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_small_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.200Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_large_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.201Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_small_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.202Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_large_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: TotalLagrangianStressDivergenceCentrosymmetricSpherical
8.73.17Small strain uniaxial patch test in 2D axisymmetric RZ coordinates passes
Specification(s): small
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.18Large strain uniaxial patch test in 2D axisymmetric RZ coordinates passes
Specification(s): large
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.19Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_small_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.20Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_large_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.21Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_small_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.22Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_large_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.190Small strain solution in 1D centrosymmetric spherical coordinates matches analytical solution
Specification(s): small
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.191Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates
Specification(s): dirichlet_small_unstabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.192Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates
Specification(s): dirichlet_small_stabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.193Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates
Specification(s): dirichlet_large_unstabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.194Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates
Specification(s): dirichlet_large_stabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.195Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates
Specification(s): neumann_small_unstabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.196Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates
Specification(s): neumann_small_stabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.197Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates
Specification(s): neumann_large_unstabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.198Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates
Specification(s): neumann_large_stabilized
Design: TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.199Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_small_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.200Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms
Specification(s): jacobian_large_no_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.201Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_small_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.202Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms
Specification(s): jacobian_large_with_stab
Design: TotalLagrangianStressDivergenceAxisymmetricCylindrical TotalLagrangianStressDivergenceCentrosymmetricSpherical
Issue(s): #20712
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: TotalLagrangianStressDivergence
8.73.28Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.29Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs
Specification(s): neumann_small_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.30Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.31Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs
Specification(s): neumann_large_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.32Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.33Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs
Specification(s): neumann_small_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.34Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.35Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs
Specification(s): neumann_large_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.36Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.37Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs
Specification(s): neumann_small_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.38Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.39Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs
Specification(s): neumann_large_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.40Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.41Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs
Specification(s): neumann_small_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.42Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.43Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs
Specification(s): neumann_large_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.44Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.45Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs
Specification(s): neumann_small_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.46Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.47Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs
Specification(s): neumann_large_neither
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.48Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.49Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs
Specification(s): neumann_small_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.50Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.51Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs
Specification(s): neumann_large_right
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.52Quadratic convergence in 1D for DirichletBCs, SMP does better than FDP for this problem.
Specification(s): dirichlet
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.53Quadratic convergence in 1D for NeumannBCs, SMP does better than FDP for this problem.
Specification(s): neumann
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.54Quadratic convergence in 2D for DirichletBCs, SMP matches FDP.
Specification(s): dirichlet
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.55Quadratic convergence in 2D for NeumannBCs, SMP matches FDP.
Specification(s): neumann
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.56Quadratic convergence in 3D for DirichletBCs, SMP matches FDP.
Specification(s): dirichlet
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.57Quadratic convergence in 3D for NeumannBCs, SMP matches FDP.
Specification(s): neumann
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.58Quadratic convergence in 3D for PresetBCs on a complicated geometry, SMP matches FDP.
Specification(s): L-large
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.59Quadratic convergence in 3D for PresetBCs on a complicated geometry, SMP matches FDP.
Specification(s): L-small
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.98Small strain uniaxial patch test passes
Specification(s): small
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.99Large strain uniaxial patch test passes
Specification(s): large
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.100The new system shall produce the correct results if residual and jacobian are computed together.
Specification(s): residual_jacobian_together
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.119System still functions if you supply a base_name
Specification(s): base_name
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.120Stabilized solution matches Cook's solution for stabilized Q4 elements.
Specification(s): cook_small_updated
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.121Stabilized solution matches Cook's solution for stabilized Q4 elements.
Specification(s): cook_large_updated
Design: TotalLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeLagrangianWrappedStress
8.73.60Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an elastic material
Specification(s): elastic_small_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.61Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an elastic material
Specification(s): elastic_large_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.62Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an elastic material
Specification(s): elastic_small_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.63Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an elastic material
Specification(s): elastic_large_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.64Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an plastic_j2 material
Specification(s): plastic_j2_small_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.65Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an plastic_j2 material
Specification(s): plastic_j2_large_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.66Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an plastic_j2 material
Specification(s): plastic_j2_small_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.67Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an plastic_j2 material
Specification(s): plastic_j2_large_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.68Resulting flow curve matches analytic calculation
Specification(s): flow_curve
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.165Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an elastic material
Specification(s): elastic_small_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.166Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an elastic material
Specification(s): elastic_large_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.167Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an elastic material
Specification(s): elastic_small_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.168Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an elastic material
Specification(s): elastic_large_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.169Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an plastic_j2 material
Specification(s): plastic_j2_small_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.170Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an plastic_j2 material
Specification(s): plastic_j2_large_neither
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.171Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an plastic_j2 material
Specification(s): plastic_j2_small_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.172Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an plastic_j2 material
Specification(s): plastic_j2_large_right
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.173Resulting flow curve matches analytic calculation
Specification(s): flow_curve
Design: ComputeLagrangianWrappedStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.222The Lagrangian kernels can use a small strain elastic update with a large kinematics formulation
Specification(s): runs_with_small_strain_model
Design: ComputeLagrangianWrappedStress
Issue(s): #21720
Collection(s): FUNCTIONAL
Type(s): RunApp

solid_mechanics: HomogenizationConstraintScalarKernel
8.73.71Jacobian is exact with rtol 1e-7 for small deformations, imposed strains, and no stabilization
Specification(s): sd-strain_no_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.72Jacobian is exact with rtol 1e-7 for small deformations, imposed stresses, and no stabilization
Specification(s): sd-stress_no_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.73Jacobian is exact with rtol 1e-7 for large deformations, imposed strains, and no stabilization
Specification(s): ld-strain_no_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.74Jacobian is exact with rtol 1e-7 for large deformations, imposed stresses, and no stabilization
Specification(s): ld-stress_no_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.75Jacobian is exact with rtol 1e-7 for small deformations, imposed strains, and stabilization on
Specification(s): sd-strain_right_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.76Jacobian is exact with rtol 1e-7 for small deformations, imposed stresses, and stabilization on
Specification(s): sd-stress_right_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.77Jacobian is exact with rtol 1e-6 for large deformations, imposed strains, and stabilization on
Specification(s): ld-strain_right_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.78Jacobian is exact with rtol 1e-7 for large deformations, imposed stresses, and stabilization on
Specification(s): ld-stress_right_stab
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.79Homogenized strain field hits the targets in 1D using large kinematics
Specification(s): 1d-strain
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.80Homogenized stress field hits the targets in 1D using large kinematics
Specification(s): 1d-stress
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.81Homogenization with strain constraints hits the targets in 2D using large kinematics
Specification(s): 2d-strain
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.82Homogenization with stress constraints hits the targets in 2D using large kinematics
Specification(s): 2d-stress
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.83Homogenization with strain constraints hits the targets in 3D using large kinematics
Specification(s): 3d-strain
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.84Homogenization with stress constraints hits the targets in 3D using large kinematics
Specification(s): 3d-stress
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.90Homogenized strain field hits the targets in 1D
Specification(s): 1d-strain
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.91Homogenized stress field hits the targets in 1D
Specification(s): 1d-stress
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.92Homogenization with strain constraints hits the targets in 2D
Specification(s): 2d-strain
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.93Homogenization with stress constraints hits the targets in 2D
Specification(s): 2d-stress
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.94Homogenization with mixed stress and strain constraints hits the targets in 2D
Specification(s): 2d-mixed
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.95Homogenization with strain constraints hits the targets in 3D
Specification(s): 3d-strain
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.96Homogenization with stress constraints hits the targets in 3D
Specification(s): 3d-stress
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.97Homogenization with mixed stress and strain constraints hits the targets in 3D
Specification(s): 3d-mixed
Design: HomogenizationConstraintScalarKernel
Issue(s): #17473
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ScalarLMKernel
8.73.85Homogenization from scalar wrapper class with strain constraints hits the targets in 2D
Specification(s): 2d-strainS
Design: ScalarLMKernel
Issue(s): #22174
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.86Homogenization from scalar wrapper class with stress constraints hits the targets in 2D
Specification(s): 2d-stressS
Design: ScalarLMKernel
Issue(s): #22174
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.87Homogenization from scalar wrapper class with mixed stress and strain constraints hits the targets in 2D
Specification(s): 2d-mixedS
Design: ScalarLMKernel
Issue(s): #22174
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.88Framework scalar kernel wrapper correctly assembles scalar-to-scalar coupling Jacobian
Specification(s): 2d-stressA
Design: ScalarLMKernel
Issue(s): #22174
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.89Framework scalar kernel wrapper correctly assembles Jacobian by rows
Specification(s): 2d-stressR
Design: ScalarLMKernel
Issue(s): #22174
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: TotalLagrangianWeakPlaneStress
8.73.1012D generalized plane strain solution shall match the 3D results in the limit of infinite thickness.
Specification(s): 2D
Design: TotalLagrangianWeakPlaneStress
Issue(s): #21757
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.102Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for small displacements without stabilization.
Specification(s): jacobian_small_unstabilized
Design: TotalLagrangianWeakPlaneStress
Issue(s): #21757
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.103Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for small displacements with stabilization.
Specification(s): jacobian_small_stabilized
Design: TotalLagrangianWeakPlaneStress
Issue(s): #21757
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.104Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for large displacements without stabilization.
Specification(s): jacobian_large_unstabilized
Design: TotalLagrangianWeakPlaneStress
Issue(s): #21757
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.105Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for large displacements with stabilization.
Specification(s): jacobian_large_stabilized
Design: TotalLagrangianWeakPlaneStress
Issue(s): #21757
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.106
Using weak plane stress,
1. the 2D weak plane stress result should match
2. the 3D result where the out-of-plane stress is zero.
Specification(s): correctness/2D, correctness/3D
Design: TotalLagrangianWeakPlaneStress
Issue(s): #21757
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeLagrangianObjectiveStress
8.73.107Classical Truesdell response to pure shear matches known solution
Specification(s): truesdell_shear
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.108Classical Jaumann response to pure shear matches known solution
Specification(s): jaumann_shear
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.109Classical Green-Naghdi response to pure shear matches known solution
Specification(s): green_naghdi_shear
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.110Classical Truesdell response to pure rotation matches known solution
Specification(s): truesdell_rotation
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.111Classical Jaumann response to pure rotation matches known solution
Specification(s): jaumann_rotation
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.112Classical Green-Naghdi response to pure rotation matches known solution
Specification(s): green_naghdi_rotation
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.113Treusdell tangent is exact within rtol of 1e-7
Specification(s): truesdell_jacobian
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.114Jaumann tangent is exact within rtol of 1e-7
Specification(s): jaumann_jacobian
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.115Green-Naghdi tangent is exact within rtol of 1e-7
Specification(s): green_naghdi_jacobian
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.116Stresses are being computed on the deformed volume
Specification(s): area_change
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.117Stress state correctly rotates from step 10 to the final step
Specification(s): rotate_stresses
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.118Classical demonstration that the shear stress/strain response remains linear for a Truesdell rate.
Specification(s): truesdell
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.176Stresses are being computed on the deformed volume
Specification(s): area_change
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.177Stress state correctly rotates from step 10 to the final step
Specification(s): rotate_stresses
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.178Classical demonstration that the shear stress/strain response remains linear for a Truesdell rate.
Specification(s): truesdell
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.179System still functions correctly if you supply a base_name
Specification(s): base_name
Design: ComputeLagrangianObjectiveStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: UpdatedLagrangianStressDivergence
8.73.122Strains are as-expected (0.1 total, 0 mechanical) for a free expansion
Specification(s): free
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.123Stresses and strain as expected for thermal expansion constrained in one direction
Specification(s): constrained
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.124Jacobian is exact with relative tolerance of 1e-7 for small displacements, no stabilization, including cross-terms
Specification(s): jacobian_small_no_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.125Jacobian is exact with relative tolerance of 1e-7 for large displacements, no stabilization, including cross-terms
Specification(s): jacobian_large_no_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.126Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, including cross-terms
Specification(s): jacobian_small_with_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.127Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, including cross-terms
Specification(s): jacobian_large_with_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.133Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.134Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs
Specification(s): neumann_small_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.135Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.136Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs
Specification(s): neumann_large_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.137Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.138Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs
Specification(s): neumann_small_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.139Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.140Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs
Specification(s): neumann_large_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.141Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.142Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs
Specification(s): neumann_small_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.143Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.144Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs
Specification(s): neumann_large_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.145Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.146Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs
Specification(s): neumann_small_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.147Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.148Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs
Specification(s): neumann_large_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.149Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.150Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs
Specification(s): neumann_small_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.151Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.152Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs
Specification(s): neumann_large_neither
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.153Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_small_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.154Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs
Specification(s): neumann_small_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.155Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs
Specification(s): dirichlet_large_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.156Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs
Specification(s): neumann_large_right
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.157Quadratic convergence in 1D for DirichletBCs, SMP does better than FDP for this problem.
Specification(s): dirichlet
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.158Quadratic convergence in 1D for NeumannBCs, SMP does better than FDP for this problem.
Specification(s): neumann
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.159Quadratic convergence in 2D for DirichletBCs, SMP matches FDP.
Specification(s): dirichlet
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.160Quadratic convergence in 2D for NeumannBCs, SMP matches FDP.
Specification(s): neumann
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.161Quadratic convergence in 3D for DirichletBCs, SMP matches FDP.
Specification(s): dirichlet
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.162Quadratic convergence in 3D for NeumannBCs, SMP matches FDP.
Specification(s): neumann
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.163The system shall achieve quadratic convergence in 3D with preset Dirichlet displacement boundary conditions on a complicated geometry for small deformation, and the preconditioning for a single matrix shall match finite-difference preconditioning results.
Specification(s): L-large
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.164The system shall achieve quadratic convergence in 3D with preset Dirichlet displacement boundary conditions for large deformation, and the preconditioning for a single matrix shall match finite-difference preconditioning results.
Specification(s): L-small
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.174Small strain uniaxial patch test passes
Specification(s): small
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.175Large strain uniaxial patch test passes
Specification(s): large
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.182Strains are as-expected (0.1 total, 0 mechanical) for a free expansion
Specification(s): free
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.183Stresses and strain as expected for thermal expansion constrained in one direction
Specification(s): constrained
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.73.184Jacobian is exact with relative tolerance of 1e-7 for small displacements, no stabilization, including cross-terms
Specification(s): jacobian_small_no_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.185Jacobian is exact with relative tolerance of 1e-7 for large displacements, no stabilization, including cross-terms
Specification(s): jacobian_large_no_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.186Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, including cross-terms
Specification(s): jacobian_small_with_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.187Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, including cross-terms
Specification(s): jacobian_large_with_stab
Design: UpdatedLagrangianStressDivergence
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: ComputeLagrangianStrain
8.73.180Stabilized solution matches Cook's solution for stabilized Q4 elements for small deformations.
Specification(s): cook_small_total
Design: ComputeLagrangianStrain
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.181Stabilized solution matches Cook's solution for stabilized Q4 elements for large deformations.
Specification(s): cook_large_total
Design: ComputeLagrangianStrain
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeStVenantKirchhoffStress
8.73.203Throw an error if you do not provide an isotropic tensor to ComputeStVenantKirchhoffStress
Specification(s): stvenantkirchhoff
Design: ComputeStVenantKirchhoffStress
Issue(s): #17472
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.73.206Correct Jacobian coming from the material model for nonlinear kinematics with relative error less than 1e-6
Specification(s): pk_stvenant
Design: ComputeStVenantKirchhoffStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.207Correct Jacobian coming from the material model for linear kinematics with relative error less than 1e-6
Specification(s): pk_stvenant_small
Design: ComputeStVenantKirchhoffStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.210Correct Jacobian coming from the material model for nonlinear kinematics with relative error less than 1e-6
Specification(s): hypoelastic_stvenant
Design: ComputeStVenantKirchhoffStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.211Correct Jacobian coming from the material model for linear kinematics with relative error less than 1e-6
Specification(s): hypoelastic_stvenant_small
Design: ComputeStVenantKirchhoffStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.215Stress matches exact solution (xx=1.6144e3, rest zero)
Specification(s): stvenantkirchhoff
Design: ComputeStVenantKirchhoffStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.217Stress matches exact solution
Specification(s): stvenantkirchhoff_small_deformation
Design: ComputeStVenantKirchhoffStress
Issue(s): #22588
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeLagrangianLinearElasticStress
8.73.204Correct Jacobian coming from the material model for nonlinear kinematics with relative error less than 1e-6
Specification(s): cauchy_linear
Design: ComputeLagrangianLinearElasticStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.205Correct Jacobian coming from the material model for linear kinematics with relative error less than 1e-6
Specification(s): cauchy_linear_small
Design: ComputeLagrangianLinearElasticStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.214Stress matches elastic solution (xx=1e4, rest zero)
Specification(s): cauchy-elastic
Design: ComputeLagrangianLinearElasticStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeNeoHookeanStress
8.73.208Correct Jacobian coming from the material model for nonlinear kinematics with relative error less than 1e-6
Specification(s): neohookean
Design: ComputeNeoHookeanStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.209Correct Jacobian coming from the material model for linear kinematics with relative error less than 1e-6
Specification(s): neohookean_small
Design: ComputeNeoHookeanStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.216Stress matches exact analytic solution, rest zero
Specification(s): neohookean
Design: ComputeNeoHookeanStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.218Stress matches exact analytic solution, rest zero
Specification(s): neohookean_small_deformation
Design: ComputeNeoHookeanStress
Issue(s): #22588
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeSimoHughesJ2PlasticityStress
8.73.212Correct Jacobian for elastoplasticity with linear hardening with relative error less than 1e-6
Specification(s): elastoplastic_linear_hardening
Design: ComputeSimoHughesJ2PlasticityStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.213Correct Jacobian for elastoplasticity with power-law hardening with relative error less than 1e-6
Specification(s): elastoplastic_powerlaw_hardening
Design: ComputeSimoHughesJ2PlasticityStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.73.220Stress matches exact analytic solution for elastoplasticity with linear hardening
Specification(s): elastoplastic_linear_hardening
Design: ComputeSimoHughesJ2PlasticityStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.73.221Stress matches exact analytic solution for elastoplasticity with power-law hardening
Specification(s): elastoplastic_powerlaw_hardening
Design: ComputeSimoHughesJ2PlasticityStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeHypoelasticStVenantKirchhoffStress
8.73.219The hypoelastic equivalent of the St. Venant-Kirchhoff model gives the same result as its hyperelastic counterpart.
Specification(s): stvenantkirchhoff_hypoelastic
Design: ComputeHypoelasticStVenantKirchhoffStress
Issue(s): #17472
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Line Material Rank Two Sampler
8.74.1The system shall allow sampling of material properties derived from rank two tensors along a line and output those quantities via a vectorpostprocessor.
Specification(s): rank_two_sampler
Design: Line Material Rank Two Sampler
Issue(s): #4462
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Line Material Rank Two Scalar Sampler
8.74.2The system shall allow sampling of scalar material properties along a line and output those quantities via a vectorpostprocessor.
Specification(s): rank_two_scalar_sampler
Design: Line Material Rank Two Scalar Sampler
Issue(s): #4462
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Tensor Representation and Utility Classes
8.75.1
The system shall solve the continuum mechanics equations in the small strain formulation
1. with full tensors
2. with symmetric Mandel notation tensors
Specification(s): small_strain/full_tensor_reference, small_strain/symmetric_tensor
Design: Tensor Representation and Utility Classes
Issue(s): #19000
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.75.2
The system shall solve the continuum mechanics equations in the finite strain formulation
1. with full tensors
2. with symmetric Mandel notation tensors
Specification(s): finite_strain/full_tensor_reference, finite_strain/symmetric_tensor
Design: Tensor Representation and Utility Classes
Issue(s): #19000
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Material Time Step Postprocessor
8.76.1The system shall compute a timestep size that is limited by a power law creep model and a specified maximum inelastic strain increment.
Specification(s): test5a_lim
Design: Material Time Step Postprocessor
Issue(s): #8553
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.76.2The system shall not impose a limit on the time step during the initial evaluation when the creep limiting time step option is used.
Specification(s): test5a_lim_on_initial
Design: Material Time Step Postprocessor
Issue(s): #10382
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.76.4The ScalarMaterialDamage model shall be capable of informing the material-based time step calculation based on the number of elements changing damage state in a step
Specification(s): elements_damage_limit
Design: Scalar Material Damage Material Time Step Postprocessor
Issue(s): #11662
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.76.5The MaterialTimeStepPostprocessor model shall be capable of computing a time step based on both the material time step limited by damage evoluation and the number of elements changing damage state in a step
Specification(s): mixed_timestep_limit
Design: Scalar Material Damage Material Time Step Postprocessor
Issue(s): #11662
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.76.6The MaterialTimeStepPostprocessor shall generate an error if an unknown property is requested with the 'time_step_limit' parameter
Specification(s): elements_damage_limit_unknown_prop
Design: Material Time Step Postprocessor
Issue(s): #11662
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.76.7The MaterialTimeStepPostprocessor shall generate an error if neither the material time step limit nor the elements changed limit is specified.
Specification(s): e
Design: Material Time Step Postprocessor
Issue(s): #11662
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.76.8The system to limit the analysis time step based on material behavior shall correctly function when used with an isotropic plasticity model.
Specification(s): nl1_lim
Design: Material Time Step Postprocessor
Issue(s): #8553
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.76.9The system to limit the analysis time step based on material behavior shall correctly function when used with an isotropic plasticity model when the MaterialTimeStepPostprocessor is run at initialization.
Specification(s): nl1_lim_on_initial
Design: Material Time Step Postprocessor
Issue(s): #8553
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.76.10The ComputeMultipleInelasticStress model shall compute a time step equal to the maximum real number if no inelastic model is provided
Specification(s): no_inelastic_model_limit
Design: Scalar Material Damage Material Time Step Postprocessor
Issue(s): #13250
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.76.11The system shall compute a time step equal to a user input maximum real number if no inelastic model is provided
Specification(s): no_inelastic_model_limit_defined
Design: Material Time Step Postprocessor
Issue(s): #22604
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Scalar Material Damage
8.76.3The ScalarMaterialDamage model shall be capable of informing the material-based time step calculation based on the damage evolution
Specification(s): scalar_damage_material_limit
Design: Scalar Material Damage
Issue(s): #11662
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.76.4The ScalarMaterialDamage model shall be capable of informing the material-based time step calculation based on the number of elements changing damage state in a step
Specification(s): elements_damage_limit
Design: Scalar Material Damage Material Time Step Postprocessor
Issue(s): #11662
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.76.5The MaterialTimeStepPostprocessor model shall be capable of computing a time step based on both the material time step limited by damage evoluation and the number of elements changing damage state in a step
Specification(s): mixed_timestep_limit
Design: Scalar Material Damage Material Time Step Postprocessor
Issue(s): #11662
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.76.10The ComputeMultipleInelasticStress model shall compute a time step equal to the maximum real number if no inelastic model is provided
Specification(s): no_inelastic_model_limit
Design: Scalar Material Damage Material Time Step Postprocessor
Issue(s): #13250
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.1The system shall calculate the effect of damage on the stress of a elastic material.
Specification(s): scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.2The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation.
Specification(s): ad_scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.3The system shall calculate damaged stress based on old damage index.
Specification(s): scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.4The system shall calculate damaged stress based on old damage index when using automatic differentiation.
Specification(s): ad_scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.5The system shall report an error when damage index is greater than 1.
Specification(s): scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.6The system shall report an error when damage index is greater than 1 also when using automatic differentiation.
Specification(s): ad_scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.7The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress
Specification(s): scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.8The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation
Specification(s): ad_scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.9The system shall calculate the maximum value of the damage index comparing different damage models.
Specification(s): combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.10The system shall calculate the effective damage index from different damage models.
Specification(s): combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.11The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model
Specification(s): combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.12The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models.
Specification(s): combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.13The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.14The system shall calculate the effective damage index from different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.15The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.16The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.17The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation.
Specification(s): scalar_damage_material_inelastic
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.18The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation.
Specification(s): scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.19The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation.
Specification(s): ad_scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.20The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object.
Specification(s): multiple_inelastic_bad_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #20722
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.21The system shall calculate the effect of damage on the stress of a nonlocal damage model.
Specification(s): nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.22The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation.
Specification(s): ad_nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Frequency Domain Analysis
8.79.1The module shall be able to perform modal analysis with the Eigenvalue Executioner.
Specification(s): modal
Design: Frequency Domain Analysis
Issue(s): #27295
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ADMultiplePowerLawCreepStressUpdate
8.82.1The AD multiple power law creep must reproduce the results of the AD single power law creep: Reference results.
Specification(s): powerlaw
Design: ADMultiplePowerLawCreepStressUpdate
Issue(s): #18850
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.82.2The AD multiple power law creep must reproduce the results of the AD single power law creep when a single stress increment is provided by the user.
Specification(s): multipowerlaw
Design: ADMultiplePowerLawCreepStressUpdate
Issue(s): #18850
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.82.3The AD multiple power law creep must reproduce the results of the AD single power law creep with multiple stress intervals with same power law material parameters.
Specification(s): multipowerlaw_two_intervals
Design: ADMultiplePowerLawCreepStressUpdate
Issue(s): #18850
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.82.4The AD multiple power law creep must avoid regression for a simple few-element problem whose solution has stress levels encompassing two different sets of power law parameters
Specification(s): multipowerlaw_two_intervals_no_continuity
Design: ADMultiplePowerLawCreepStressUpdate
Issue(s): #18850
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.82.5Stress thresholds must be provided in increasing order, otherwise an error will inform the user of such a requirement.
Specification(s): multipowerlaw_user_input_error
Design: ADMultiplePowerLawCreepStressUpdate
Issue(s): #18850
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: CauchyStressFromNEML2
8.84.1The system shall be capable of capturing errors occurring during the evaluation of a NEML2 model.
Specification(s): neml2_error
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): RunException
8.84.2The system shall throw an error upon instantiation of NEML2 interface objects if NEML2 is not available.
Specification(s): no_neml2
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): RunException
8.84.3
The system shall be capable of modularly interfacing with the NEML2 library to perform constitutive update
1. to solve an elasticity problem;
2. to solve a perfect viscoplasticity problem;
3. to solve a viscoplasticity problem with isotropic hardening;
4. to solve a viscoplasticity problem with kinematic hardening;
5. to solve a viscoplasticity problem with both isotropic and kinematic hardening;
6. to solve a viscoplasticity problem with non-associative Chaboche hardening;
7. to solve a viscoplasticity problem using radial return;
8. to solve a rate-independent problem with perfect plasticity;
9. to solve a rate-independent problem with isotropic hardening;
10. to solve a rate-independent problem with kinematic hardening;
11. to solve a rate-independent problem with both isotropic and kinematic hardening.
Specification(s): neml2_modular/elasticity, neml2_modular/viscoplasticity_perfect, neml2_modular/viscoplasticity_isoharden, neml2_modular/viscoplasticity_kinharden, neml2_modular/viscoplasticity_isokinharden, neml2_modular/viscoplasticity_chaboche, neml2_modular/viscoplasticity_radial_return, neml2_modular/rate_independent_plasticity_perfect, neml2_modular/rate_independent_plasticity_isoharden, neml2_modular/rate_independent_plasticity_kinharden, neml2_modular/rate_independent_plasticity_isokinharden
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #27493
Collection(s): SYSTEM
Type(s): Exodiff
8.84.4The system shall provide a modular way to transfer variables and/or real material property to NEML2 for use as model parameters.
Specification(s): moose_to_neml2_parameter
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.5The system shall error out while trying to set a parameter that does not exist.
Specification(s): moose_to_neml2_parameter_error
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.84.6The system shall provide for a modular way to compute NEML2 output with respect to specific model parameters and save that it as a MOOSE material property.
Specification(s): neml2_parameter_derivative
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.7The system shall provide for a modular way to transfer NEML2 results to material properties..
Specification(s): neml2_to_moose_material
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.8
The system shall be capable of interfacing with the NEML2 library to perform constitutive update
1. to solve an elasticity problem;
2. to solve a perfect viscoplasticity problem;
3. to solve a viscoplasticity problem with isotropic hardening;
4. to solve a viscoplasticity problem with kinematic hardening;
5. to solve a viscoplasticity problem with both isotropic and kinematic hardening;
6. to solve a viscoplasticity problem with non-associative Chaboche hardening;
7. to solve a viscoplasticity problem using radial return;
8. to solve a rate-independent problem with perfect plasticity;
9. to solve a rate-independent problem with isotropic hardening;
10. to solve a rate-independent problem with kinematic hardening;
11. to solve a rate-independent problem with both isotropic and kinematic hardening.
12. in a batched fashion.
Specification(s): neml2_legacy/elasticity, neml2_legacy/viscoplasticity_perfect, neml2_legacy/viscoplasticity_isoharden, neml2_legacy/viscoplasticity_kinharden, neml2_legacy/viscoplasticity_isokinharden, neml2_legacy/viscoplasticity_chaboche, neml2_legacy/viscoplasticity_radial_return, neml2_legacy/rate_independent_plasticity_perfect, neml2_legacy/rate_independent_plasticity_isoharden, neml2_legacy/rate_independent_plasticity_kinharden, neml2_legacy/rate_independent_plasticity_isokinharden, neml2_legacy/batched
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): Exodiff

solid_mechanics: CauchyStressFromNEML2UO
8.84.1The system shall be capable of capturing errors occurring during the evaluation of a NEML2 model.
Specification(s): neml2_error
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): RunException
8.84.2The system shall throw an error upon instantiation of NEML2 interface objects if NEML2 is not available.
Specification(s): no_neml2
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): RunException
8.84.3
The system shall be capable of modularly interfacing with the NEML2 library to perform constitutive update
1. to solve an elasticity problem;
2. to solve a perfect viscoplasticity problem;
3. to solve a viscoplasticity problem with isotropic hardening;
4. to solve a viscoplasticity problem with kinematic hardening;
5. to solve a viscoplasticity problem with both isotropic and kinematic hardening;
6. to solve a viscoplasticity problem with non-associative Chaboche hardening;
7. to solve a viscoplasticity problem using radial return;
8. to solve a rate-independent problem with perfect plasticity;
9. to solve a rate-independent problem with isotropic hardening;
10. to solve a rate-independent problem with kinematic hardening;
11. to solve a rate-independent problem with both isotropic and kinematic hardening.
Specification(s): neml2_modular/elasticity, neml2_modular/viscoplasticity_perfect, neml2_modular/viscoplasticity_isoharden, neml2_modular/viscoplasticity_kinharden, neml2_modular/viscoplasticity_isokinharden, neml2_modular/viscoplasticity_chaboche, neml2_modular/viscoplasticity_radial_return, neml2_modular/rate_independent_plasticity_perfect, neml2_modular/rate_independent_plasticity_isoharden, neml2_modular/rate_independent_plasticity_kinharden, neml2_modular/rate_independent_plasticity_isokinharden
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #27493
Collection(s): SYSTEM
Type(s): Exodiff
8.84.4The system shall provide a modular way to transfer variables and/or real material property to NEML2 for use as model parameters.
Specification(s): moose_to_neml2_parameter
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.5The system shall error out while trying to set a parameter that does not exist.
Specification(s): moose_to_neml2_parameter_error
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.84.6The system shall provide for a modular way to compute NEML2 output with respect to specific model parameters and save that it as a MOOSE material property.
Specification(s): neml2_parameter_derivative
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.7The system shall provide for a modular way to transfer NEML2 results to material properties..
Specification(s): neml2_to_moose_material
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.8
The system shall be capable of interfacing with the NEML2 library to perform constitutive update
1. to solve an elasticity problem;
2. to solve a perfect viscoplasticity problem;
3. to solve a viscoplasticity problem with isotropic hardening;
4. to solve a viscoplasticity problem with kinematic hardening;
5. to solve a viscoplasticity problem with both isotropic and kinematic hardening;
6. to solve a viscoplasticity problem with non-associative Chaboche hardening;
7. to solve a viscoplasticity problem using radial return;
8. to solve a rate-independent problem with perfect plasticity;
9. to solve a rate-independent problem with isotropic hardening;
10. to solve a rate-independent problem with kinematic hardening;
11. to solve a rate-independent problem with both isotropic and kinematic hardening.
12. in a batched fashion.
Specification(s): neml2_legacy/elasticity, neml2_legacy/viscoplasticity_perfect, neml2_legacy/viscoplasticity_isoharden, neml2_legacy/viscoplasticity_kinharden, neml2_legacy/viscoplasticity_isokinharden, neml2_legacy/viscoplasticity_chaboche, neml2_legacy/viscoplasticity_radial_return, neml2_legacy/rate_independent_plasticity_perfect, neml2_legacy/rate_independent_plasticity_isoharden, neml2_legacy/rate_independent_plasticity_kinharden, neml2_legacy/rate_independent_plasticity_isokinharden, neml2_legacy/batched
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): Exodiff

solid_mechanics: CauchyStressFromNEML2Receiver
8.84.1The system shall be capable of capturing errors occurring during the evaluation of a NEML2 model.
Specification(s): neml2_error
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): RunException
8.84.2The system shall throw an error upon instantiation of NEML2 interface objects if NEML2 is not available.
Specification(s): no_neml2
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): RunException
8.84.3
The system shall be capable of modularly interfacing with the NEML2 library to perform constitutive update
1. to solve an elasticity problem;
2. to solve a perfect viscoplasticity problem;
3. to solve a viscoplasticity problem with isotropic hardening;
4. to solve a viscoplasticity problem with kinematic hardening;
5. to solve a viscoplasticity problem with both isotropic and kinematic hardening;
6. to solve a viscoplasticity problem with non-associative Chaboche hardening;
7. to solve a viscoplasticity problem using radial return;
8. to solve a rate-independent problem with perfect plasticity;
9. to solve a rate-independent problem with isotropic hardening;
10. to solve a rate-independent problem with kinematic hardening;
11. to solve a rate-independent problem with both isotropic and kinematic hardening.
Specification(s): neml2_modular/elasticity, neml2_modular/viscoplasticity_perfect, neml2_modular/viscoplasticity_isoharden, neml2_modular/viscoplasticity_kinharden, neml2_modular/viscoplasticity_isokinharden, neml2_modular/viscoplasticity_chaboche, neml2_modular/viscoplasticity_radial_return, neml2_modular/rate_independent_plasticity_perfect, neml2_modular/rate_independent_plasticity_isoharden, neml2_modular/rate_independent_plasticity_kinharden, neml2_modular/rate_independent_plasticity_isokinharden
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #27493
Collection(s): SYSTEM
Type(s): Exodiff
8.84.4The system shall provide a modular way to transfer variables and/or real material property to NEML2 for use as model parameters.
Specification(s): moose_to_neml2_parameter
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.5The system shall error out while trying to set a parameter that does not exist.
Specification(s): moose_to_neml2_parameter_error
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.84.6The system shall provide for a modular way to compute NEML2 output with respect to specific model parameters and save that it as a MOOSE material property.
Specification(s): neml2_parameter_derivative
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.7The system shall provide for a modular way to transfer NEML2 results to material properties..
Specification(s): neml2_to_moose_material
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.84.8
The system shall be capable of interfacing with the NEML2 library to perform constitutive update
1. to solve an elasticity problem;
2. to solve a perfect viscoplasticity problem;
3. to solve a viscoplasticity problem with isotropic hardening;
4. to solve a viscoplasticity problem with kinematic hardening;
5. to solve a viscoplasticity problem with both isotropic and kinematic hardening;
6. to solve a viscoplasticity problem with non-associative Chaboche hardening;
7. to solve a viscoplasticity problem using radial return;
8. to solve a rate-independent problem with perfect plasticity;
9. to solve a rate-independent problem with isotropic hardening;
10. to solve a rate-independent problem with kinematic hardening;
11. to solve a rate-independent problem with both isotropic and kinematic hardening.
12. in a batched fashion.
Specification(s): neml2_legacy/elasticity, neml2_legacy/viscoplasticity_perfect, neml2_legacy/viscoplasticity_isoharden, neml2_legacy/viscoplasticity_kinharden, neml2_legacy/viscoplasticity_isokinharden, neml2_legacy/viscoplasticity_chaboche, neml2_legacy/viscoplasticity_radial_return, neml2_legacy/rate_independent_plasticity_perfect, neml2_legacy/rate_independent_plasticity_isoharden, neml2_legacy/rate_independent_plasticity_kinharden, neml2_legacy/rate_independent_plasticity_isokinharden, neml2_legacy/batched
Design: CauchyStressFromNEML2 CauchyStressFromNEML2UO CauchyStressFromNEML2Receiver
Issue(s): #26450 #26920
Collection(s): SYSTEM
Type(s): Exodiff

solid_mechanics: Stresses in Solid Mechanics
8.86.1
SolidMechanics shall be able to simulate the confined, uniaxial extension of a notched block which has constitutive law described by:
1. unsmoothed capped-Mohr-Coulomb plasticity
2. smoothed capped-Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al
3. unsmoothed Mohr-Coulomb plasticity
4. smoothed Mohr-Coulomb plasticity, with smoothing performed by the Abbo et al method
5. smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the cosine smoother
6. smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the poly1 smoother
7. smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the poly2 smoother
8. smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the poly3 smoother
Specification(s): confined_uniaxial/cmc_planar, confined_uniaxial/cmc_smooth, confined_uniaxial/biaxial_planar, confined_uniaxial/biaxial_abbo, confined_uniaxial/biaxial_smooth_cos, confined_uniaxial/biaxial_smooth_poly1, confined_uniaxial/biaxial_smooth_poly2, confined_uniaxial/biaxial_smooth_poly3
Design: Stresses in Solid Mechanics
Issue(s): #13766
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.110.1The mechanics system shall correctly compute the jacobian for 3D problems using small strain.
Specification(s): smallstrain_3D
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.2The mechanics system shall correctly compute the jacobian for 3D problems using incremental small strain.
Specification(s): incrementalstrain_3D
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.3The mechanics system shall correctly compute the jacobian for 3D problems using finite strain.
Specification(s): finitestrain_3D
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.7The mechanics system shall correctly compute the jacobian for RZ problems using small strain.
Specification(s): smallstrain_RZ
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.8The mechanics system shall correctly compute the jacobian for RZ problems using incremental small strain.
Specification(s): incrementalstrain_RZ
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.9The mechanics system shall correctly compute the jacobian for RZ problems using finite strain.
Specification(s): finitestrain_RZ
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.13The mechanics system shall correctly compute the jacobian for planestrain problems using small strain.
Specification(s): smallplanestrain
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.14The mechanics system shall correctly compute the jacobian for planestrain problems using incremental small strain.
Specification(s): incrementalplanestrain
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.15The mechanics system shall correctly compute the jacobian for planestrain problems using finite strain.
Specification(s): finiteplanestrain
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.19The mechanics system shall correctly compute the jacobian for spherical problems using small strain.
Specification(s): smallstrain_spherical
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.20The mechanics system shall correctly compute the jacobian for spherical problems using small, incremental strain.
Specification(s): incrementalstrain_spherical
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: WeakPlaneStress
8.88.1The system shall compute the correct Jacobian for plane stress conditions
Specification(s): weak_plane_stress_elastic_jacobian
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.88.2The system shall compute the correct Jacobian for plane stress conditions
Specification(s): ad_weak_plane_stress_elastic_jacobian
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.88.3The system shall compute plane stress conditions with small strains with input provided using the Master action
Specification(s): weak_plane_stress_small
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.88.4The system shall compute plane stress conditions with small strains
Specification(s): ad_weak_plane_stress_small
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.88.5The system shall compute plane stress conditions with incremental strains with input provided using the Master action
Specification(s): weak_plane_stress_incremental
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.88.6The system shall compute plane stress conditions with incremental strains with input provided using the Master action
Specification(s): ad_weak_plane_stress_incremental
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.88.7The system shall compute plane stress conditions with finite strains with input provided using the Master action
Specification(s): weak_plane_stress_finite
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.88.8The system shall compute plane stress conditions with finite strains with input provided using the Master action
Specification(s): ad_weak_plane_stress_finite
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.88.9The system shall compute the response of a 3D cube in uniaxial tension with finite strain to provide a benchmark for a 2D plane stress, finite strain model
Specification(s): 3D_finite_tension_pull
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.88.10The system shall compute the response of a cube in uniaxial tension using a 2D plane stress, finite strain model, and produce the same result as a 3D model
Specification(s): weak_plane_stress_finite_tension_pull
Design: WeakPlaneStress
Issue(s): #7902
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: PorosityFromStrain
8.90.1
The system shall compute a Porosity material property from a strain tensor
1. using traditional materials.
2. using automatic differentiation materials.
Specification(s): p/reg, p/ad
Design: PorosityFromStrain ADPorosityFromStrain
Issue(s): #15974
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.90.2
The system shall handle a negative calculated porosity computed from a strain tensor
1. by setting the porosity to zero.
2. by setting the porosity to the initial condition.
3. by throwing an exception.
Specification(s): negative/zero, negative/initial, negative/exception
Design: PorosityFromStrain ADPorosityFromStrain
Issue(s): #15974
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunExceptionCSVDiff
8.90.3
The system shall handle a nan calcualted porosity computed from a strain tensor
1. by throwing an exception.
Specification(s): nan/exception
Design: PorosityFromStrain ADPorosityFromStrain
Issue(s): #15974
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: ADPorosityFromStrain
8.90.1
The system shall compute a Porosity material property from a strain tensor
1. using traditional materials.
2. using automatic differentiation materials.
Specification(s): p/reg, p/ad
Design: PorosityFromStrain ADPorosityFromStrain
Issue(s): #15974
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.90.2
The system shall handle a negative calculated porosity computed from a strain tensor
1. by setting the porosity to zero.
2. by setting the porosity to the initial condition.
3. by throwing an exception.
Specification(s): negative/zero, negative/initial, negative/exception
Design: PorosityFromStrain ADPorosityFromStrain
Issue(s): #15974
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunExceptionCSVDiff
8.90.3
The system shall handle a nan calcualted porosity computed from a strain tensor
1. by throwing an exception.
Specification(s): nan/exception
Design: PorosityFromStrain ADPorosityFromStrain
Issue(s): #15974
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Side Reaction Postprocessor
8.91.1The system shall be able to compute the force on a sideset.
Specification(s): sideset_force
Design: Side Reaction Postprocessor
Issue(s): #15163
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Material Tensor Average
8.91.2The system shall be able to compute the volume average of rank two tensor component.
Specification(s): material_tensor_avg_test
Design: Material Tensor Average
Issue(s): #15424
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.91.3The system shall be able to compute the volume average of rank two tensor component, which was computed using automatic differentiation.
Specification(s): material_tensor_avg_AD_test
Design: Material Tensor Average
Issue(s): #15424
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: NormalBoundaryDisplacement
8.91.4The system shall compute normal displacements on a surface for checking correct application of penalty boundary conditions.
Specification(s): normal_displacement
Design: NormalBoundaryDisplacement
Issue(s): #16346
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: MooseException
8.92.1
The system shall gracefully allow exceptions from the radial return mapping algorithm
1. not using automatic differentiation methods.
2. using automatic differentiation methods.
Specification(s): exception/non, exception/ad
Design: MooseException
Issue(s): #9659 #20290
Collection(s): FUNCTIONAL
Type(s): RunApp

solid_mechanics: NonlinearSystem
8.93.1Convergence matches previous version of MOOSE without the preconditioner reuse system
Specification(s): without_reuse
Design: NonlinearSystem
Issue(s): #21868
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.93.2Preconditioner is reused until the linear iterations exceed the value of reuse_preconditioner_max_its upon which the system recalculates the preconditioner
Specification(s): with_reuse
Design: NonlinearSystem
Issue(s): #21868
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Pressure
8.94.3The Pressure boundary condition shall compute the correct Jacobian for a problem in 3D space using hex8 elements.
Specification(s): jacobian_3D_hex8
Design: Pressure
Issue(s): #19657
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.94.4The Pressure boundary condition shall compute the correct Jacobian for a problem in 3D space using hex20 elements.
Specification(s): jacobian_3D_hex20
Design: Pressure
Issue(s): #19657
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.94.5The Pressure boundary condition shall compute the correct Jacobian for a problem in RZ coordinates with quad4 elements.
Specification(s): jacobian_RZ
Design: Pressure
Issue(s): #19657
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.94.6The Pressure boundary condition shall compute the correct Jacobian for a problem in RZ coordinates with quad8 elements.
Specification(s): jacobian_RZ_quad8
Design: Pressure
Issue(s): #19657
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.21The mechanics system shall correctly compute the jacobian for spherical problems using small, incremental strain.
Specification(s): incstrn_pressure_spherical
Design: Pressure
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: RadialDisplacementCylinderAux
8.95.1The system shall compute the radial component of displacement for axisymmetric cylindrical models
Specification(s): cylinder_2d_axisymmetric
Design: RadialDisplacementCylinderAux
Issue(s): #7604
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.95.2The system shall compute the radial component of displacement for 2D Cartesian cylindrical models
Specification(s): cylinder_2d_cartesian
Design: RadialDisplacementCylinderAux
Issue(s): #7604
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.95.3The system shall compute the radial component of displacement for 3D Cartesian cylindrical models
Specification(s): cylinder_3d_cartesian
Design: RadialDisplacementCylinderAux
Issue(s): #7604
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.95.8The system shall report an error if "axis_vector" is supplied to RadialDisplacementCylinderAux and the model is not 3D Cartesian
Specification(s): cylinder_2d_axisymmetric_except_1
Design: RadialDisplacementCylinderAux
Issue(s): #7604
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.95.9The system shall report an error if "axis_vector" has length of zero
Specification(s): cylinder_3d_cartesian_except_1
Design: RadialDisplacementCylinderAux
Issue(s): #7604
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: RadialDisplacementSphereAux
8.95.4The system shall compute the radial component of displacement for 1D spherical models
Specification(s): sphere_1d_spherical
Design: RadialDisplacementSphereAux
Issue(s): #7604
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.95.5The system shall compute the radial component of displacement for axisymmetric spherical models
Specification(s): sphere_2d_axisymmetric
Design: RadialDisplacementSphereAux
Issue(s): #7604
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.95.6The system shall compute the radial component of displacement for 3D Cartesian spherical models
Specification(s): sphere_3d_cartesian
Design: RadialDisplacementSphereAux
Issue(s): #7604
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.95.7The system shall report an error if "origin" is supplied to RadialDisplacementSphereAux when the coordinate system is not Cartesian or axisymmetric
Specification(s): sphere_1d_spherical_except_1
Design: RadialDisplacementSphereAux
Issue(s): #7604
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Combined Nonlinear Hardening Plasticity
8.96.1The system shall compute the J2 linear kinematic plasticity stress based on the imposed cyclic nonsymmetric strain
Specification(s): linear_kinharden_nonsymmetric_strain_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.96.2The system shall compute the J2 linear kinematic plasticity stress based on the imposedcyclic symmetric strain
Specification(s): linear_kinharden_symmetric_strain_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.96.3The system shall compute the J2 nonlinear isotropic plasticity stress based on the imposedcyclic symmetric strain
Specification(s): nonlin_isoharden_symmetric_strain_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.96.4The system shall compute the J2 nonlinear combined plasticity stress based on the imposed cyclic symmetric strain
Specification(s): nonlin_isokinharden_symmetric_strain_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.96.5The system shall compute the J2 nonlinear kinematic plasticity stress based on the imposed cyclic nonsymmetric strain
Specification(s): nonlin_kinharden_nonsymmetric_strain_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.96.6The system shall compute the J2 nonlinear kinematic plasticity stress based on the imposed cyclic nonsymmetric strain
Specification(s): nonlin_kinharden_symmetric_strain_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.96.7The system shall compute the J2 nonlinear kinematic plasticity strain based on the imposed cyclic nonsymmetric loading
Specification(s): 1D_ratcheting_nonlin_kinharden_stress_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.96.8The system shall compute the J2 linear kinematic plasticity strain based on the imposed cyclic nonsymmetric loading
Specification(s): linear_kinharden_nonsymmetric_stress_controlled
Design: Combined Nonlinear Hardening Plasticity
Issue(s): #28688
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Isotropic Plasticity Stress Update
8.97.1The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation.
Specification(s): isotropic_plasticity_incremental
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.2The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation while prescribing a base name for the isotropic plasticity material properties.
Specification(s): isotropic_plasticity_incremental_base_name
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.3The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation and using the b-bar element volume correction.
Specification(s): isotropic_plasticity_incremental_Bbar
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.4The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation.
Specification(s): isotropic_plasticity_finite
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.5The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation and using the b-bar element volume correction.
Specification(s): isotropic_plasticity_finite_Bbar
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.7The system shall only allow the calculation of a J2 isotropic plasticity stress response with only one but not both of a hardening function or hardening constant specified to define the evolving yield surface.
Specification(s): isotropic_plasticity_error1
Design: Isotropic Plasticity Stress Update
Issue(s): #5481 #11239
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.97.8The system shall only calculate the J2 isotropic plasticity stress response when either a hardening function or a hardening constant is specified to define the evolving yield surface.
Specification(s): isotropic_plasticity_error2
Design: Isotropic Plasticity Stress Update
Issue(s): #5481 #11239
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.97.9The system shall only calculate the J2 isotropic plasticity stress response when either a constant yield stress or a yield stress function is specified to define the initial yield surface.
Specification(s): isotropic_plasticity_error3
Design: Isotropic Plasticity Stress Update
Issue(s): #5481 #11239
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.97.10The system shall return an error if a negative yield stress is supplied when calculating the J2 isotropic plasticity stress response.
Specification(s): isotropic_plasticity_error4
Design: Isotropic Plasticity Stress Update
Issue(s): #5481 #11239
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.97.11The system shall return an error if anisotropic elasticity tensor is supplied when the J2 isotropic plasticity stress response calculation is requested.
Specification(s): isotropic_plasticity_error5
Design: Isotropic Plasticity Stress Update
Issue(s): #5481 #11239
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.97.12The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213.
Specification(s): affine_plasticity
Design: Isotropic Plasticity Stress Update Compute Multiple Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.97.13The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213. This shall be done with a coupled creep and plasticity model where the creep model is inactive.
Specification(s): cp_affine_plasticity
Design: Isotropic Plasticity Stress Update Compute Creep and Plasticity Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Hyperbolic Viscoplasticity Stress Update
8.97.6The system shall compute the hyperbolic visoplastic stress response for a time-dependent linear strain hardening plasticity model in a small incremental strain formulation in a manner equivalent to the ABAQUS result.
Specification(s): uniaxial_viscoplasticity
Design: Hyperbolic Viscoplasticity Stress Update
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Compute Creep and Plasticity Inelastic Stress
8.97.13The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213. This shall be done with a coupled creep and plasticity model where the creep model is inactive.
Specification(s): cp_affine_plasticity
Design: Isotropic Plasticity Stress Update Compute Creep and Plasticity Inelastic Stress
Issue(s): #5481 #11239
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: LAROMANCE Stress Update with Automatic Differentiation
8.98.1
The system shall compute a creep rate based on a reduced order model
1. and evolve over time with an good finite difference width.
2. and evolve over time with an poor finite difference width with more nonlinear iterations than with a good finite difference width.
3. in 3D.
4. with units of stress other than Pascal.
5. in 2DRz.
6. in 2DRz with a model loaded from a JSON data file.
7. in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a small set of input parameters not using AD.
8. in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a large set of input parameters not using AD.
9. at the lower temperature limit.
10. below the lower temperature limit and extrapolate correctly.
11. but should error out below the lower temperature limit if requested by the user.
12. but should error out above the upper temperature limit if requested by the user.
13. when substepping is off and the time step size does not guarantee the most accurate results.
14. when substepping is off and the time step size guarantees accurate results.
15. when substepping is on and the numerical integration error selected by the user guarantees accurate results.
16. when substepping is on and the numerical integration error selected by the user guarantees accurate results but substepping settings require a system-wise time step cut because the computed number of substeps exceeds the maximum_number_substeps parameter.
17. for a variety of overlapping tiles and two overlapping partitions.
18. for a variety of overlapping tiles and two overlapping partitions with a model loaded from a JSON data file.
19. for a variety of overlapping tiles and two overlapping partitions with a model loaded from a JSON data file relative to the input.
20. for a variety of overlapping tiles and two overlapping partitions, and be able to export the model data to a JSON file.
Specification(s): rom/3tile_strain, rom/3tile_strain_small_fd, rom/3d, rom/3d_MPA, rom/2drz, rom/2drz_json, rom/nonad_verification, rom/nonad_verification_heavy, rom/lower_limit, rom/lower_limit_extrapolated, rom/lower_limit_error, rom/upper_limit_error, rom/creep_ramp_sub_false, rom/creep_ramp_sub_false_more_steps, rom/creep_ramp_sub_true, rom/creep_ramp_sub_true_exception, rom/3tile, rom/3tile_json, rom/3tile_json_relative, rom/3tile_json_export
Design: LAROMANCE Stress Update with Automatic Differentiation
Issue(s): #14046 #16520 #17287 #20827
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): JSONDiffRunExceptionRunAppCSVDiff
8.98.2
The system shall compute a creep rate based on a reduced order model using AD
1. in 3D.
2. with units of stress other than Pascal.
3. in 3D and compute a perfect Jacobian.
4. in 2DRz.
5. in 2DRz and compute a perfect Jacobian.
6. in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a small set of input parameters using AD.
7. in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a large set of input parameters using AD.
8. at the lower temperature limit.
9. below the lower temperature limit and extrapolate correctly.
Specification(s): ADrom/3d, ADrom/3d_MPA, ADrom/3d-jac, ADrom/2drz, ADrom/2drz-jac, ADrom/ad_verification, ADrom/ad_verification_heavy, ADrom/lower_limit, ADrom/lower_limit_extrapolated
Design: LAROMANCE Stress Update with Automatic Differentiation
Issue(s): #14046
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTesterCSVDiff

solid_mechanics: Compute Damage Stress
8.99.1The system shall calculate the effect of damage on the stress of a elastic material.
Specification(s): scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.2The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation.
Specification(s): ad_scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.3The system shall calculate damaged stress based on old damage index.
Specification(s): scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.4The system shall calculate damaged stress based on old damage index when using automatic differentiation.
Specification(s): ad_scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.5The system shall report an error when damage index is greater than 1.
Specification(s): scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.6The system shall report an error when damage index is greater than 1 also when using automatic differentiation.
Specification(s): ad_scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.7The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress
Specification(s): scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.8The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation
Specification(s): ad_scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.9The system shall calculate the maximum value of the damage index comparing different damage models.
Specification(s): combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.10The system shall calculate the effective damage index from different damage models.
Specification(s): combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.11The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model
Specification(s): combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.12The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models.
Specification(s): combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.13The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.14The system shall calculate the effective damage index from different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.15The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.16The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.17The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation.
Specification(s): scalar_damage_material_inelastic
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.18The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation.
Specification(s): scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.19The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation.
Specification(s): ad_scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.20The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object.
Specification(s): multiple_inelastic_bad_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #20722
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.21The system shall calculate the effect of damage on the stress of a nonlocal damage model.
Specification(s): nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.22The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation.
Specification(s): ad_nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: NonlocalDamage
8.99.1The system shall calculate the effect of damage on the stress of a elastic material.
Specification(s): scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.2The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation.
Specification(s): ad_scalar_damage_material
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.3The system shall calculate damaged stress based on old damage index.
Specification(s): scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.4The system shall calculate damaged stress based on old damage index when using automatic differentiation.
Specification(s): ad_scalar_damage_material_old
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.5The system shall report an error when damage index is greater than 1.
Specification(s): scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.6The system shall report an error when damage index is greater than 1 also when using automatic differentiation.
Specification(s): ad_scalar_damage_material_out_of_bounds
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.7The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress
Specification(s): scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.8The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation
Specification(s): ad_scalar_damage_incompatible_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.9The system shall calculate the maximum value of the damage index comparing different damage models.
Specification(s): combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.10The system shall calculate the effective damage index from different damage models.
Specification(s): combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.11The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model
Specification(s): combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.12The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models.
Specification(s): combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.13The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_max
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.14The system shall calculate the effective damage index from different damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_mult
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.15The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_sub
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.16The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation.
Specification(s): ad_combined_scalar_damage_limit_combined
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.17The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation.
Specification(s): scalar_damage_material_inelastic
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.18The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation.
Specification(s): scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.19The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation.
Specification(s): ad_scalar_damage_material_creep_power
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #11041
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.20The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object.
Specification(s): multiple_inelastic_bad_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #20722
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.99.21The system shall calculate the effect of damage on the stress of a nonlocal damage model.
Specification(s): nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.99.22The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation.
Specification(s): ad_nonlocal_damage_model
Design: Compute Damage Stress Scalar Material Damage Compute Multiple Inelastic Stress NonlocalDamage
Issue(s): #21786
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Shell elements
8.100.1
The mechanics system shall accurately predict the dynamic behavior of a shell element with clamped-free-free-free conditions when
1. the surface is on the XY plane
2. the surface is at a 45 deg. angle w.r.t. the Y axis
3. the surface is at a 45 deg. angle w.r.t. the Y axis and HHT input is provided
Specification(s): verification_tests/shell_dynamics_bending_moment_free, verification_tests/shell_dynamics_bending_moment_free_orientation_inclined, verification_tests/shell_dynamics_bending_moment_free_orientation_inclined_hht
Design: Shell elements
Issue(s): #15067
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.100.3The mechanics system shall accurately compute the deflection of a cantilever beam when it is modeled using shell elements.
Specification(s): beam_bending
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.4The mechanics system shall accurately compute the deflection of a rotated cantilever beam when it is modeled using shell elements.
Specification(s): rotated_beam_bending
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.5The mechanics system shall accurately compute the deflection of a cantilever beam when it is modeled using shell elements under large strain and rotations are included.
Specification(s): large_beam_bending
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.6The mechanics system shall accurately compute the Jacobian for a small strain quasi-static shell element.
Specification(s): beam_bending_jacobian
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.100.7The mechanics system shall accurately compute the Jacobian for a large strain quasi-static shell element.
Specification(s): large_beam_bending_jacobian
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.100.8The mechanics system shall accurately model the deflection of a simply supported under uniform loading.
Specification(s): plate_bending
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.9The mechanics system shall accurately model deflection of a plate with multiple force and moment boundary conditions.
Specification(s): plate_bending2
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.10The mechanics system shall converge to the analytic displacement of a cylinder modeled with shell elements, with point loading applied in the x direction.
Specification(s): pinched_cylinder
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.100.11The mechanics system shall converge to the analytic displacement of a cylinder modeled with shell elements, with point loading applied in the y direction.
Specification(s): pinched_cylinder_y
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.100.12The mechanics system shall accurately model the deflection of a inclined shell elements.
Specification(s): inclined_plane
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.13The mechanics system shall accurately compute the axial stress and strain of the shell elements.
Specification(s): straintest_axial
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.14The mechanics system shall accurately compute the axial stress and strain of the shell elements using the finite strain formulation.
Specification(s): finite_straintest_axial
Design: Shell elements
Issue(s): #25266
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.15The mechanics system shall accurately compute the stress and strain of the shell elements subjected to shear deformation.
Specification(s): straintest_shear
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.16The mechanics system shall accurately compute the stress and strain of the tapered shell elements.
Specification(s): tapered
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.100.17The system shall generate an error if the shell strain material is evaluated when the number of quadrature points does not equal 4.
Specification(s): qp_error
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.100.18Shell elements should have compatible stresses even for unstructured meshes.
Specification(s): pinched_cylinder_symm_unstructured
Design: Shell elements
Issue(s): #14280 #21384 #28471
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ADInertialForceShell
8.100.2The mechanics system shall accurately predict the dynamic behavior of a shell element.
Specification(s): shell_dynamics
Design: ADInertialForceShell
Issue(s): #15067
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Smeared Cracking Stress
8.101.1The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in cartesian coordinates.
Specification(s): cracking
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.2The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in rz coordinates.
Specification(s): cracking_rz
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.3The MOOSE SolidMechanics module shall simulate cracking while the cracking strength is prescribed by an elemental AuxVariable.
Specification(s): cracking_function
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.4The MOOSE SolidMechanics module shall simulate exponential stress release.
Specification(s): exponential
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.5The MOOSE SolidMechanics module shall simulate exponential stress relase while using the rz coordinate system.
Specification(s): rz_exponential
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.6The MOOSE SolidMechanics module shall demonstrate softening using the power law for smeared cracking.
Specification(s): power
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.7The MOOSE SolidMechanics module shall demonstrate the prescribed softening laws in three directions, power law (x), exponential (y), and abrupt (z).
Specification(s): multiple_softening
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.8The MOOSE SolidMechanics module shall simulate smeared cracking in the x y and z directions.
Specification(s): xyz
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.9The MOOSE SolidMechanics module shall simulate smeared cracking under plane stress conditions.
Specification(s): plane_stress
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.10The MOOSE SolidMechanics module shall demonstrate that the smeared cracking model correctly handles finite rotation of cracked elements.
Specification(s): cracking_rotation
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.11The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in x.
Specification(s): cracking_rotation_pres_dir_x
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.12The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in z.
Specification(s): cracking_rotation_pres_dir_z
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.13The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where two cracks are prescribed in x and z.
Specification(s): cracking_rotation_pres_dir_xz
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.101.14The ComputeSmearedCrackingStress model shall generate a warning if 'cracked_elasticity_type' is not specified
Specification(s): cracking_err_diagonal
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.101.15The ComputeSmearedCrackingStress model shall generate an error if an invalid number of softening models is specified
Specification(s): cracking_err_softening
Design: Compute Smeared Cracking Stress
Issue(s): #6815 #9227
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Strain Energy Density
8.104.1The system shall be capable of calculating strain energy density incrementally in materials with elastic stress and finite strain.
Specification(s): incr_elas
Design: Strain Energy Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.104.2The system shall be capable of informing a user when they incorrectly choose not to use the incremental strain energy density formulation with an incremental material model.
Specification(s): incr_chk1
Design: Strain Energy Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.104.4The system shall be capable of calculating strain energy density for materials with elastic stress and small strain.
Specification(s): tot_elas
Design: Strain Energy Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.104.5The system shall be capable of informing a user when they incorrectly choose to use the incremental strain energy density formulation in a material utilizing small strain.
Specification(s): tot_chk1
Design: Strain Energy Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.104.6The system shall be capable of calculating strain energy density incrementally in materials with inelastic stress and isotropic plasticity.
Specification(s): incr_elas_plas
Design: Strain Energy Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.104.11The system shall be capable of calculating strain energy density for materials with a user-specified stress by name and small strain.
Specification(s): tot_elas_stress_name
Design: Strain Energy Density
Issue(s): #25202
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compliance Sensitivity
8.104.3The system shall be able to create a compliance sensitivity material.
Specification(s): incr_model_sensitivity
Design: Compliance Sensitivity
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Strain Energy Rate Density
8.104.7The system shall be capable of calculating strain energy rate density with elastic stress and finite strain.
Specification(s): rate_model
Design: Strain Energy Rate Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.104.8The system shall be capable of calculating strain energy rate density when using small strain assumptions.
Specification(s): rate_model_small
Design: Strain Energy Rate Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.104.9The system shall be capable of calculating strain energy rate density when using automatic differentiation and weak plane stress.
Specification(s): ad_rate_model_weak_plane
Design: Strain Energy Rate Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.104.10The system shall be capable of calculating strain energy rate density when using hand-coded Jacobian and weak plane stress.
Specification(s): nonAD_rate_model_weak_plane
Design: Strain Energy Rate Density
Issue(s): #10972 #25602
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Radial Return Stress Update with automatic differentiation
8.106.1The system shall report diverged return mapping solve due to large deformation imposed in one step using automatic differentiation
Specification(s): ad_power_law
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.106.2The system shall converge under large deformation owing to the help of substepping using automatic differentiation
Specification(s): ad_power_law_substepping
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.106.3The system shall converge under large deformation owing to the help of adaptive substepping using automatic differentiation with an increment based substepping criterion
Specification(s): ad_power_law_adaptive_substepping_increment
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.106.4The system shall converge under large deformation owing to the help of adaptive substepping using automatic differentiation with an error based substepping criterion
Specification(s): ad_power_law_adaptive_substepping_error
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.106.5The system shall report diverged return mapping solve due to large deformation imposed in one step
Specification(s): power_law
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.106.6The system shall converge under large deformation owing to the help of substepping
Specification(s): power_law_substepping
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.106.7The system shall converge under large deformation owing to the help of adaptive substepping with an increment based substepping criterion
Specification(s): power_law_adaptive_substepping_increment
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.106.8The system shall converge under large deformation owing to the help of adaptive substepping with an error based substepping criterion
Specification(s): power_law_adaptive_substepping_error
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.106.9The system shall output verbose information about radial return iterations.
Specification(s): output
Design: Radial Return Stress Update with automatic differentiation
Issue(s): #14757
Collection(s): FUNCTIONAL
Type(s): RunApp

solid_mechanics: Temperature Dependent Hardening Stress Update
8.108.1The system shall compute the stress as a function of temperature and plastic strain from user-supplied hardening functions not using automatic differentiation.
Specification(s): test
Design: Temperature Dependent Hardening Stress Update
Issue(s): #7043
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.108.2The system shall compute the stress as a function of temperature and plastic strain from user-supplied hardening functions using automatic differentiation.
Specification(s): ADtest
Design: Temperature Dependent Hardening Stress Update
Issue(s): #18454
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Strain Formulations in Solid Mechanics
8.110.1The mechanics system shall correctly compute the jacobian for 3D problems using small strain.
Specification(s): smallstrain_3D
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.2The mechanics system shall correctly compute the jacobian for 3D problems using incremental small strain.
Specification(s): incrementalstrain_3D
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.3The mechanics system shall correctly compute the jacobian for 3D problems using finite strain.
Specification(s): finitestrain_3D
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.7The mechanics system shall correctly compute the jacobian for RZ problems using small strain.
Specification(s): smallstrain_RZ
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.8The mechanics system shall correctly compute the jacobian for RZ problems using incremental small strain.
Specification(s): incrementalstrain_RZ
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.9The mechanics system shall correctly compute the jacobian for RZ problems using finite strain.
Specification(s): finitestrain_RZ
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.13The mechanics system shall correctly compute the jacobian for planestrain problems using small strain.
Specification(s): smallplanestrain
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.14The mechanics system shall correctly compute the jacobian for planestrain problems using incremental small strain.
Specification(s): incrementalplanestrain
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.15The mechanics system shall correctly compute the jacobian for planestrain problems using finite strain.
Specification(s): finiteplanestrain
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.19The mechanics system shall correctly compute the jacobian for spherical problems using small strain.
Specification(s): smallstrain_spherical
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.110.20The mechanics system shall correctly compute the jacobian for spherical problems using small, incremental strain.
Specification(s): incrementalstrain_spherical
Design: Strain Formulations in Solid Mechanics Stresses in Solid Mechanics
Issue(s): #8235
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Compute Thermal Expansion Eigenstrain
8.111.1The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion.
Specification(s): constant_expansion_coeff
Design: Compute Thermal Expansion Eigenstrain
Issue(s): #7457
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.2The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion when restarting the simulation.
Specification(s): constant_expansion_coeff_restart
Design: Compute Thermal Expansion Eigenstrain
Issue(s): #7457
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.3The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion with an initial strain due to the difference between the stress free temperature and initial temperature of the material.
Specification(s): constant_expansion_stress_free_temp
Design: Compute Thermal Expansion Eigenstrain Rank Two Aux
Issue(s): #8909
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.4The tensor mechanics module shall have the capability to combine multiple eigenstrains to correctly calculate an eigenstrain tensor resulting from isotropic thermal expansion.
Specification(s): multiple_thermal_eigenstrains
Design: Compute Thermal Expansion Eigenstrain Rank Two Aux
Issue(s): #7457
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.5The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion.
Specification(s): ad_constant_expansion_coeff
Design: Compute Thermal Expansion Eigenstrain
Issue(s): #13091
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.6The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion using the previous timestep.
Specification(s): ad_constant_expansion_coeff_old
Design: Compute Thermal Expansion Eigenstrain
Issue(s): #13091
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.7The Jacobian for the AD eigenstrain tensor resulting from isotropic thermal expansion shall be perfect
Specification(s): ad_constant_expansion_coeff-jac
Design: Compute Thermal Expansion Eigenstrain
Issue(s): #13091
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.111.8The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion with an initial strain due to the difference between the stress free temperature and initial temperature of the material.
Specification(s): ad_constant_expansion_stress_free_temp
Design: Compute Thermal Expansion Eigenstrain
Issue(s): #13091
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.9The Jacobian for the AD eigenstrain tensor resulting from isotropic thermal expansion with an initial strain shall be perfect
Specification(s): ad_constant_expansion_stress_free_temp-jac
Design: Compute Thermal Expansion Eigenstrain
Issue(s): #13091
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester

solid_mechanics: Rank Two Aux
8.111.3The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion with an initial strain due to the difference between the stress free temperature and initial temperature of the material.
Specification(s): constant_expansion_stress_free_temp
Design: Compute Thermal Expansion Eigenstrain Rank Two Aux
Issue(s): #8909
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.111.4The tensor mechanics module shall have the capability to combine multiple eigenstrains to correctly calculate an eigenstrain tensor resulting from isotropic thermal expansion.
Specification(s): multiple_thermal_eigenstrains
Design: Compute Thermal Expansion Eigenstrain Rank Two Aux
Issue(s): #7457
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Torque
8.113.1The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations.
Specification(s): non-ad
Design: Torque PolarMomentOfInertia RotationAngle
Issue(s): #17176
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.113.2The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations with automatic differentiation.
Specification(s): ad
Design: Torque PolarMomentOfInertia RotationAngle
Issue(s): #17176
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: PolarMomentOfInertia
8.113.1The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations.
Specification(s): non-ad
Design: Torque PolarMomentOfInertia RotationAngle
Issue(s): #17176
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.113.2The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations with automatic differentiation.
Specification(s): ad
Design: Torque PolarMomentOfInertia RotationAngle
Issue(s): #17176
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: RotationAngle
8.113.1The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations.
Specification(s): non-ad
Design: Torque PolarMomentOfInertia RotationAngle
Issue(s): #17176
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.113.2The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations with automatic differentiation.
Specification(s): ad
Design: Torque PolarMomentOfInertia RotationAngle
Issue(s): #17176
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Torque Reaction
8.114.1The system shall compute the torque for an applied deformation at the end of a beam in 2D
Specification(s): torque_reaction_2D
Design: Torque Reaction
Issue(s): #6484
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.114.2The system shall compute the torque for an applied deformation at the end of a beam in 3D
Specification(s): torque_reaction_3D
Design: Torque Reaction
Issue(s): #6484
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.114.3The system shall compute the torque resulting from twisting applied using DisplacementAboutAxis to the end of an elastic cylinder
Specification(s): torque_reaction_cylinder
Design: Torque Reaction Displacement About Axis
Issue(s): #6484
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: Displacement About Axis
8.114.3The system shall compute the torque resulting from twisting applied using DisplacementAboutAxis to the end of an elastic cylinder
Specification(s): torque_reaction_cylinder
Design: Torque Reaction Displacement About Axis
Issue(s): #6484
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.114.4The system shall provide a boundary condition that applies pure finite rigid body rotation to a surface of an elastic body
Specification(s): disp_about_axis_motion
Design: Displacement About Axis
Issue(s): #15092
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.114.5The system shall provide a boundary condition that applies pure finite rigid body rotation to a surface of an elastic body incrementally
Specification(s): disp_about_axis_motion_incremental
Design: Displacement About Axis
Issue(s): #15388
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.114.6The system shall be able to use disaplcement about axis after applying an arbitraty deformation
Specification(s): disp_about_axis_axial_motion_delayed
Design: Displacement About Axis
Issue(s): #15388
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.114.7The system shall generate an error if the DisplacementAboutAxis boundary condition is applied to a component outside the range applicable for the dimensionality of the model
Specification(s): disp_about_axis_error1
Design: Displacement About Axis
Issue(s): #15092
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.114.8The system shall generate an error if the vector prescribed using the axis_direction parameter in the DisplacementAboutAxis boundary condition has a length of zero
Specification(s): disp_about_axis_error2
Design: Displacement About Axis
Issue(s): #15092
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Transfers System
8.115.1The system shall be able to transfer a field from a displaced source domain to a target domain, using shape function evaluations in the source domain.
Specification(s): test
Design: Transfers System
Issue(s): #22534
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: LinearElasticTruss
8.116.1The mechanics system shall accurately model the axial response of 3D truss elements.
Specification(s): truss_3d
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.2The truss element shall work correctly when hex elements are also included in the same input or mesh file.
Specification(s): truss_hex
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.3The mechanics system shall accurately model the static response of a 2D frame modeled using truss elements.
Specification(s): truss_2d
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.4The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 3D truss elements.
Specification(s): truss_3d_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.5The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using truss and hex elements.
Specification(s): truss_hex_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.6The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 2D truss elements.
Specification(s): truss_2d_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.7The LineElementAction shall produce an error if area is not provided as input for truss elements.
Specification(s): action_error_1
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.116.8The LineElementAction shall produce an error if rotational variables are provided as input for truss elements.
Specification(s): action_error_2
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: StressDivergenceTensorsTruss
8.116.1The mechanics system shall accurately model the axial response of 3D truss elements.
Specification(s): truss_3d
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.2The truss element shall work correctly when hex elements are also included in the same input or mesh file.
Specification(s): truss_hex
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.3The mechanics system shall accurately model the static response of a 2D frame modeled using truss elements.
Specification(s): truss_2d
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.4The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 3D truss elements.
Specification(s): truss_3d_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.5The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using truss and hex elements.
Specification(s): truss_hex_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.6The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 2D truss elements.
Specification(s): truss_2d_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.7The LineElementAction shall produce an error if area is not provided as input for truss elements.
Specification(s): action_error_1
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.116.8The LineElementAction shall produce an error if rotational variables are provided as input for truss elements.
Specification(s): action_error_2
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: LineElement Action
8.116.1The mechanics system shall accurately model the axial response of 3D truss elements.
Specification(s): truss_3d
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.2The truss element shall work correctly when hex elements are also included in the same input or mesh file.
Specification(s): truss_hex
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.3The mechanics system shall accurately model the static response of a 2D frame modeled using truss elements.
Specification(s): truss_2d
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.4The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 3D truss elements.
Specification(s): truss_3d_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.5The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using truss and hex elements.
Specification(s): truss_hex_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.6The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 2D truss elements.
Specification(s): truss_2d_action
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.7The LineElementAction shall produce an error if area is not provided as input for truss elements.
Specification(s): action_error_1
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.116.8The LineElementAction shall produce an error if rotational variables are provided as input for truss elements.
Specification(s): action_error_2
Design: LinearElasticTruss StressDivergenceTensorsTruss LineElement Action
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: Plastic Truss
8.116.9The system shall correctly model the plastic response of truss elements with a linear hardening model under tension.
Specification(s): tensile
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.10The system shall correctly model the plastic response of truss elements with perfect plasticity under tension.
Specification(s): tensile_nohardening
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.11The system shall correctly model the plastic response of truss elements with a user-defined hardening function model under tension.
Specification(s): tensile_hardeningfn
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.12The system shall correctly model the plastic response of truss elements with a linear hardening model under compression.
Specification(s): compressive
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.13The system shall correctly model the plastic response of truss elements with perfect plasticity under compression.
Specification(s): compressive_nohardening
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.14The system shall correctly model the plastic response of truss elements with a user-defined hardening function model under compression.
Specification(s): compressive_hardeningfn
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.116.15PlasticTruss material should produce error if neither the hardening constant nor a hardening function is provided.
Specification(s): error_nohardening
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.116.16PlasticTruss material should produce error if both hardening constant and hardening function are provided.
Specification(s): error_hardening
Design: Plastic Truss
Issue(s): #6789 #2460 #10313 #14304
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException

solid_mechanics: AbaqusUserElement
8.117.1The UEL tri tests example shall be built.
Specification(s): build_uel_tri_tests
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): RunCommand
8.117.2The UEL tri states tests example shall be built.
Specification(s): build_uel_tri_states_tests
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): RunCommand
8.117.3The UEL build tests example shall be built.
Specification(s): build_uel_build_tests
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): RunCommand
8.117.4The UEL tri tests example shall be built.
Specification(s): build_uel_tri_tests_dbg
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): RunCommand
8.117.5The UEL tri states tests example shall be built.
Specification(s): build_uel_tri_states_tests_dbg
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): RunCommand
8.117.6The UEL build tests example shall be built.
Specification(s): build_uel_build_tests_dbg
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): RunCommand
8.117.7The system shall be able to solve a simple mechanics problem with small elastic deformation with a triangular mesh using MOOSE capabilities.
Specification(s): reference
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.8The system shall be able to solve a simple mechanics problem with small elastic deformation with a triangular mesh using a UEL plugin.
Specification(s): small
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.9The system shall be able to solve a simple mechanics problem with small elastic deformation with a triangular mesh using a UEL plugin calling a UMAT routine with its standard interface.
Specification(s): small_test
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.10The Abaqus UEL interface shall be able to pass initial correct values of coordinates into a user-defined UEL routine for a hexahedral element and a non-trivial setup.
Specification(s): uel_test_print
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): RunApp
8.117.11The Abaqus UEL interface shall be able to interface with a UEL that calls a UMAT interface and must yield the same results for a triangular element as a UEL routine that computes internal forces without calling a UMAT routine.
Specification(s): small_test_uel_umat
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.12The Abaqus UMAT interface shall be able to yield the same results for a triangular element as a UEL routine that computes internal forces without calling a UMAT routine or an analogous UEL interface that calls a UMAT routine for computing the stress vector and the Jacobian.
Specification(s): small_test_moose_umat
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.13The Abaqus UEL interface, calling a UMAT routine, shall be able to yield the same results for a triangular element that a UMAT routine that computes internal forces when the solution depends on system states and two external fields, including temperature.
Specification(s): small_test_uel_states_fields
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.14The Abaqus UMAT interface shall be able to yield the same results for a triangular element that a UEL routine that computes internal forces, calling a UMAT routine, when the solution depends on system states and two external fields, including temperature.
Specification(s): small_test_umat_states_fields
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.15The Abaqus UMAT interface shall be able to yield the same results for a triangular element that a UEL routine that computes internal forces, calling a UMAT routine, when the solution depends on system states and two external fields, including temperature, which vary significantly with space.
Specification(s): small_test_umat_states_fields_gradient
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.117.16The Abaqus UEL interface shall be able to yield the same results for a triangular element that a UMAT routine that computes internal forces when the solution depends on system states and two external fields, including temperature, which vary significantly with space. Therefore, the system shall properly handle state and external fields whose values depend on element location.
Specification(s): small_test_uel_states_fields_gradient
Design: AbaqusUserElement
Issue(s): #25163
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: AbaqusUExternalDB
8.118.1
The Abaqus UEXTERNALDB interface shall execute the UEXTERNALDB routine at the
1. beginning of the simulation.
2. beginning of each MOOSE time step.
3. end of each MOOSE time step.
4. end of the simulation.
Specification(s): execution/initial, execution/timestep_begin, execution/timestep_end, execution/final
Design: AbaqusUExternalDB
Issue(s): #1
Collection(s): FUNCTIONAL
Type(s): RunApp
8.118.2The Abaqus UEXTERNALDB interface shall interface with a general user object to obtain the proper loading step and pass it to the user routine.
Specification(s): steps
Design: AbaqusUExternalDB
Issue(s): #1
Collection(s): FUNCTIONAL
Type(s): RunApp
8.118.3The Abaqus UEXTERNALDB interface shall provide the Abaqus API to obtain the simulation output directory.
Specification(s): getoutdir
Design: AbaqusUExternalDB
Issue(s): #1
Collection(s): FUNCTIONAL
Type(s): RunApp
8.118.4The Abaqus UEXTERNALDB interface shall provide the Abaqus API to obtain the simulation job name.
Specification(s): getjobname
Design: AbaqusUExternalDB
Issue(s): #1
Collection(s): FUNCTIONAL
Type(s): RunApp
8.118.5
The Abaqus UEXTERNALDB interface shall provide Abaqus compatible message routine supporting the
1. info level.
2. warning level.
3. non-fatal error level.
4. fatal error level.
Specification(s): messages/info, messages/warning, messages/non_fatal, messages/error
Design: AbaqusUExternalDB
Issue(s): #1
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunAppRunException
8.118.6
The Abaqus UEXTERNALDB interface shall provide Abaqus compatible mutex management
1. supporting single threaded execution.
2. supporting at least 2 threads.
3. supporting at least 4 threads.
Specification(s): mutex/single_thread, mutex/two_threads, mutex/four_threads
Design: AbaqusUExternalDB
Issue(s): #1
Collection(s): FUNCTIONAL
Type(s): RunApp
8.118.7
The Abaqus UEXTERNALDB interface shall provide the Abaqus API for accessing shared memory objects
1. supporting single threaded execution.
2. supporting two threaded execution.
3. supporting four threaded execution.
Specification(s): sma_memory/single_thread, sma_memory/two_threads, sma_memory/four_threads
Design: AbaqusUExternalDB
Issue(s): #1
Collection(s): FUNCTIONAL
Type(s): RunApp

solid_mechanics: Abaqus UMAT Stress
8.119.1The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for stateful properties
Specification(s): linear_strain_hardening
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.2The system shall raise an error if a UMAT that requires incremental quantities is being used with a total strain formulation
Specification(s): total_strain_error
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.119.3The system shall provide an interface to use Abaqus UMAT materials written in Fortran77 as constitutive models, with support for finite strain elastic material models
Specification(s): elastic
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.4The system shall provide an interface to use Abaqus UMAT materials written in Fortran77 as constitutive models, with support for small strain elastic material models
Specification(s): elastic_small
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.5The system shall provide an interface to use Abaqus UMAT materials written in C/C++ as constitutive models, with support for finite strain elastic material models
Specification(s): elastic_C
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.6The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for finite strain elasticity
Specification(s): elastic_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.7The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for small strain elasticity
Specification(s): elastic_small_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.8The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for incremental strain elastic material models
Specification(s): elastic_incremental
Design: Abaqus UMAT Stress
Issue(s): #18843
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.9The Abaqus UMAT interface shall produce the correct stresses for the hyperelasticNeo-Hookean model under shear loading. The results shall not depend on the time step size.Reference computation with fine time stepping.
Specification(s): elastic_shear_reference
Design: Abaqus UMAT Stress
Issue(s): #21797
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.10The Abaqus UMAT interface shall produce the correct stresses for the hyperelasticNeo-Hookean model under shear loading. The results shall not depend on the time step size.Comparison with coarse time stepping.
Specification(s): elastic_shear
Design: Abaqus UMAT Stress
Issue(s): #21797
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.11The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with the ability to provide different parameters for different blocks using the same interface plug-in.
Specification(s): multiple_blocks
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.12The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with the ability to provide different parameters for different blocks using distinct interface plug-ins.
Specification(s): multiple_blocks_two_materials
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.13The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with the ability to provide different parameters for different blocks using distinct interface plug-ins in multi processor runs.
Specification(s): multiple_blocks_two_materials_parallel
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.14The system shall be able to simulate a multiblock solid mechanics test in which the blocks are meshed contiguously using the UMAT interface.
Specification(s): rve_multimaterial_umat
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.15The system shall be able to simulate a multiblock solid mechanics test in which the blocks are meshed contiguously.
Specification(s): rve_multimaterial_moose
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.18The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with an external field (not temperature) affecting material behavior
Specification(s): predef
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.19The system shall avoid regression in a simple mechanical problem where a strain field modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external field verification
Specification(s): predef_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.20The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with an external field (not temperature) step increment affecting material behavior
Specification(s): dpredef
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.21The system shall avoid regression in a simple mechanical problem where a real number representing the strain increment modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external field increment verification
Specification(s): dpredef_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.22The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with two external fields (not temperature) affecting material behavior
Specification(s): predef_multiple
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.23The system shall avoid regression in a simple mechanical problem where two strain fields modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external field verification
Specification(s): predef_multiple_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.24The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with two external material properties affecting material behavior
Specification(s): predef_multiple_mat
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.25The system shall avoid regression in a simple mechanical problem where two strain fields modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external material property verification
Specification(s): predef_multiple_reference_mat
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.26The Abaqus UMAT interface shall pass correct values for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when a single element is subjected to axial loading. Values are checked against verified references
Specification(s): predef
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): RunApp
8.119.27The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with two external fields (not temperature) step increment affecting material behavior and shear deformation
Specification(s): print_shear
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.28The system shall avoid regression in a simple mechanical problem where two strain increments modify the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT behavior in the presence of shear deformation.
Specification(s): print_shear_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.29The Abaqus UMAT interface shall pass the correct values for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when shear deformation (causing nontrivial rotation kinematics) is present.
Specification(s): print_shear_print
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): RunApp
8.119.30The Abaqus UMAT interface shall pass the correct values for the deformation gradient DFGRD1 and the rotation increment DROT, accounting for the fact, that the calling C++ code is row majorand the called Fortran code is column major.
Specification(s): print_shear_defgrad
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): RunApp
8.119.31The Abaqus UMAT interface shall pass the values for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when shear deformation is present and large deformation kinematics is true, which captures variables or properties that may rely on the displaced mesh, such as COORDS and CELENT.
Specification(s): print_shear_defgrad_deformed
Design: Abaqus UMAT Stress
Issue(s): #22880
Collection(s): FUNCTIONAL
Type(s): RunApp
8.119.32The Abaqus UMAT interface shall pass correct values into a C UMAT routine for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when a single element is subjected to axial loading. Values are checked against verified references
Specification(s): print_c
Design: Abaqus UMAT Stress
Issue(s): #18237
Collection(s): FUNCTIONAL
Type(s): RunApp
8.119.33The system shall generate identical numerical results regardless of whether the UMAT interface is written in Fortran or C. Generation of reference results.
Specification(s): print_compare_c
Design: Abaqus UMAT Stress
Issue(s): #18237
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.34The system shall generate identical numerical results regardless of whether the UMAT interface is written in Fortran or C. Verification.
Specification(s): print_compare_f
Design: Abaqus UMAT Stress
Issue(s): #18237
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.35The system shall allow for the correct use of Eigen matrices in C UMAT functions.
Specification(s): print_eigen
Design: Abaqus UMAT Stress
Issue(s): #18237
Collection(s): FUNCTIONAL
Type(s): RunApp
8.119.36UMAT shall generate the correct shear deformation and stress when a single element is sheared via a Dirichlet boundary condition on the XY plane with anisotropic shear stiffness; results must coincide with those of MOOSE.
Specification(s): shear_order_umat_umat_x
Design: Abaqus UMAT Stress
Issue(s): #20111
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.37UMAT shall generate the correct shear deformation and stress when a single element is sheared via a Dirichlet boundary condition on the YZ plane with anisotropic shear stiffness; results must coincide with those of MOOSE.
Specification(s): shear_order_umat_umat_z
Design: Abaqus UMAT Stress
Issue(s): #20111
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.38The system shall generate reference results of a sheared finite element on the XY plane.
Specification(s): shear_order_umat_moose_x
Design: Abaqus UMAT Stress
Issue(s): #20111
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.39The system shall generate reference results of a sheared finite element on the YZ plane.
Specification(s): shear_order_umat_moose_z
Design: Abaqus UMAT Stress
Issue(s): #20111
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.40The system shall generate a system Jacobian from the UMAT routines using large strain kinematics that is of the same order as the one generated by MOOSE using Rashid strain incrementation when the shear stiffness is anisotropic.
Specification(s): shear_order_umat_umat_z_jacobian
Design: Abaqus UMAT Stress
Issue(s): #20111
Collection(s): FUNCTIONAL
Type(s): PetscJacobianTester
8.119.41The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system.
Specification(s): elastic_temperature_steps
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.42The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object.
Specification(s): elastic_temperature_steps_uo
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.43The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object, to which the user only provides the step durations.
Specification(s): elastic_temperature_steps_uo_durations
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.44The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object, to which the user only provides the number of steps and the total time interval.
Specification(s): elastic_temperature_steps_uo_intervals
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.45The system shall ensure that solution synchronization times are enforced by default when employing a user object to determine the steps of the simulation.
Specification(s): elastic_temperature_steps_uo_sync
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.46The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object.
Specification(s): elastic_temperature_steps_uo_input
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.47The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence
Specification(s): elastic_temperature
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.48The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for finite strain elasticity and temperature dependence
Specification(s): elastic_temperature_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.49The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence, include the temperature step increment
Specification(s): elastic_dtemperature
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.50The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for finite strain elasticity and temperature dependence, including the temperature step increment
Specification(s): elastic_dtemperature_reference
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.119.51The system shall provide an interface to use Abaqus UMAT materials that allows the user to control the time step increment within the UMAT routine and combine it with MOOSE native time step controls, including cutback and growth factors, and soft terminations.
Specification(s): elastic_timestep
Design: Abaqus UMAT Stress
Issue(s): #14974
Collection(s): FUNCTIONAL
Type(s): Exodiff

solid_mechanics: ComputeDeformGradBasedStress
8.121.1The ComputeDeformGradBasedStress class shall correctly compute the stress based on the lagrangian strain.
Specification(s): elastic
Design: ComputeDeformGradBasedStress
Issue(s): #6604
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.121.2The ComputeDeformGradBasedStress class shall correctly compute the stress from lagrangian strain when volumetric locking correction is used.
Specification(s): elastic_Bbar
Design: ComputeDeformGradBasedStress Volumetric Locking Correction
Issue(s): #6604
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: ComputeVolumetricDeformGrad
8.121.3The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration.
Specification(s): interface
Design: ComputeVolumetricDeformGrad
Issue(s): #6604
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.121.4The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration when volumetric locking correction is used.
Specification(s): interface_Bbar
Design: ComputeVolumetricDeformGrad VolumeDeformGradCorrectedStress Volumetric Locking Correction
Issue(s): #6604
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: VolumeDeformGradCorrectedStress
8.121.4The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration when volumetric locking correction is used.
Specification(s): interface_Bbar
Design: ComputeVolumetricDeformGrad VolumeDeformGradCorrectedStress Volumetric Locking Correction
Issue(s): #6604
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: Compute Volumetric Eigenstrain
8.122.1The system shall correctly compute an eigenstrain tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain.
Specification(s): volumetric_eigenstrain
Design: Compute Volumetric Eigenstrain Rank Two Scalar Aux
Issue(s): #8615 #11743
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.122.3The volumetric strain computed using RankTwoScalarAux for a unit cube with imposed displacements shall be identical to that obtained by imposing an eigenstrain that causes the same deformation of that model.
Specification(s): volumetric_mechanical
Design: Compute Volumetric Eigenstrain Rank Two Scalar Aux
Issue(s): #8615 #11743
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: AD Compute Volumetric Eigenstrain
8.122.2The system shall correctly compute an eigenstrain using AD tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain.
Specification(s): ad_volumetric_eigenstrain
Design: AD Compute Volumetric Eigenstrain Rank Two Scalar Aux
Issue(s): #8615 #11743 #26880
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: SolidMechanicsPlasticWeakPlaneShear
8.124.1The system shall not allow a weak plane shear friction angle less than the dilation angle.
Specification(s): except1
Design: SolidMechanicsPlasticWeakPlaneShear
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.124.2The system shall not allow a zero length transverse direction vector
Specification(s): except2
Design: SolidMechanicsPlasticWeakPlaneShear
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.124.4
For the case of small deformations the system shall
1. return a value of shear of 1 and a normal stress value of 0 when the apex of the shear envelope is (0,2);
2. utlize the small smoother parameter under both pure tension and pure shear to solve;
3. return the stress state to the yield surface under random loading;
4. utilize the cap smoothing functionality under both pure tension and pure shear to solve the simulation.
Specification(s): small_deformations/small1, small_deformations/small2, small_deformations/small3, small_deformations/small4
Design: SolidMechanicsPlasticWeakPlaneShear
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.124.5
For large deformation cases the system shall
1. produce a solution without plasticity after the mesh is rotated by 90 degrees;
2. return the stress state to the yield surface under pure tensile loading conditions after the mesh is rotated by 45 degrees;
3. return the stress state to the yield surface under pseudo-random loading directions;
4. return the stress state to the yield surface under pseudo-random loading while using the cap-tip yeild surface scheme.
Specification(s): large_deformation/large1, large_deformation/large2, large_deformation/large3, large_deformation/large4
Design: SolidMechanicsPlasticWeakPlaneShear
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONAL
Type(s): ExodiffCSVDiff
8.124.6
Under small deformation loading selected to induce cohesion hardening the system shall
1. with repeated stretch loading;
2. for pure tension and then pure shear to map out the yield function;
3. with linearly increasing loading and an exponential hardening model;
4. with a linearly increasing load and a cubic hardening model.
Specification(s): small_deformation_hardening/small_harden1, small_deformation_hardening/small_harden2, small_deformation_hardening/small_harden3, small_deformation_hardening/small_harden4
Design: SolidMechanicsPlasticWeakPlaneShear
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.124.7The system shall return the stress state to the yield surface under random large deformation loads.
Specification(s): large_harden3
Design: SolidMechanicsPlasticWeakPlaneShear
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONAL
Type(s): CSVDiff

solid_mechanics: SolidMechanicsPlasticWeakPlaneTensile
8.125.1The system shall not allow a negative tensile strength value.
Specification(s): except1
Design: SolidMechanicsPlasticWeakPlaneTensile
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONALFAILURE_ANALYSIS
Type(s): RunException
8.125.2
With a single element stretched by 1e-6m, for small deformation, the system shall
1. return the stress state to the yield surface when the applied stress is above the yield surface tensile strength;
2. return the stress state to the specified vector yield surface;
3. not calculate a plastic solution because the applied stress is lower than the tension cutoff for the yield surface.
Specification(s): small_deformation/small1, small_deformation/small1N, small_deformation/small2
Design: SolidMechanicsPlasticWeakPlaneTensile
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONAL
Type(s): CSVDiff
8.125.3
Under large deformation loading the system shall
1. calculate a solution without plasticity after the mesh is rotated by 90 degrees;
2. return the stress state to the yield surface under pure tensile loading after the mesh is rotated by 45 degrees.
Specification(s): large_deformation/large1, large_deformation/large2
Design: SolidMechanicsPlasticWeakPlaneTensile
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONAL
Type(s): Exodiff
8.125.4
Under small deformation loading selected to induce hardening the system shall
1. the deformation shall produce increments of plastic strain in response to incremental loading steps;
2. evolve the plastic internal state variable for an exponential hardening model;
3. return the stress state to the evolving yield surface when loaded solely in the z-direction for an exponential hardening model;
4. return the stress state to the evolving yield surface when loaded solely in the z-direction for an cubic hardening model;
Specification(s): small_deformation_hardening/small_hard1, small_deformation_hardening/small_hard2, small_deformation_hardening/small_hard3, small_deformation_hardening/small_hard_cubic
Design: SolidMechanicsPlasticWeakPlaneTensile
Issue(s): #3878 #4150 #4507
Collection(s): FUNCTIONAL
Type(s): CSVDiff

References

ISO/IEC/IEEE 24765:2010(E). Systems and software engineering—Vocabulary. first edition, December 15 2010.

@manual{ISO-systems-software,
    author = "24765:2010(E), ISO/IEC/IEEE",
    title = "Systems and software engineering---Vocabulary",
    edition = "First",
    year = "2010",
    month = "December 15"
}

ASME NQA-1. ASME NQA-1-2008 with the NQA-1a-2009 addenda: Quality Assurance Requirements for Nuclear Facility Applications. first edition, August 31 2009.

@manual{ASME-NQA-1-2008,
    author = "NQA-1, ASME",
    title = "ASME NQA-1-2008 with the NQA-1a-2009 addenda: Quality Assurance Requirements for Nuclear Facility Applications",
    orginization = "American Socieity of Mechanical Engineers",
    year = "2009",
    month = "August 31",
    edition = "First"
}

[./axisymmetric_gps_incremental]
  type = 'Exodiff'
  input = 'axisymmetric_gps_incremental.i'
  exodiff = 'axisymmetric_gps_incremental_out.e'
  design = 'GeneralizedPlaneStrainAction.md'
  requirement = 'The system shall support generalized plane strain with incremental strain for 1D meshes using the SolidMechanics/QuasiStatic Physics.'
[../]

[./axisymmetric_gps_small]
  type = 'Exodiff'
  input = 'axisymmetric_gps_small.i'
  exodiff = 'axisymmetric_gps_small_out.e'
  design = 'GeneralizedPlaneStrainAction.md'
  requirement = 'The system shall support generalized plane strain with small strain for 1D meshes using the SolidMechanics/QuasiStatic Physics.'
[../]

[./axisymmetric_gps_finite]
  type = 'Exodiff'
  input = 'axisymmetric_gps_finite.i'
  exodiff = 'axisymmetric_gps_finite_out.e'
  design = 'GeneralizedPlaneStrainAction.md'
  requirement = 'The system shall support generalized plane strain with finite strain for 1D meshes using the SolidMechanics/QuasiStatic Physics.'
[../]

[generalized_plane_strain_squares]
  type = 'Exodiff'
  input = 'generalized_plane_strain_squares.i'
  exodiff = 'generalized_plane_strain_squares_out.e'
  abs_zero = 1e-7
  requirement = 'The system shall support setting up a generalized plane strain problem through an action'
  design = 'GeneralizedPlaneStrainAction.md'
  issues = '#7840'
[]

[out_of_plane_pressure_function]
  type = 'Exodiff'
  input = 'out_of_plane_pressure.i'
  exodiff = 'out_of_plane_pressure_out.e'
  abs_zero = 1e-9
  requirement = 'The system shall support setting the out-of-plane pressure using a function for generalized plane strain problems'
  design = 'GeneralizedPlaneStrainAction.md'
  issues = '#7840'
[]

[out_of_plane_pressure_material]
  type = 'Exodiff'
  input = 'out_of_plane_pressure.i'
  exodiff = 'out_of_plane_pressure_out.e'
  cli_args = 'Physics/SolidMechanics/GeneralizedPlaneStrain/gps/out_of_plane_pressure_function=0 Physics/SolidMechanics/GeneralizedPlaneStrain/gps/out_of_plane_pressure_material=traction_material'
  abs_zero = 1e-9
  requirement = 'The system shall support setting the out-of-plane pressure using a material property for generalized plane strain problems'
  design = 'GeneralizedPlaneStrainAction.md'
  issues = '#17250'
  prereq = out_of_plane_pressure_function
[]

[generalized_plane_strain_scalar_vector]
  type = 'Exodiff'
  input = 'generalized_plane_strain_scalar_vector.i'
  exodiff = 'generalized_plane_strain_scalar_vector_out.e'
  prereq = 'generalized_plane_strain_squares'
  abs_zero = 1e-7
  allow_test_objects = true
  requirement = 'The system shall support listing all of the out-of-plane strain variables in the strain calculator'
  design = 'GeneralizedPlaneStrainAction.md'
  issues = '#7840'
[]

[./axisymmetric_plane_strain_incremental]
  type = 'Exodiff'
  input = 'axisymm_plane_strain_incremental.i'
  exodiff = 'axisymm_plane_strain_incremental_out.e'
  design = 'source/materials/ComputeAxisymmetric1DIncrementalStrain.md'
  requirement = 'The ComputeAxisymmetric1DIncrementalStrain class shall compute the elastic stress for a 1D axisymmetric small incremental strain formulation under a combination of applied tensile displacement and thermal expansion loading using the SolidMechanics/QuasiStatic Physics.'
[../]

[./axisymm_gps_incremental]
  type = 'Exodiff'
  input = 'axisymm_gps_incremental.i'
  exodiff = 'axisymm_gps_incremental_out.e'
  design = 'source/materials/ComputeAxisymmetric1DIncrementalStrain.md'
  requirement = 'The ComputeAxisymmetric1DIncrementalStrain class shall, under generalized plane strain conditions, compute the elastic stress for a 1D axisymmetric small incremental strain formulation under a combination of applied tensile displacement and thermal expansion loading.'
[../]

[./axisymmetric_plane_strain_small]
  type = 'Exodiff'
  input = 'axisymm_plane_strain_small.i'
  exodiff = 'axisymm_plane_strain_small_out.e'
  design = 'source/materials/ComputeAxisymmetric1DSmallStrain.md'
  requirement = 'The ComputeAxisymmetric1DSmallStrain class shall compute the elastic stress for a 1D axisymmetric small total strain formulation under a combination of applied tensile displacement and thermal expansion loading using the SolidMechanics/QuasiStatic Physics.'
[../]

[./axisymm_gps_small]
  type = 'Exodiff'
  input = 'axisymm_gps_small.i'
  exodiff = 'axisymm_gps_small_out.e'
  design = 'source/materials/ComputeAxisymmetric1DSmallStrain.md'
  requirement = 'The ComputeAxisymmetric1DSmallStrain class shall, under generalized plane strain conditions, compute the elastic stress for a 1D axisymmetric small total strain formulation under a combination of applied tensile displacement and thermal expansion loading.'
[../]

[./axisymmetric_plane_strain_finite]
  type = 'Exodiff'
  input = 'axisymm_plane_strain_finite.i'
  exodiff = 'axisymm_plane_strain_finite_out.e'
  design = 'source/materials/ComputeAxisymmetric1DFiniteStrain.md'
  requirement = 'The ComputeAxisymmetric1DFiniteStrain class shall compute the elastic stress for a 1D axisymmetric incremental finite strain formulation under a combination of applied tensile displacement and thermal expansion loading using the SolidMechanics/QuasiStatic Physics.'
[../]

[./axisymm_gps_finite]
  type = 'Exodiff'
  input = 'axisymm_gps_finite.i'
  exodiff = 'axisymm_gps_finite_out.e'
  design = 'source/materials/ComputeAxisymmetric1DFiniteStrain.md'
  requirement = 'The ComputeAxisymmetric1DFiniteStrain class shall, under generalized plane strain conditions, compute the elastic stress for a 1D axisymmetric incremental finite strain formulation under a combination of applied tensile displacement and thermal expansion loading.'
[../]

[./1d_finite_rz_coord_axis_error]
  type = 'RunException'
  prereq = axisymmetric_gps_finite
  input = 'axisymm_gps_finite.i'
  cli_args = 'Problem/rz_coord_axis=X'
  expect_err = 'rz_coord_axis=Y is the only supported option for StressDivergenceRZTensors'
  design = 'source/materials/ComputeAxisymmetric1DFiniteStrain.md'
  requirement = 'The StressDivergenceRZTensors class shall generate an error if used with Problem/rz_coord_axis set to anything other than Y'
[../]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false Materials/stress/type=ComputeLinearElasticStress'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true Materials/stress/type=ComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[./rspherical_incremental_small_elastic-noad]
  type = 'Exodiff'
  input = 'rspherical_incremental_small_elastic-noad.i'
  exodiff = 'rspherical_incremental_small_elastic_out.e'
  requirement = 'We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation. (non-AD reference)'
  design = 'ComputeRSphericalIncrementalStrain.md'
[../]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false Materials/stress/type=ComputeLinearElasticStress'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true Materials/stress/type=ComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[./elastic_patch]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#458'
[../]

[./elastic_patch_incremental_small]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584'
[../]

[./elastic_patch_incremental_small_no_disp_mesh]
  prereq = elastic_patch_total_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Mesh/use_displaced_mesh=false Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584 #12580'
[../]

[./elastic_patch_Bbar]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'elastic_patch'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[./elastic_patch_2Procs]
  type = Exodiff
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  min_parallel = 2
  prereq = 'elastic_patch_Bbar'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when running on 2 processors in parallel.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#458'
[../]

[./elastic_patch_2Procs_Bbar]
  type = Exodiff
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  min_parallel = 2
  prereq = 'elastic_patch_2Procs'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[./elastic_patch_quadratic]
  type = Exodiff
  input = 'elastic_patch_quadratic.i'
  exodiff = 'elastic_patch_quadratic_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular 20-noded quadratic hexes.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#620'
[../]

[new]
  type = 'Exodiff'
  input = 'finite_strain_elastic_new_test.i'
  exodiff = 'finite_strain_elastic_new_test_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.'
[]

[new_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_elastic_new_test.i'
  exodiff = 'finite_strain_elastic_new_test_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'new'
  issues = '#8235 #4716'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.'
[]

[rotation_new]
  type = 'Exodiff'
  input = 'elastic_rotation_test.i'
  exodiff = 'elastic_rotation_test_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the QuasiStatic SolidMechanics Physics.'
[]

[rotation_new_Bbar]
  type = 'Exodiff'
  input = 'elastic_rotation_test.i'
  exodiff = 'elastic_rotation_test_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'rotation_new'
  issues = '#4716 #8235'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the volumetric locking correction b-bar formulation.'
[]

[eigen_sol]
  type = 'Exodiff'
  input = 'finite_strain_elastic_eigen_sol.i'
  exodiff = 'finite_strain_elastic_eigen_sol_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.'
[]

[eigen_sol_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_elastic_eigen_sol.i'
  exodiff = 'finite_strain_elastic_eigen_sol_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'eigen_sol'
  issues = '#8235 #4716'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.'
[]

[stress_errorcheck]
  type = 'RunException'
  input = 'finite_strain_stress_errorcheck.i'
  expect_err = 'This linear elastic stress calculation only works for small strains; use ComputeFiniteStrainElasticStress for simulations using incremental and finite strains.'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeLinearElasticStress.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeLinearElasticStress class shall generate an error if a user attempts to run a problem using ComputeLinearElasticStress with a finite strain formulation.'
[]

[./3d_isotropic]
  type = 'Exodiff'
  input = '3d_bar_orthotropic.i'
  exodiff = '3d_bar_orthotropic_out.e'
  issues = '#16016'
  design = '/ComputeFiniteStrainElasticStress.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   complex strain state simulation in 3D using an orhotropic filling with isotropic properties.'
[../]

[./3d_orthotropic_isotropic]
  type = 'Exodiff'
  input = '3d_bar_orthotropic.i'
  exodiff = '3d_bar_orthotropic_out.e'
  cli_args = "Materials/elasticity_tensor/fill_method=symmetric_isotropic_E_nu Materials/elasticity_tensor/C_ijkl='2.0e5 0.4'"
  issues = '#16016'
  design = '/ComputeFiniteStrainElasticStress.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   complex strain state simulation in 3D using an orhotropic filling with isotropic properties.'
  custom_cmp = ortho.cmp
[../]

[./3d_bar_orthotropic_90deg_rotation]
  type = 'Exodiff'
  input = '3d_bar_orthotropic_90deg_rotation.i'
  exodiff = '3d_bar_orthotropic_90deg_rotation_out.e'
  issues = '#16016'
  design = '/ComputeFiniteStrainElasticStress.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 90 degrees and retrieve
                   the proper displacement after being solicited by a pressure boundary condition.'
  custom_cmp = ortho.cmp
[../]

[./3d_bar_orthotropic_90deg_rotation_ad]
  type = 'Exodiff'
  input = '3d_bar_orthotropic_90deg_rotation_ad.i'
  exodiff = '3d_bar_orthotropic_90deg_rotation_ad_out.e'
  issues = '#16016'
  design = '/ComputeFiniteStrainElasticStress.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 90 degrees and retrieve
                   the proper displacement after being solicited by a pressure boundary condition when automatic differentiation is used.'
  custom_cmp = ortho.cmp
[../]

[./3d_bar_orthotropic_full_rotation]
  type = 'Exodiff'
  input = '3d_bar_orthotropic_full_rotation.i'
  exodiff = '3d_bar_orthotropic_full_rotation_out.e'
  issues = '#16016'
  design = '/ComputeFiniteStrainElasticStress.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 360 degrees and retrieve
                   the proper displacement after being solicited by a pressure boundary condition.'
  heavy = true
  custom_cmp = ortho.cmp
[../]

[./3d_bar_orthotropic_full_rotation_ad]
  type = 'Exodiff'
  input = '3d_bar_orthotropic_full_rotation_ad.i'
  exodiff = '3d_bar_orthotropic_full_rotation_ad_out.e'
  issues = '#16016'
  design = '/ComputeFiniteStrainElasticStress.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to rotate an orthotropic beam-like element 360 degrees and retrieve
                   the proper displacement after being solicited by a pressure boundary condition when automatic differentiation is used.'
  heavy = true
  custom_cmp = ortho.cmp
[../]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false Materials/stress/type=ComputeLinearElasticStress'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true Materials/stress/type=ComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[./3D_RZ_finitestrain]
  type = Exodiff
  input = '3D-RZ_finiteStrain_test.i'
  exodiff = '3D-RZ_finiteStrain_test_out.e'
  valgrind = 'HEAVY'
  heavy = true
  abs_zero = 1e-5
  rel_err = 3E-3
  design = 'syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The QuasiStatic SolidMechanics Physics shall calculate the elastic stress and strain response for a 3D pressurized hollow cylinder with a large strain incremental strain formulation.'
[../]

[two_block_base_name]
  type = Exodiff
  input = "two_block_base_name.i"
  exodiff = "two_block_base_name_out.e"
  issues = "#13860"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall support changing the base name when creating a consistent strain calculator material and stress divergence kernel and shall generate different sets of outputs for different mesh subblocks with the appropriate base name."
[]

[two_block_new]
  type = Exodiff
  input = "two_block_new.i"
  exodiff = "two_block_new_out.e"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall create a consistent strain calculator material and stress divergence kernel and shall generate different sets of outputs for different mesh subblocks."
[]

[two_block]
  type = Exodiff
  input = "two_block.i"
  exodiff = "two_block_out.e"
  cli_args = "Physics/SolidMechanics/QuasiStatic/block1/block=1"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks requesting different strain formulations."
[]

[two_block_lagrangian]
  type = Exodiff
  input = "two_block_lagrangian.i"
  exodiff = "two_block_lagrangian_out.e"
  cli_args = "Physics/SolidMechanics/QuasiStatic/block1/block=1"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks requesting different strain formulations with the new kernel system."
[]

[two_block.error_unrestricted]
  type = RunException
  input = "two_block.i"
  expect_err = "No SolidMechanics/QuasiStatic action can be block unrestricted if more than one SolidMechanics/QuasiStatic action is specified."
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall error if an input file does not specify block restrictions for the MasterAction in input files with more than one instance of the MasterAction block."
[]

[two_block.error_overlapping]
  type = RunException
  input = "two_block.i"
  cli_args = "Physics/SolidMechanics/QuasiStatic/block1/block=2"
  expect_err = "The block restrictions in the SolidMechanics/QuasiStatic actions must be non-overlapping."
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall error if an input file specifies overlapping block restrictions for the MasterAction in input files with more than one instance of the MasterAction block."
[]

[no_block]
  type = RunException
  input = "no_block.i"
  cli_args = "--error"
  expect_err = "Common parameters are supplied, but not used in"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall warn if global Master action parameters are supplied but no Master action subblock have been added."
[]

[two_coord]
  type = Exodiff
  input = "two_coord.i"
  exodiff = "two_coord_out.e"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks using different coordinate systems."
[]

[two_coord.error_different_coords]
  type = RunException
  input = "two_coord.i"
  cli_args = "Physics/SolidMechanics/QuasiStatic/active=error"
  expect_err = "The SolidMechanics action requires all subdomains to have the same coordinate system."
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall error if an input file assigns the same QuasiStatic SolidMechanics Physics block to mesh blocks with different coordinate systems."
[]

[action_eigenstrain]
  type = RunApp
  input = "action_eigenstrain.i"
  expect_out = "solid: eigenstrain1, eigenstrain2"
  match_literal = true
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console."
[]

[action_multi_eigenstrain]
  type = RunApp
  input = "action_multi_eigenstrain.i"
  expect_out = "block1: eigenstrain1\n.*\nblock2: eigenstrain2\n"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console."
[]

[action_multi_eigenstrain_same_conditions]
  type = RunApp
  input = "action_multi_eigenstrain_same_conditions.i"
  expect_out = "block1: eigenstrain\n.*\nblock2: eigenstrain\n"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console."
[]

[ad_converter_action_multi_eigenstrain]
  type = RunApp
  input = "ad_converter_action_multi_eigenstrain.i"
  expect_out = "block1: eigenstrain1\n.*\nblock2: eigenstrain2\n"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console."
[]

[reduced_eigenstrain_action]
  type = RunApp
  input = "reduced_eigenstrain_action.i"
  expect_out = "all: reduced_eigenstrain"
  match_literal = true
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console."
[]

[composite_eigenstrain]
  type = RunApp
  input = "composite_eigenstrain.i"
  expect_out = "solid: eigenstrain"
  match_literal = true
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall extract eigenstrain names from material classes and correctly output these names to the console."
[]

[material_output_order.empty]
  type = RunApp
  input = "material_output_order.i"
  expect_out = "all: CONSTANT CONSTANT CONSTANT\n.*\nall: MONOMIAL MONOMIAL MONOMIAL\n"
  cli_args = "Physics/SolidMechanics/QuasiStatic/verbose=true"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall determine the necessary orders and families to apply to material outputs."
[]

[material_output_order.single]
  type = RunApp
  input = "material_output_order.i"
  expect_out = "all: FIRST FIRST FIRST\n.*\nall: MONOMIAL MONOMIAL MONOMIAL\n"
  cli_args = "Physics/SolidMechanics/QuasiStatic/verbose=true Physics/SolidMechanics/QuasiStatic/material_output_order=FIRST"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall apply a single given output order to all output variables."
[]

[material_output_order.family_single]
  type = RunApp
  input = "material_output_order.i"
  expect_out = "all: FIRST FIRST FIRST\n.*\nall: LAGRANGE LAGRANGE LAGRANGE\n"
  cli_args = "Physics/SolidMechanics/QuasiStatic/verbose=true Physics/SolidMechanics/QuasiStatic/material_output_order=FIRST Physics/SolidMechanics/QuasiStatic/material_output_family=LAGRANGE"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall apply a single given output family to all output variables."
[]

[material_output_order.error1]
  type = RunException
  input = "material_output_order.i"
  cli_args = 'Physics/SolidMechanics/QuasiStatic/material_output_family="LAGRANGE MONOMIAL"'
  expect_err = "The number of families assigned to material outputs must be: 0 to be assigned MONOMIAL; 1 to assign all outputs the same value, or the same size as the number of generate outputs listed."
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall error if an the material outputs and or families do not match the number of material outputs."
[]

[material_output_first_lagrange_manual]
  type = Exodiff
  input = "material_output_first_lagrange_manual.i"
  exodiff = "material_output_first_lagrange_manual_out.e"
  max_parallel = 1
  max_threads = 1
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall determine the necessary orders and families to apply to material outputs."
[]

[material_output_first_lagrange_automatic]
  type = Exodiff
  input = "material_output_first_lagrange_automatic.i"
  exodiff = "material_output_first_lagrange_automatic_out.e"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall determine the necessary orders and families to apply to material outputs."
[]

[custom_output]
  type = Exodiff
  input = "custom_output.i"
  exodiff = "custom_output_out.e"
  design = "syntax/Physics/SolidMechanics/QuasiStatic/index.md"
  requirement = "The QuasiStatic SolidMechanics Physics shall permit scalar quantity output from arbitrary tensors."
[]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[smallStrain_1DSphere-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[smallStrain_1DSphere_incremental-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[finiteStrain_1DSphere_hollow-jac]
  type = 'PetscJacobianTester'
  input = 'finiteStrain_1DSphere_hollow.i'
  run_sim = 'True'
  difference_tol = 1
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[./two_block_new]
  type = Exodiff
  input = 'two_block_new.i'
  exodiff = 'two_block_new_out.e'
  requirement = 'The QuasiStatic SolidMechanics Physics shall create a consistent strain calculator material and stress divergence kernel and shall generate different sets of outputs for different mesh subblocks.'
[../]

[./two_block]
  type = Exodiff
  input = 'two_block.i'
  exodiff = 'two_block_out.e'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/block1/block=1'
  requirement = 'The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks requesting different strain formulations.'
[../]

[./error_unrestricted]
  type = RunException
  input = 'two_block.i'
  expect_err = 'No SolidMechanics/QuasiStatic action can be block unrestricted if more than one SolidMechanics/QuasiStatic action is specified.'
  prereq = 'two_block'
  requirement = 'The QuasiStatic SolidMechanics Physics shall error if an input file does not specify block restrictions for the MasterAction in input files with more than one instance of the MasterAction block.'
[../]

[./error_overlapping]
  type = RunException
  input = 'two_block.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/block1/block=2'
  expect_err = 'The block restrictions in the SolidMechanics/QuasiStatic actions must be non-overlapping.'
  prereq = 'error_unrestricted'
  requirement = 'The QuasiStatic SolidMechanics Physics shall error if an input file specifies overlapping block restrictions for the MasterAction in input files with more than one instance of the MasterAction block.'
[../]

[./two_coord]
  type = Exodiff
  input = 'two_coord.i'
  exodiff = 'two_coord_out.e'
  rel_err = 1e-5
  requirement = 'The QuasiStatic SolidMechanics Physics shall create different sets of consistent strain calculator material and stress divergence kernel pairs for different mesh subblocks using different coordinate systems.'
[../]

[./error_coord]
  type = RunException
  input = 'two_coord.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/active=error'
  expect_err = 'The SolidMechanics action requires all subdomains to have the same coordinate system.'
  prereq = 'two_coord'
  requirement = 'The QuasiStatic SolidMechanics Physics shall error if an input file assigns the same QuasiStatic SolidMechanics Physics block to mesh blocks with different coordinate systems.'
[../]

[./two_block-jac]
  type = 'PetscJacobianTester'
  input = 'two_block.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  cli_args = 'Physics/SolidMechanics/QuasiStatic/block1/block=1'
  requirement = 'The Jacobian for the automatic differentiation in the two_block testproblem shall be perfect'
[../]

[./two_block_no_action-jac]
  type = 'PetscJacobianTester'
  input = 'two_block_no_action.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  requirement = 'The Jacobian for the automatic differentiation in the two_block testproblem shall be perfect (non action test case)'
[../]

[./two_block_new-jac]
  type = 'PetscJacobianTester'
  input = 'two_block_new.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  requirement = 'The Jacobian for the automatic differentiation in the two_block_new problem shall be perfect'
[../]

[./two_coord-jac]
  type = 'PetscJacobianTester'
  input = 'two_coord.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  requirement = 'The Jacobian for the automatic differentiation two_coord problem shall be perfect'
[../]

[./test]
  type = 'Exodiff'
  input = 'anisotropic_patch_test.i'
  exodiff = 'anisotropic_patch_test_out.e'
  scale_refine = 1
  issues = '#4716 #7555'
  design = 'source/materials/ComputeLinearElasticStress.md source/materials/ComputeSmallStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The mechanics system shall be capable of accurately computing the elastic response of an anisotropic elastic material where 6 components of a symmetric elasticity tensor are output on an irregular patch of elements with total small strain assumptions'
[../]

[new]
  type = 'Exodiff'
  input = 'finite_strain_elastic_new_test.i'
  exodiff = 'finite_strain_elastic_new_test_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.'
[]

[rotation_new]
  type = 'Exodiff'
  input = 'elastic_rotation_test.i'
  exodiff = 'elastic_rotation_test_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the QuasiStatic SolidMechanics Physics.'
[]

[eigen_sol]
  type = 'Exodiff'
  input = 'finite_strain_elastic_eigen_sol.i'
  exodiff = 'finite_strain_elastic_eigen_sol_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.'
[]

[stress_errorcheck]
  type = 'RunException'
  input = 'finite_strain_stress_errorcheck.i'
  expect_err = 'This linear elastic stress calculation only works for small strains; use ComputeFiniteStrainElasticStress for simulations using incremental and finite strains.'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeLinearElasticStress.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeLinearElasticStress class shall generate an error if a user attempts to run a problem using ComputeLinearElasticStress with a finite strain formulation.'
[]

[free_expansion_abs_ref]
  type = 'Exodiff'
  input = 'free_expansion_abs_ref.i'
  exodiff = 'free_expansion_abs_ref_out.e'
  requirement = 'The tensor mechanics action shall set up the mechanics kernels with the appropriate options to accumulate absolute values of the residual to a tag vector usable for relative convergence checks.'
  design = 'Physics/SolidMechanics/QuasiStatic/index.md ReferenceResidualProblem.md'
[]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false Materials/stress/type=ComputeLinearElasticStress'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true Materials/stress/type=ComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.
'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[smallStrain_1DSphere-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[smallStrain_1DSphere_incremental-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[finiteStrain_1DSphere_hollow-jac]
  type = 'PetscJacobianTester'
  input = 'finiteStrain_1DSphere_hollow.i'
  run_sim = 'True'
  difference_tol = 1
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[./plane_strain_xy_small]
  type = Exodiff
  input = 'planestrain_xy.i'
  exodiff = 'planestrain_xy_small_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the x-y plane for small strain"
  design = 'source/materials/ComputePlaneSmallStrain.md'
  issues = '#11257'
[../]

[./plane_strain_xz_small]
  type = Exodiff
  input = 'planestrain_xz.i'
  exodiff = 'planestrain_xz_small_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the x-z plane for small strain"
  design = 'source/materials/ComputePlaneSmallStrain.md'
  issues = '#11257'
[../]

[./plane_strain_yz_small]
  type = Exodiff
  input = 'planestrain_yz.i'
  exodiff = 'planestrain_yz_small_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the y-z plane for small strain"
  design = 'source/materials/ComputePlaneSmallStrain.md'
  issues = '#11257'
[../]

[./plane_strain]
  type = Exodiff
  input = 'planestrain.i'
  exodiff = 'planestrain_out.e'
  abs_zero = 1e-6
  compiler = 'CLANG GCC'
  design = 'source/materials/ComputePlaneSmallStrain.md'
  requirement = 'The ComputePlaneSmallStrain class shall compute the elastic stress and strain for a planar square geometry under tension using a total small plane strain formulation.'
[../]

[./plane_strain_Bbar]
  type = Exodiff
  input = 'planestrain.i'
  exodiff = 'planestrain_out.e'
  abs_zero = 5e-6
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'plane_strain'
  design = 'source/materials/ComputePlaneSmallStrain.md VolumetricLocking.md'
  requirement = 'The ComputePlaneSmallStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a total small plane strain formulation.'
[../]

[plane_strain]
  type = 'Exodiff'
  input = 'plane_strain.i'
  exodiff = 'plane_strain_out.e'
  custom_cmp = 'plane_strain.exodiff'
  requirement = 'The system shall support a traditional plane strain mechanics solution'
  design = 'ComputePlaneSmallStrain.md'
[]

[plane_strain_prescribed]
  type = 'Exodiff'
  input = 'plane_strain_prescribed.i'
  exodiff = 'plane_strain_prescribed_out.e'
  custom_cmp = 'plane_strain.exodiff'
  requirement = 'The system shall support a traditional plane strain mechanics solution where the out-of-plane strain is prescribed'
  design = 'ComputePlaneSmallStrain.md'
[]

[generalized_plane_strain_small]
  type = 'Exodiff'
  input = 'generalized_plane_strain_small.i'
  exodiff = 'generalized_plane_strain_small_out.e'
  custom_cmp = 'generalized.exodiff'
  requirement = 'The system shall support a generalized plane strain mechanics solution'
  design = 'ComputePlaneSmallStrain.md'
[]

[generalized_plane_strain_ref_resid_absolute_value_vector_tags]
  type = 'Exodiff'
  input = 'generalized_plane_strain_ref_resid.i'
  exodiff = 'generalized_plane_strain_ref_resid_out.e'
  custom_cmp = 'generalized.exodiff'
  requirement = 'The system shall support a generalized plane strain mechanics solution using the reference residual approach to check solution convergence of the field and scalar variables when the reference vector is constructed using absolute value vector tags.'
  design = 'ComputePlaneSmallStrain.md'
[]

[generalized_plane_strain_ref_resid_extra_vector_tags]
  prereq = generalized_plane_strain_ref_resid_absolute_value_vector_tags
  type = 'Exodiff'
  input = 'generalized_plane_strain_ref_resid.i'
  cli_args = "Physics/SolidMechanics/QuasiStatic/all/absolute_value_vector_tags='' Physics/SolidMechanics/QuasiStatic/all/extra_vector_tags='ref' Outputs/file_base=generalized_plane_strain_ref_resid_extra_vector_tags_out"
  exodiff = 'generalized_plane_strain_ref_resid_extra_vector_tags_out.e'
  custom_cmp = 'generalized.exodiff'
  requirement = 'The system shall support a generalized plane strain mechanics solution using the reference residual approach to check solution convergence of the field and scalar variables when the reference vector is constructed using unbalanced kernel contributions.'
  design = 'ComputePlaneSmallStrain.md'
[]

[./plane_strain_xy_incremental]
  type = Exodiff
  input = 'planestrain_xy.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/plane_strain/incremental=true
                Materials/elastic_stress/type=ComputeStrainIncrementBasedStress
              Outputs/file_base=planestrain_xy_incremental_out'
  exodiff = 'planestrain_xy_incremental_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the x-y plane for incremental strain"
  design = 'source/materials/ComputePlaneIncrementalStrain.md'
  issues = '#11257'
[../]

[./plane_strain_xz_incremental]
  type = Exodiff
  input = 'planestrain_xz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/plane_strain/incremental=true
                Materials/elastic_stress/type=ComputeStrainIncrementBasedStress
                Outputs/file_base=planestrain_xz_incremental_out'
  exodiff = 'planestrain_xz_incremental_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the x-z plane for incremental strain"
  design = 'source/materials/ComputePlaneIncrementalStrain.md'
  issues = '#11257'
[../]

[./plane_strain_yz_incremental]
  type = Exodiff
  input = 'planestrain_yz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/plane_strain/incremental=true
                Materials/elastic_stress/type=ComputeStrainIncrementBasedStress
                Outputs/file_base=planestrain_yz_incremental_out'
  exodiff = 'planestrain_yz_incremental_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the y-z plane for incremental strain"
  design = 'source/materials/ComputePlaneIncrementalStrain.md'
  issues = '#11257'
[../]

[generalized_plane_strain_increment]
  type = 'Exodiff'
  input = 'generalized_plane_strain_increment.i'
  exodiff = 'generalized_plane_strain_increment_out.e'
  custom_cmp = 'generalized.exodiff'
  requirement = 'The system shall support a generalized plane strain mechanics solution with incremental strain'
  design = 'ComputePlaneIncrementalStrain.md'
[]

[./plane_strain_xy_finite]
  type = Exodiff
  input = 'planestrain_xy.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/plane_strain/strain=FINITE
                Materials/elastic_stress/type=ComputeFiniteStrainElasticStress
                Outputs/file_base=planestrain_xy_finite_out'
  exodiff = 'planestrain_xy_finite_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the x-y plane for finite strain"
  design = 'source/materials/ComputePlaneFiniteStrain.md'
  issues = '#11257'
[../]

[./plane_strain_xz_finite]
  type = Exodiff
  input = 'planestrain_xz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/plane_strain/strain=FINITE
                Materials/elastic_stress/type=ComputeFiniteStrainElasticStress
                Outputs/file_base=planestrain_xz_finite_out'
  exodiff = 'planestrain_xz_finite_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the x-z plane for finite strain"
  design = 'source/materials/ComputePlaneFiniteStrain.md'
  issues = '#11257'
[../]

[./plane_strain_yz_finite]
  type = Exodiff
  input = 'planestrain_yz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/plane_strain/strain=FINITE
                Materials/elastic_stress/type=ComputeFiniteStrainElasticStress
                Outputs/file_base=planestrain_yz_finite_out'
  exodiff = 'planestrain_yz_finite_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve plane strain in the y-z plane for finite strain"
  design = 'source/materials/ComputePlaneFiniteStrain.md'
  issues = '#11257'
[../]

[./finite_planestrain]
  type = Exodiff
  input = 'finite_planestrain.i'
  exodiff = 'finite_planestrain_out.e'
  abs_zero = 1e-9
  compiler = 'CLANG GCC'
  design = 'source/materials/ComputePlaneFiniteStrain.md'
  requirement = 'The ComputePlaneFiniteStrain class shall compute the elastic stress and strain for a planar square geometry under tension using a finite incremental plane strain formulation.'
[../]

[./finite_planestrain_Bbar]
  type = Exodiff
  input = 'finite_planestrain.i'
  exodiff = 'finite_planestrain_out.e'
  abs_zero = 1e-9
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'finite_planestrain'
  design = 'source/materials/ComputePlaneFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ComputePlaneFiniteStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a finite incremental plane strain formulation.'
[../]

[generalized_plane_strain_finite]
  type = 'Exodiff'
  input = 'generalized_plane_strain_finite.i'
  exodiff = 'generalized_plane_strain_finite_out.e'
  custom_cmp = 'generalized.exodiff'
  requirement = 'The system shall support a generalized plane strain mechanics solution with finite strain'
  design = 'ComputePlaneFiniteStrain.md'
[]

[./gps_xy_small]
  type = Exodiff
  input = 'gps_xy.i'
  exodiff = 'gps_xy_small_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the x-y plane for small strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_xy_incremental]
  type = Exodiff
  input = 'gps_xy.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/generalized_plane_strain/incremental=true
                Materials/elastic_stress/type=ComputeStrainIncrementBasedStress
                Outputs/file_base=gps_xy_incremental_out'
  exodiff = 'gps_xy_incremental_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the x-y plane for incremental strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_xy_finite]
  type = Exodiff
  input = 'gps_xy.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/generalized_plane_strain/strain=FINITE
                Materials/elastic_stress/type=ComputeFiniteStrainElasticStress
              Postprocessors/react_z/use_displaced_mesh=true
                Outputs/file_base=gps_xy_finite_out'
  exodiff = 'gps_xy_finite_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the x-y plane for finite strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_xz_small]
  type = Exodiff
  input = 'gps_xz.i'
  exodiff = 'gps_xz_small_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the x-z plane for small strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_xz_incremental]
  type = Exodiff
  input = 'gps_xz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/generalized_plane_strain/incremental=true
                Materials/elastic_stress/type=ComputeStrainIncrementBasedStress
                Outputs/file_base=gps_xz_incremental_out'
  exodiff = 'gps_xz_incremental_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the x-z plane for incremental strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_xz_finite]
  type = Exodiff
  input = 'gps_xz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/generalized_plane_strain/strain=FINITE
                Materials/elastic_stress/type=ComputeFiniteStrainElasticStress
                Postprocessors/react_y/use_displaced_mesh=true
                Outputs/file_base=gps_xz_finite_out'
  exodiff = 'gps_xz_finite_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the x-z plane for finite strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_yz_small]
  type = Exodiff
  input = 'gps_yz.i'
  exodiff = 'gps_yz_small_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the y-z plane for small strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_yz_incremental]
  type = Exodiff
  input = 'gps_yz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/generalized_plane_strain/incremental=true
                Materials/elastic_stress/type=ComputeStrainIncrementBasedStress
                Outputs/file_base=gps_yz_incremental_out'
  exodiff = 'gps_yz_incremental_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the y-z plane for incremental strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./gps_yz_finite]
  type = Exodiff
  input = 'gps_yz.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/generalized_plane_strain/strain=FINITE
                Materials/elastic_stress/type=ComputeFiniteStrainElasticStress
                Postprocessors/react_x/use_displaced_mesh=true
                Outputs/file_base=gps_yz_finite_out'
  exodiff = 'gps_yz_finite_out.e'
  abs_zero = 1e-7
  requirement = "The tensor mechanics strain calculators shall solve generalized plane strain in the y-z plane for finite strain"
  design = 'modules/solid_mechanics/generalized_plane_strain.md'
  issues = '#11257'
[../]

[./planestrain_jacobian_xy]
  type = 'PetscJacobianTester'
  input = 'planestrain_jacobian_testing_xy.i'
  ratio_tol = 1E-10
  difference_tol = 1E10
  requirement = "The Jacobian for plane strain in the x-y plane shall be correct"
  design = 'source/kernels/StressDivergenceTensors.md'
  issues = '#11257'
[../]

[./planestrain_jacobian_xz]
  type = 'PetscJacobianTester'
  input = 'planestrain_jacobian_testing_xz.i'
  ratio_tol = 1E-10
  difference_tol = 1E10
  requirement = "The Jacobian for plane strain in the x-z plane shall be correct"
  design = 'source/kernels/StressDivergenceTensors.md'
  issues = '#11257'
[../]

[./planestrain_jacobian_yz]
  type = 'PetscJacobianTester'
  input = 'planestrain_jacobian_testing_yz.i'
  ratio_tol = 1E-10
  difference_tol = 1E10
  requirement = "The Jacobian for plane strain in the y-z plane shall be correct"
  design = 'source/kernels/StressDivergenceTensors.md'
  issues = '#11257'
[../]

[./gps_jacobian_xy]
  type = 'PetscJacobianTester'
  input = 'gps_jacobian_testing_xy.i'
  ratio_tol = 1E-10
  difference_tol = 1E10
  requirement = "The Jacobian for generalized plane strain in the x-y plane shall be correct"
  design = 'source/kernels/StressDivergenceTensors.md'
  issues = '#11257'
[../]

[./gps_jacobian_xz]
  type = 'PetscJacobianTester'
  input = 'gps_jacobian_testing_xz.i'
  ratio_tol = 1E-10
  difference_tol = 1E10
  requirement = "The Jacobian for generalized plane strain in the x-z plane shall be correct"
  design = 'source/kernels/StressDivergenceTensors.md'
  issues = '#11257'
[../]

[./gps_jacobian_yz]
  type = 'PetscJacobianTester'
  input = 'gps_jacobian_testing_yz.i'
  ratio_tol = 1E-10
  difference_tol = 1E10
  requirement = "The Jacobian for generalized plane strain in the y-z plane shall be correct"
  design = 'source/kernels/StressDivergenceTensors.md'
  issues = '#11257'
[../]

[./plane_strain_Bbar]
  type = Exodiff
  input = 'planestrain.i'
  exodiff = 'planestrain_out.e'
  abs_zero = 5e-6
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'plane_strain'
  design = 'source/materials/ComputePlaneSmallStrain.md VolumetricLocking.md'
  requirement = 'The ComputePlaneSmallStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a total small plane strain formulation.'
[../]

[./finite_planestrain_Bbar]
  type = Exodiff
  input = 'finite_planestrain.i'
  exodiff = 'finite_planestrain_out.e'
  abs_zero = 1e-9
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'finite_planestrain'
  design = 'source/materials/ComputePlaneFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ComputePlaneFiniteStrain class shall compute the same result for elastic strain and stress when using the B-bar volumentric locking correction as computed without the volumetric locking correction for a planar geometry using a finite incremental plane strain formulation.'
[../]

[./axisym_resid_Bbar]
  type = Exodiff
  input = '2D-RZ_finiteStrain_resid.i'
  exodiff = '2D-RZ_finiteStrain_resid_bbar_out.e'
  use_old_floor = true
  abs_zero = 1e-8
  compiler = 'GCC CLANG'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=2D-RZ_finiteStrain_resid_bbar_out'
  prereq = 'axisym_resid'
  design = 'source/materials/ComputeAxisymmetricRZFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.'
[../]

[./axisymmetric_vlc_centerline_pp]
  type = CSVDiff
  input = '2D-RZ_centerline_VLC.i'
  csvdiff = '2D-RZ_centerline_VLC_out.csv'
  design = 'VolumetricLocking.md source/postprocessors/AxisymmetricCenterlineAverageValue.md'
  issues = '#12437 #10866'
  requirement = 'The volumetric locking correction option in ComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.'
[../]

[./axisym_resid_Bbar]
  type = Exodiff
  input = '2D-RZ_finiteStrain_resid.i'
  exodiff = '2D-RZ_finiteStrain_resid_bbar_out.e'
  use_old_floor = true
  abs_zero = 1e-8
  compiler = 'GCC CLANG'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=2D-RZ_finiteStrain_resid_bbar_out'
  prereq = 'axisym_resid'
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.'
[../]

[./axisymmetric_vlc_centerline_pp]
  type = CSVDiff
  input = '2D-RZ_centerline_VLC.i'
  csvdiff = '2D-RZ_centerline_VLC_out.csv'
  design = 'VolumetricLocking.md source/postprocessors/AxisymmetricCenterlineAverageValue.md'
  issues = '#12437 #10866'
  requirement = 'The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.'
[../]

[./axisym_resid_Bbar-jac]
  type = PetscJacobianTester
  input = '2D-RZ_finiteStrain_resid.i'
  compiler = 'GCC CLANG'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  run_sim = 'True'
  ratio_tol = 5e-8
  difference_tol = 10
  issues = '#12650'
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction and shall produce perfect jacobians.'
[../]

[./axisymmetric_vlc_centerline_pp-jac]
  type = PetscJacobianTester
  input = '2D-RZ_centerline_VLC.i'
  cli_args = "Outputs/active='' Outputs/csv=false"
  run_sim = 'True'
  ratio_tol = 7e-8
  difference_tol = 1e4
  issues = '#12650'
  design = 'VolumetricLocking.md source/postprocessors/AxisymmetricCenterlineAverageValue.md'
  requirement = 'The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation and shall produce perfect jacobians.'
[../]

[./elastic_patch_Bbar]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'elastic_patch'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[./elastic_patch_2Procs_Bbar]
  type = Exodiff
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  min_parallel = 2
  prereq = 'elastic_patch_2Procs'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[new_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_elastic_new_test.i'
  exodiff = 'finite_strain_elastic_new_test_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'new'
  issues = '#8235 #4716'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.'
[]

[fake_plastic]
  type = 'Exodiff'
  input = 'finite_strain_fake_plastic.i'
  exodiff = 'finite_strain_fake_plastic_out.e'
  issues = '#9212 #7555'
  design = 'source/materials/ComputeMultiPlasticityStress.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the QuasiStatic SolidMechanics Physics.'
[]

[fake_plastic_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_fake_plastic.i'
  exodiff = 'finite_strain_fake_plastic_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'fake_plastic'
  issues = '#9212 #8235'
  design = 'source/materials/ComputeMultiPlasticityStress.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the volumetric locking correction b-bar formulation.'
[]

[rotation_new_Bbar]
  type = 'Exodiff'
  input = 'elastic_rotation_test.i'
  exodiff = 'elastic_rotation_test_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'rotation_new'
  issues = '#4716 #8235'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress based on a finite strain fomulation and then follow the stress as the mesh is rotated 90 degrees in accordance with Kamojjala et al.(2015) using the volumetric locking correction b-bar formulation.'
[]

[eigen_sol_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_elastic_eigen_sol.i'
  exodiff = 'finite_strain_elastic_eigen_sol_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'eigen_sol'
  issues = '#8235 #4716'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.'
[]

[./smallstrain_3D_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'finitestrain_3D'
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using small strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./incrementalstrain_3D_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallstrain_3D_Bbar'
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using incremental small strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./finitestrain_3D_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=FINITE
                Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalstrain_3D_Bbar'
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using finite strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./smallstrain_RZ_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'finitestrain_RZ'
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using small strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./incrementalstrain_RZ_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallstrain_RZ_Bbar'
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using incremental small strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./finitestrain_RZ_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=FINITE
                Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalstrain_RZ_Bbar'
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using finite strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./smallplanestrain_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneSmallStrain
                Materials/stress/type=ComputeLinearElasticStress
                GlobalParams/volumetric_locking_correction=true'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'finiteplanestrain'
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using small strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./incrementalplanestrain_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneIncrementalStrain
                Materials/stress/type=ComputeFiniteStrainElasticStress
                GlobalParams/volumetric_locking_correction=true'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallplanestrain_Bbar'
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using incremental small strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./finiteplanestrain_Bbar]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneFiniteStrain
                Materials/stress/type=ComputeFiniteStrainElasticStress
                GlobalParams/volumetric_locking_correction=true'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalplanestrain_Bbar'
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using finite strain and volumetric locking correction."
  design = "VolumetricLocking.md"
[../]

[./elastic_Bbar]
  type = 'CSVDiff'
  input = 'elastic_stress.i'
  cli_args = 'Kernels/SolidMechanics/volumetric_locking_correction=true Materials/strain/volumetric_locking_correction=true'
  csvdiff = 'elastic_stress_out.csv'
  prereq = 'elastic'
  requirement = "The ComputeDeformGradBasedStress class shall correctly compute the stress from lagrangian strain when volumetric locking correction is used."
  design = "source/materials/ComputeDeformGradBasedStress.md VolumetricLocking.md"
  issues = "#6604"
[../]

[./interface_Bbar]
  type = 'CSVDiff'
  input = 'volumetric_strain_interface.i'
  csvdiff = 'volumetric_strain_interface_out.csv'
  prereq = 'interface'
  cli_args = 'Kernels/SolidMechanics/volumetric_locking_correction=true Materials/strain/volumetric_locking_correction=true'
  requirement = "The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration when volumetric locking correction is used."
  design = "source/materials/ComputeVolumetricDeformGrad.md source/materials/VolumeDeformGradCorrectedStress.md VolumetricLocking.md"
  issues = "#6604"
[../]

[./vol_lock_2D]
  type = Exodiff
  input = '42_node.i'
  exodiff = '42_node_out.e'
  compiler = 'CLANG GCC'
  design = 'VolumetricLocking.md'
  requirement = 'The mechanics system shall correctly model the deformation of a 2D membrane with nearly incompressible material when volumetric locking correction is set to true.'
[../]

[./no_vol_lock_2D]
  type = Exodiff
  input = '42_node.i'
  exodiff = '42_node_no_vol_lock_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=false Outputs/file_base=42_node_no_vol_lock_out'
  prereq = 'vol_lock_2D'
  design = 'VolumetricLocking.md'
  requirement = 'The mechanics system shall correctly model the locking behavior of a 2D membrane with nearly incompressible material when volumetric locking correction is set to false.'
[../]

[./axisym_smallstrain]
  type = Exodiff
  input = '2D-RZ_test.i'
  exodiff = '2D-RZ_test_out.e'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ComputeLinearElasticStress'
  design = 'source/materials/ComputeAxisymmetricRZSmallStrain.md'
  requirement = 'The ComputeAxisymmetricRZSmallStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small total axisymmetric strain formulation.'
[../]

[./rz_small_elastic-noad]
  type = 'Exodiff'
  input = 'rz_small_elastic-noad.i'
  exodiff = 'rz_small_elastic_out.e'
  requirement = 'We shall be able to reproduce small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation. (non-AD reference)'
  design = 'ComputeAxisymmetricRZSmallStrain.md'
[../]

[./axisym_incremental_strain]
  type = Exodiff
  input = '2D-RZ_test.i'
  exodiff = '2D-RZ_incremental_strain_test_out.e'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ComputeFiniteStrainElasticStress
                Outputs/file_base=2D-RZ_incremental_strain_test_out'
  prereq = 'axisym_smallstrain'
  design = 'source/materials/ComputeAxisymmetricRZIncrementalStrain.md'
  requirement = 'The ComputeAxisymmetricRZIncrementalStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.'
[../]

[./rz_incremental_small_elastic-noad]
  type = 'Exodiff'
  input = 'rz_incremental_small_elastic-noad.i'
  exodiff = 'rz_incremental_small_elastic_out.e'
  requirement = 'We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation. (non-AD reference)'
  design = 'ComputeAxisymmetricRZIncrementalStrain.md'
[../]

[./axisym_finitestrain]
  type = Exodiff
  input = '2D-RZ_finiteStrain_test.i'
  exodiff = '2D-RZ_finiteStrain_test_out.e'
  rel_err = 5E-4
  design = 'source/materials/ComputeAxisymmetricRZFiniteStrain.md'
  requirement = 'The ComputeAxisymmetricRZFiniteStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.'
[../]

[./axisym_resid]
  type = Exodiff
  input = '2D-RZ_finiteStrain_resid.i'
  exodiff = '2D-RZ_finiteStrain_resid_out.e'
  use_old_floor = true
  abs_zero = 1e-8
  compiler = 'GCC CLANG'
  design = 'source/materials/ComputeAxisymmetricRZFiniteStrain.md'
  requirement = 'The ComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension.'
[../]

[./axisym_resid_Bbar]
  type = Exodiff
  input = '2D-RZ_finiteStrain_resid.i'
  exodiff = '2D-RZ_finiteStrain_resid_bbar_out.e'
  use_old_floor = true
  abs_zero = 1e-8
  compiler = 'GCC CLANG'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=2D-RZ_finiteStrain_resid_bbar_out'
  prereq = 'axisym_resid'
  design = 'source/materials/ComputeAxisymmetricRZFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.'
[../]

[./rz_finite_elastic-noad]
  type = 'Exodiff'
  input = 'rz_finite_elastic-noad.i'
  exodiff = 'rz_finite_elastic_out.e'
  requirement = 'We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation. (non-AD reference)'
  design = 'ComputeAxisymmetricRZFiniteStrain.md'
[../]

[./axisymmetric_vlc_centerline_pp]
  type = CSVDiff
  input = '2D-RZ_centerline_VLC.i'
  csvdiff = '2D-RZ_centerline_VLC_out.csv'
  design = 'VolumetricLocking.md source/postprocessors/AxisymmetricCenterlineAverageValue.md'
  issues = '#12437 #10866'
  requirement = 'The volumetric locking correction option in ComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.'
[../]

[./axisymmetric_vlc_centerline_pp]
  type = CSVDiff
  input = '2D-RZ_centerline_VLC.i'
  csvdiff = '2D-RZ_centerline_VLC_out.csv'
  design = 'VolumetricLocking.md source/postprocessors/AxisymmetricCenterlineAverageValue.md'
  issues = '#12437 #10866'
  requirement = 'The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation.'
[../]

[./axisymmetric_vlc_centerline_pp-jac]
  type = PetscJacobianTester
  input = '2D-RZ_centerline_VLC.i'
  cli_args = "Outputs/active='' Outputs/csv=false"
  run_sim = 'True'
  ratio_tol = 7e-8
  difference_tol = 1e4
  issues = '#12650'
  design = 'VolumetricLocking.md source/postprocessors/AxisymmetricCenterlineAverageValue.md'
  requirement = 'The volumetric locking correction option in ADComputeAxisymmetricRZFiniteStrain shall reinit material properties without inverting a zero tensor when called from a side postprocessor applied to the axis of rotation in an axisymmetric simulation and shall produce perfect jacobians.'
[../]

[test]
  type = 'Exodiff'
  input = 'test.i'
  exodiff = 'test_out.e'
  requirement = "The Tensor Mechanics system shall support transformations
    of a rank two tensor into cylindircal coordinates."
[]

[test_Bbar]
  type = 'Exodiff'
  input = 'test.i'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=test_bbar_out'
  exodiff = 'test_bbar_out.e'
  prereq = 'test'
  requirement = "The Tensor Mechanics system including volumetric locking
    correction shall support transformations of a rank two tensor into cylindircal coordinates."
[]

[test]
  type = 'Exodiff'
  input = 'test.i'
  exodiff = 'test_out.e'
  requirement = "The Tensor Mechanics system shall support transformations
    of a rank two tensor into cylindircal coordinates."
[]

[test_Bbar]
  type = 'Exodiff'
  input = 'test.i'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=test_bbar_out'
  exodiff = 'test_bbar_out.e'
  prereq = 'test'
  requirement = "The Tensor Mechanics system including volumetric locking
    correction shall support transformations of a rank two tensor into cylindircal coordinates."
[]

[./accumulate_aux]
  type = 'Exodiff'
  input = 'accumulate_aux.i'
  exodiff = 'accumulate_aux_out.e'
  max_parallel = 1 # This mesh only has a single element
  issues = '#7091'
  design = 'AccumulateAux.md'
  requirement = 'The system shall provide an aux kernel that accumulates the values of a given variable.'
[../]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[smallStrain_1DSphere-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[smallStrain_1DSphere_incremental-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[finiteStrain_1DSphere_hollow-jac]
  type = 'PetscJacobianTester'
  input = 'finiteStrain_1DSphere_hollow.i'
  run_sim = 'True'
  difference_tol = 1
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[./rspherical_small_elastic-noad]
  type = 'Exodiff'
  input = 'rspherical_small_elastic-noad.i'
  exodiff = 'rspherical_small_elastic_out.e'
  requirement = 'We shall be able to reproduce small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation. (non-AD reference)'
  design = 'ComputeRSphericalSmallStrain.md'
[../]

[smallStrain_1DSphere]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalSmallStrain class, called through the QuasiStatic SolidMechanics Physics action, shall compute the total linearized solution for the displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with total small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[smallStrain_1DSphere_incremental]
  type = Exodiff
  input = 'smallStrain_1DSphere.i'
  exodiff = 'smallStrain_1DSphere_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  prereq = 'smallStrain_1DSphere'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalIncrementalStrain class, called through the QuasiStatic SolidMechanics Physics, shall find the linearized incremental strain displacement of a solid isotropic elastic sphere with a pressure applied to the outer surface using a 1D spherical symmetric formulation with incremental small strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial and hoop stress.'
[]

[finiteStrain_1DSphere_hollow]
  type = Exodiff
  input = 'finiteStrain_1DSphere_hollow.i'
  exodiff = 'finiteStrain_1DSphere_hollow_out.e'
  compiler = 'CLANG GCC'
  issues = '#6256 #7555 #18876'
  requirement = 'The ComputeRSphericalFiniteStrain class, called through the QuasiStatic SolidMechanics Physics action, shall find the finite incremental strain displacement of a thick walled hollow isotropic elastic sphere under an applied load using a 1D spherical symmetric fomulation with incremental finite strain assumptions. The RankTwoSphericalComponent class, called through the QuasiStatic SolidMechanics Physics, shall output the spherical radial stress.'
[]

[smallStrain_1DSphere-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[smallStrain_1DSphere_incremental-jac]
  type = 'PetscJacobianTester'
  input = 'smallStrain_1DSphere.i'
  run_sim = 'True'
  difference_tol = 1e-5
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[finiteStrain_1DSphere_hollow-jac]
  type = 'PetscJacobianTester'
  input = 'finiteStrain_1DSphere_hollow.i'
  run_sim = 'True'
  difference_tol = 1
  issues = '#12650'
  requirement = 'The Jacobian for the AD small incremental strain elasticity problem with Pressure BC in spherical coordinates shall be perfect'
[]

[./test]
  type = 'Exodiff'
  input = 'anisotropic_patch_test.i'
  exodiff = 'anisotropic_patch_test_out.e'
  scale_refine = 1
  issues = '#4716 #7555'
  design = 'source/materials/ComputeLinearElasticStress.md source/materials/ComputeSmallStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The mechanics system shall be capable of accurately computing the elastic response of an anisotropic elastic material where 6 components of a symmetric elasticity tensor are output on an irregular patch of elements with total small strain assumptions'
[../]

[./elastic_patch_total_small]
  prereq = elastic_patch_incremental_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeSmallStrain Materials/stress/type=ComputeLinearElasticStress Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeSmallStrain.md ComputeLinearElasticStress.md'
  issues = '#12584'
[../]

[stress_errorcheck]
  type = 'RunException'
  input = 'finite_strain_stress_errorcheck.i'
  expect_err = 'This linear elastic stress calculation only works for small strains; use ComputeFiniteStrainElasticStress for simulations using incremental and finite strains.'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeLinearElasticStress.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeLinearElasticStress class shall generate an error if a user attempts to run a problem using ComputeLinearElasticStress with a finite strain formulation.'
[]

[./axisym_smallstrain]
  type = Exodiff
  input = '2D-RZ_test.i'
  exodiff = '2D-RZ_test_out.e'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Materials/stress/type=ADComputeLinearElasticStress'
  design = 'source/materials/ADComputeAxisymmetricRZSmallStrain.md'
  requirement = 'The ADComputeAxisymmetricRZSmallStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small total axisymmetric strain formulation.'
[../]

[./axisym_smallstrain-jac]
  type = PetscJacobianTester
  input = '2D-RZ_test.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
    Materials/stress/type=ADComputeLinearElasticStress'
  run_sim = 'True'
  heavy = true
  ratio_tol = 5e-8
  difference_tol = 1e7
  issues = '#12650'
  design = 'source/materials/ADComputeAxisymmetricRZSmallStrain.md'
  requirement = 'The ADComputeAxisymmetricRZSmallStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small total axisymmetric strain formulation and shall produce perfect jacobians.'
[../]

[./rz_small_elastic]
  type = 'Exodiff'
  input = 'rz_small_elastic.i'
  exodiff = 'rz_small_elastic_out.e'
  prereq = 'rz_small_elastic-noad'
  requirement = 'We shall be able to reproduce small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation.'
  design = 'ADComputeAxisymmetricRZSmallStrain.md'
[../]

[./rz_small_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'rz_small_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e0
  cli_args = '-mat_fd_type ds'
  requirement = 'The Jacobian for the AD small strain elasticity problem in cylindrical coordinates shall be perfect'
  design = 'ADComputeAxisymmetricRZSmallStrain.md'
[../]

[./axisym_incremental_strain]
  type = Exodiff
  input = '2D-RZ_test.i'
  exodiff = '2D-RZ_incremental_strain_test_out.e'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress
                Outputs/file_base=2D-RZ_incremental_strain_test_out'
  prereq = 'axisym_smallstrain'
  design = 'source/materials/ADComputeAxisymmetricRZIncrementalStrain.md'
  requirement = 'The ADComputeAxisymmetricRZIncrementalStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.'
[../]

[./axisym_incremental_strain-jac]
  type = PetscJacobianTester
  input = '2D-RZ_test.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Materials/stress/type=ADComputeFiniteStrainElasticStress'
  run_sim = 'True'
  ratio_tol = 5e-8
  heavy = true
  difference_tol = 1e7
  issues = '#12650'
  design = 'source/materials/ADComputeAxisymmetricRZIncrementalStrain.md'
  requirement = 'The ADComputeAxisymmetricRZIncrementalStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation and shall produce perfect jacobians.'
[../]

[./rz_incremental_small_elastic]
  type = 'Exodiff'
  input = 'rz_incremental_small_elastic.i'
  exodiff = 'rz_incremental_small_elastic_out.e'
  prereq = 'rz_incremental_small_elastic-noad'
  requirement = 'We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation.'
  design = 'ADComputeAxisymmetricRZIncrementalStrain.md'
[../]

[./rz_incremental_small_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'rz_incremental_small_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e0
  cli_args = '-mat_fd_type ds'
  requirement = 'The Jacobian for the AD incremental small strain elasticity problem in cylindrical coordinates shall be perfect'
  design = 'ADComputeAxisymmetricRZIncrementalStrain.md'
[../]

[./axisym_finitestrain]
  type = Exodiff
  input = '2D-RZ_finiteStrain_test.i'
  exodiff = '2D-RZ_finiteStrain_test_out.e'
  rel_err = 5E-4
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation.'
[../]

[./axisym_resid]
  type = Exodiff
  input = '2D-RZ_finiteStrain_resid.i'
  exodiff = '2D-RZ_finiteStrain_resid_out.e'
  use_old_floor = true
  abs_zero = 1e-8
  compiler = 'GCC CLANG'
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension.'
[../]

[./axisym_resid_Bbar]
  type = Exodiff
  input = '2D-RZ_finiteStrain_resid.i'
  exodiff = '2D-RZ_finiteStrain_resid_bbar_out.e'
  use_old_floor = true
  abs_zero = 1e-8
  compiler = 'GCC CLANG'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=2D-RZ_finiteStrain_resid_bbar_out'
  prereq = 'axisym_resid'
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction.'
[../]

[./axisym_finitestrain-jac]
  type = PetscJacobianTester
  input = '2D-RZ_finiteStrain_test.i'
  run_sim = 'True'
  heavy = true
  ratio_tol = 5e-8
  difference_tol = 1e7
  issues = '#12650'
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the mechanical response for a pressurized hollow cylinder with a small incremental axisymmetric strain formulation and shall produce perfect jacobians.'
[../]

[./axisym_resid-jac]
  type = PetscJacobianTester
  input = '2D-RZ_finiteStrain_resid.i'
  compiler = 'GCC CLANG'
  run_sim = 'True'
  ratio_tol = 5e-8
  difference_tol = 1e1
  issues = '#12650'
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension and shall produce perfect jacobians.'
[../]

[./axisym_resid_Bbar-jac]
  type = PetscJacobianTester
  input = '2D-RZ_finiteStrain_resid.i'
  compiler = 'GCC CLANG'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  run_sim = 'True'
  ratio_tol = 5e-8
  difference_tol = 10
  issues = '#12650'
  design = 'source/materials/ADComputeAxisymmetricRZFiniteStrain.md VolumetricLocking.md'
  requirement = 'The ADComputeAxisymmetricRZFiniteStrain class shall compute the reaction forces on the top surface of a cylinder which is loaded axially in tension when using the B-bar volumetric locking correction and shall produce perfect jacobians.'
[../]

[./rz_finite_elastic]
  type = 'Exodiff'
  input = 'rz_finite_elastic.i'
  exodiff = 'rz_finite_elastic_out.e'
  prereq = 'rz_finite_elastic-noad'
  requirement = 'We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in cylindrical coordinates using automatic differentiation.'
  design = 'ADComputeAxisymmetricRZFiniteStrain.md'
[../]

[./rz_finite_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'rz_finite_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e0
  requirement = 'The Jacobian for the AD finite strain elasticity problem in cylindrical coordinates shall be perfect'
  design = 'ADComputeAxisymmetricRZFiniteStrain.md'
[../]

[anis_mech_hill_tensor_creep_small_tiny_step_ts_limit_test]
  type = 'Exodiff'
  input = 'anis_mech_hill_tensor_creep_small_tiny_step_ts_limit_test.i'
  exodiff = 'anis_mech_hill_tensor_creep_small_tiny_step_ts_limit_test_out.e'
  min_parallel = 2
  custom_cmp = 'generalized.exodiff'
  requirement = 'The system shall avoid regression on material time step and combined anisotropic creep computations'
[]

[ad_aniso_creep_x_3d]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_x_3d.i'
  csvdiff = ad_aniso_creep_x_3d_out.csv
  requirement = 'The system shall be capable of reproducing verification results of creep strain ratios along the X direction.'
  min_parallel = 2
  rel_err = 1.0e-4
  abs_zero = 5.0e-7
[]

[aniso_creep_x_3d]
  type = 'CSVDiff'
  input = 'aniso_creep_x_3d.i'
  csvdiff = aniso_creep_x_3d_out.csv
  requirement = 'The system shall be capable of reproducing verification results of creep strain ratios along the X direction using hand-coded Jacobians.'
  min_parallel = 2
  rel_err = 1.0e-4
  abs_zero = 5.0e-7
[]

[ad_aniso_creep_x_3d_aniso_elasticity]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_x_3d_anisoElasticity.i'
  csvdiff = ad_aniso_creep_x_3d_anisoElasticity_out.csv
  requirement = 'The system shall reproduce the creep strain as those evaluated with residual and derivative computations used for isotropic elasticity.'
  min_parallel = 2
  rel_err = 1.0e-4
  abs_zero = 5.0e-7
  heavy = true
  max_time = 900
[]

[ad_aniso_creep_x_3d_shear]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_x_3d_shear.i'
  csvdiff = ad_aniso_creep_x_3d_shear_out.csv
  requirement = 'The system shall compute shear creep strain in an element subject to shear load in one direction.'
  rel_err = 1.0e-4
  abs_zero = 5.0e-7
[]

[ad_aniso_creep_xy_3d_shear]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_xy_3d_shear.i'
  csvdiff = ad_aniso_creep_xy_3d_shear_out.csv
  requirement = 'The system shall compute shear creep strain in an element subject to shear load in two directions.'
  rel_err = 1.0e-4
  abs_zero = 5.0e-7
[]

[ad_aniso_creep_xy_3d_aniso_elasticity]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_xy_3d_anisoElasticity.i'
  csvdiff = ad_aniso_creep_xy_3d_anisoElasticity_out.csv
  requirement = 'The system shall compute creep strains in an element with anisotropic elasticity and subject to biaxial tensile load.'
  min_parallel = 2
  rel_err = 1.0e-4
  abs_zero = 5.0e-7
  heavy = true
  max_time = 900
[]

[aniso_creep_x_3d_no_trafo]
  type = 'CSVDiff'
  input = 'aniso_creep_x_3d.i'
  csvdiff = aniso_creep_x_3d_no_trafo_out.csv
  cli_args = "Materials/trial_creep_two/use_transformation=false Outputs/file_base=aniso_creep_x_3d_no_trafo_out"
  requirement = 'The system shall be capable of reproducing verification results of creep strain ratios along the X direction using hand-coded Jacobians when no transformation is used to rotate the Hill tensor for small deformation.'
  min_parallel = 2
  rel_err = 1.0e-4
  abs_zero = 5.0e-7
[]

[ad_aniso_creep_y_3d]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_y_3d.i'
  csvdiff = ad_aniso_creep_y_3d_out.csv
  requirement = 'The system shall be capable of reproducing verification results of creep strain ratios along the Y direction.'
  min_parallel = 2
  rel_err = 1.0e-5
  abs_zero = 1.0e-7
[]

[ad_aniso_creep_z_3d]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_z_3d.i'
  csvdiff = ad_aniso_creep_z_3d_out.csv
  requirement = 'The system shall be capable of reproducing verification results of creep strain ratios along the Z direction.'
  min_parallel = 2
  rel_err = 1.0e-5
  abs_zero = 1.0e-7
[]

[ad_aniso_iso_iso]
  type = 'CSVDiff'
  input = 'ad_aniso_iso_creep_x_3d.i'
  csvdiff = ad_aniso_iso_creep_x_3d_out.csv
  cli_args = "Materials/elastic_strain/inelastic_models='trial_creep_iso' Materials/inactive='trial_creep_aniso_iso' Outputs/file_base=ad_aniso_iso_creep_x_3d_out"
  requirement = 'The system shall be capable of reproducing isotropic creep with the right anisotropic creep parameters: Baseline'
  min_parallel = 2
  rel_err = 1.0e-5
  abs_zero = 1.0e-8
[]

[jac_ad]
  type = 'PetscJacobianTester'
  input = 'ad_aniso_iso_creep_x_3d.i'
  run_sim = 'True'
  cli_args = "Executioner/num_steps=2 Outputs/active='' -snes_test_err 1e-12 Materials/elastic_strain/inelastic_models='trial_creep_iso' Materials/inactive='trial_creep_aniso_iso' Materials/elasticity_tensor/poissons_ratio=0.25"
  petsc_version = '>=3.9'
  ratio_tol = 1e-2
  difference_tol = 0.1
  only_final_jacobian = 'True'
  issues = '#17456'
  requirement = 'The system shall provide a perfect Jacobian while calculating large deformation creep.'
[]

[jac]
  type = 'PetscJacobianTester'
  input = 'aniso_iso_creep_x_3d.i'
  run_sim = 'True'
  cli_args = "Executioner/num_steps=2 Outputs/active='' -snes_test_err 1e-12 Materials/elastic_strain/inelastic_models='trial_creep_iso' Materials/inactive='trial_creep_aniso_iso' Materials/elasticity_tensor/poissons_ratio=0.25"
  petsc_version = '>=3.9'
  ratio_tol = 0.035
  difference_tol = 0.35
  only_final_jacobian = 'True'
  issues = '#21824'
  requirement = 'The system shall provide a reasonable Jacobian while calculating large deformation creep using the elasticity tensor as the tangent operator.'
[]

[ad_aniso_iso_aniso]
  type = 'CSVDiff'
  input = 'ad_aniso_iso_creep_x_3d.i'
  csvdiff = ad_aniso_iso_aniso_creep_x_3d_out.csv
  cli_args = "Materials/elastic_strain/inelastic_models='trial_creep_aniso_iso' Materials/inactive='trial_creep_iso' Outputs/file_base=ad_aniso_iso_aniso_creep_x_3d_out"
  requirement = 'The system shall be capable of reproducing isotropic creep with the right anisotropic creep parameters.'
  min_parallel = 2
  rel_err = 1.0e-4
  abs_zero = 1.0e-8
[]

[aniso_creep_integration_error]
  type = 'CSVDiff'
  input = 'aniso_creep_integration_error.i'
  csvdiff = aniso_creep_integration_error_out.csv
  requirement = 'The system shall be capable of enforcing a time step such that the creep rate integration error is controled by the user with the aid of a soft terminator when regular (non-AD) objects are used.'
  heavy = true
  rel_err = 1.0e-4
  abs_zero = 1.0e-8
[]

[ad_aniso_creep_integration_error]
  type = 'CSVDiff'
  input = 'ad_aniso_creep_integration_error.i'
  csvdiff = ad_aniso_creep_integration_error_out.csv
  requirement = 'The system shall be capable of enforcing a time step such that the creep rate integration error is controled by the user with the aid of a soft terminator.'
  heavy = true
  rel_err = 1.0e-4
  abs_zero = 1.0e-8
[]

[ad_aniso_creep_temperature_coefficients]
  type = 'Exodiff'
  input = 'ad_aniso_creep_temperature_coefficients.i'
  exodiff = ad_aniso_creep_temperature_coefficients_out.e
  requirement = 'The system shall be capable of running Hill materials with constant coefficients and coefficients that are function of temperature to capture material texture. This test performs a reference run with constant coefficients'
  rel_err = 1.0e-4
  abs_zero = 1.0e-8
  heavy = true
[]

[ad_aniso_creep_temperature_coefficients_function]
  type = 'Exodiff'
  input = 'ad_aniso_creep_temperature_coefficients_function.i'
  exodiff = ad_aniso_creep_temperature_coefficients_function_out.e
  custom_cmp = 'temperature.exodiff'
  requirement = 'The system shall be capable of running Hill materials with constant coefficients and coefficients that are function of temperature to capture material texture. This test performs a run using a constant temperature function.'
  rel_err = 1.0e-4
  abs_zero = 1.0e-8
  heavy = true
[]

[ad_aniso_creep_temperature_coefficients_function_variation]
  type = 'Exodiff'
  input = 'ad_aniso_creep_temperature_coefficients_function_variation.i'
  exodiff = ad_aniso_creep_temperature_coefficients_function_variation_out.e
  requirement = 'The system shall be capable of running anisotropic Hill creep with temperature-dependent Hill coefficients and generating correct output.'
  rel_err = 1.0e-4
  abs_zero = 1.0e-8
  heavy = true
[]

[3d_bar_orthotropic_90deg_rotation_ad_creep_z_no_rotation]
  type = 'CSVDiff'
  input = '3d_bar_orthotropic_90deg_rotation_ad_creep_z_no_rotation.i'
  csvdiff = 3d_bar_orthotropic_90deg_rotation_ad_creep_z_no_rotation_out.csv
  requirement = 'The system shall be capable of using large deformation rotation to update the orientation of Hill parameters even when there is no rigid body rotation. This test also serves as a reference to verify the updates to the Hill parameters when there is significant rigid body motion'
  rel_err = 1.0e-3
  abs_zero = 1.0e-10
  heavy = true
[]

[3d_bar_orthotropic_90deg_rotation_ad_creep_z]
  type = 'CSVDiff'
  input = '3d_bar_orthotropic_90deg_rotation_ad_creep_z.i'
  csvdiff = 3d_bar_orthotropic_90deg_rotation_ad_creep_z_out.csv
  requirement = 'The system shall be capable of using large deformation rotation to update the orientation of Hill parameters when there is 90-degree rigid body orientation change about the Z axis. The creep strains have to be very similar to the output when there is no rigid body motion (Note: The mere constraints enforcing rigid body rotation induce numerical errors). In this case using Hill constants.'
  rel_err = 2.0e-2
  abs_zero = 5.0e-10
  heavy = true
[]

[3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation]
  type = 'CSVDiff'
  input = '3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation.i'
  csvdiff = 3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation_out.csv
  requirement = 'The system shall be capable of using large deformation rotation to update the orientation of Hill parameters even when there is no rigid body rotation. This test also serves as a reference to verify the updates to the Hill parameters when there is significant rigid body motion'
  rel_err = 1.0e-3
  abs_zero = 1.0e-10
  heavy = true
[]

[3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation_no_transformation]
  type = 'CSVDiff'
  input = '3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation.i'
  csvdiff = 3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation_no_transformation_out.csv
  cli_args = "Materials/hill_tensor/use_large_rotation=false Materials/trial_creep/use_transformation=false Outputs/file_base=3d_bar_orthotropic_90deg_rotation_ad_creep_x_no_rotation_no_transformation_out"
  requirement = 'The system shall be capable of not using large deformation rotation to define Hill anisotropic parameters. '
  rel_err = 1.0e-3
  abs_zero = 1.0e-10
  heavy = true
[]

[3d_bar_orthotropic_90deg_rotation_ad_creep_x]
  type = 'CSVDiff'
  input = '3d_bar_orthotropic_90deg_rotation_ad_creep_x.i'
  csvdiff = 3d_bar_orthotropic_90deg_rotation_ad_creep_x_out.csv
  requirement = 'The system shall be capable of using large deformation rotation to update the orientation of Hill parameters when there is 90-degree rigid body orientation change about the X axis. The creep strains have to be very similar to the output when there is no rigid body motion (Note: The mere constraints enforcing rigid body rotation induce numerical errors). In this case using Hill constants.'
  rel_err = 2.0e-2
  abs_zero = 5.0e-10
  heavy = true
[]

[./finite_elastic-noad]
  type = 'Exodiff'
  input = 'finite_elastic-noad.i'
  exodiff = 'finite_elastic_out.e'
  requirement = 'We shall be able to reproduce finite strain elasticity results of the hand-coded simulation using automatic differentiation. (non-AD reference)'
  design = 'ComputeFiniteStrain.md'
[../]

[new]
  type = 'Exodiff'
  input = 'finite_strain_elastic_new_test.i'
  exodiff = 'finite_strain_elastic_new_test_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.'
[]

[new_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_elastic_new_test.i'
  exodiff = 'finite_strain_elastic_new_test_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'new'
  issues = '#8235 #4716'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation found with the Taylor expansion from Rashid(1993) on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.'
[]

[eigen_sol]
  type = 'Exodiff'
  input = 'finite_strain_elastic_eigen_sol.i'
  exodiff = 'finite_strain_elastic_eigen_sol_out.e'
  issues = '#4716 #7555'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the QuasiStatic SolidMechanics Physics.'
[]

[eigen_sol_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_elastic_eigen_sol.i'
  exodiff = 'finite_strain_elastic_eigen_sol_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'eigen_sol'
  issues = '#8235 #4716'
  design = 'source/materials/ComputeFiniteStrainElasticStress.md source/materials/ComputeFiniteStrain.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeFiniteStrainElasticStress class shall compute the elastic stress for a finite strain formulation using a direct eigensolution to perform the polar decomposition of stretch and rotation on a unit 3D cube in a Cartesian system using the volumetric locking correction b-bar formulation.'
[]

[./bending]
  type = 'Exodiff'
  input = 'bending_jacobian.i'
  exodiff = 'bending_jacobian_out.e'
  issues = '#7228'
  design = '/ComputeFiniteStrain.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   bar bending simulation in 2D'
[../]

[./bending_Bbar]
  type = 'Exodiff'
  input = 'bending_jacobian.i'
  exodiff = 'bending_jacobian_bbar_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=bending_jacobian_bbar_out'
  prereq = 'bending'
  issues = '#7228'
  design = '/ComputeFiniteStrain.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   bar bending simulation in 2D using a volumetric locking correction'
[../]

[./3d_bar]
  type = 'Exodiff'
  input = '3d_bar.i'
  exodiff = '3d_bar_out.e'
  issues = '#7228'
  design = '/ComputeFiniteStrain.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   tensile test simulation in 3D'
[../]

[./3d_bar_Bbar]
  type = 'Exodiff'
  input = '3d_bar.i'
  exodiff = '3d_bar_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = '3d_bar'
  issues = '#7228'
  design = '/ComputeFiniteStrain.md'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   tensile test simulation in 3D using a volumetric locking correction'
[../]

[except3]
  type = 'RunException'
  input = 'large_deform1.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/decomposition_method=TaylorExpansion'
  expect_err = 'Cannot take square root of a number less than or equal to zero in the calculation of C1 for the Rashid approximation for the rotation tensor. This zero or negative number may occur when elements become heavily distorted.'
  issues = '#19067'
  design = '/ComputeFiniteStrain.md'
  requirement = 'The system shall cut the timestep through a mooseException when the loading conditions deform the element enough to produce a negative number under a square root term in the Rashid approximation for the rotation tensor'
[]

[./finite_elastic]
  type = 'Exodiff'
  input = 'finite_elastic.i'
  exodiff = 'finite_elastic_out.e'
  prereq = 'finite_elastic-noad'
  requirement = 'We shall be able to reproduce finite strain elasticity results of the hand-coded simulation using automatic differentiation.'
  design = 'ADComputeFiniteStrain.md'
[../]

[./finite_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'finite_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-4
  requirement = 'The Jacobian for the AD finite strain elasticity problem shall be perfect'
  design = 'ADComputeFiniteStrain.md'
[../]

[bending]
  type = Exodiff
  input = 'bending_jacobian.i'
  exodiff = 'bending_jacobian_out.e'
  issues = '#7228 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   bar bending simulation in 2D using AD and match non-AD methods'
[]

[bending_Bbar]
  type = Exodiff
  input = 'bending_jacobian.i'
  exodiff = 'bending_jacobian_bbar_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Outputs/file_base=bending_jacobian_bbar_out'
  prereq = 'bending'
  issues = '#7228 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   bar bending simulation in 2D using a volumetric locking correction using AD and
                   match non-AD methods'
[]

[3d_bar]
  type = Exodiff
  input = '3d_bar.i'
  exodiff = '3d_bar_out.e'
  issues = '#7228 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   tensile test simulation in 3D using AD and match non-AD methods'
[]

[3d_bar_Bbar]
  type = Exodiff
  input = '3d_bar.i'
  exodiff = '3d_bar_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = '3d_bar'
  issues = '#7228 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   tensile test simulation in 3D using a volumetric locking correction using AD and
                   match non-AD methods'
[]

[bending-jac]
  type = PetscJacobianTester
  input = 'bending_jacobian.i'
  run_sim = 'True'
  prereq = 'bending'
  ratio_tol = 5e-8
  difference_tol = 1
  issues = '#12650 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   bar bending simulation in 2D using AD and calculate perfect Jacobians'
[]

[bending_Bbar-jac]
  type = PetscJacobianTester
  input = 'bending_jacobian.i'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  run_sim = 'True'
  prereq = 'bending_Bbar'
  ratio_tol = 5e-8
  difference_tol = 1
  issues = '#12650 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   bar bending simulation in 2D using a volumetric locking correction using AD and
                   calculate perfect Jacobians'
[]

[3d_bar-jac]
  type = PetscJacobianTester
  input = '3d_bar.i'
  prereq = '3d_bar'
  run_sim = 'True'
  ratio_tol = 5e-8
  difference_tol = 1
  issues = '#12650 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   tensile test simulation in 3D using AD and calculate perfect Jacobians'
  valgrind = 'none' # too slow especially after #14547
  cli_args = 'Executioner/num_steps=1'
[]

[3d_bar_Bbar-jac]
  type = PetscJacobianTester
  input = '3d_bar.i'
  cli_args = 'GlobalParams/volumetric_locking_correction=true Executioner/num_steps=1'
  prereq = '3d_bar_Bbar'
  run_sim = 'True'
  ratio_tol = 5e-8
  difference_tol = 1
  issues = '#12650 #13260'
  requirement = 'Finite strain methods in Tensor Mechanics should be able to adequately simulate a
                   tensile test simulation in 3D using a volumetric locking correction using AD and
                   calculate perfect Jacobians'
  valgrind = 'none' # too slow especially after #14547
[]

[bending_exception]
  type = 'RunException'
  input = bending_jacobian.i
  cli_args = 'BCs/move_y/function="-100*t"'
  expect_err = 'Cannot take square root of a number less than or equal to zero in the calculation of C3_test for the Rashid approximation for the rotation tensor. This zero or negative number may occur when elements become heavily distorted.'
  issues = '#19067'
  requirement = 'Finite strain methods in Tensor Mechanics, using the auto differentiation capabilities, shall cut the timestep through  a mooseException when the loading conditions deform the elements so much as to produce a negative number under the square root term in the Rashid approximation for the rotation tensor calcuation'
[]

[./incremental_small_elastic-noad]
  type = 'Exodiff'
  input = 'incremental_small_elastic-noad.i'
  exodiff = 'incremental_small_elastic_out.e'
  requirement = 'We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation using automatic differentiation. (non-AD reference)'
  design = 'ComputeIncrementalStrain.md'
[../]

[./elastic_patch_incremental_small]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584'
[../]

[./elastic_patch_incremental_small_no_disp_mesh]
  prereq = elastic_patch_total_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Mesh/use_displaced_mesh=false Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584 #12580'
[../]

[./incremental_small_elastic]
  type = 'Exodiff'
  input = 'incremental_small_elastic.i'
  exodiff = 'incremental_small_elastic_out.e'
  prereq = 'incremental_small_elastic-noad'
  requirement = 'We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation using automatic differentiation.'
  design = 'ADComputeIncrementalStrain.md'
[../]

[./incremental_small_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'incremental_small_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e0
  requirement = 'The Jacobian for the AD incremental small strain elasticity problem shall be perfect'
  design = 'ADComputeIncrementalStrain.md'
[../]

[./green-lagrange]
  type = 'Exodiff'
  input = 'green-lagrange.i'
  exodiff = 'green-lagrange_out.e'
  requirement = 'The system shall provide an AD enabled Green-Lagrange strain calculator'
  allow_test_objects = true
  design = 'ADComputeGreenLagrangeStrain.md'
[../]

[./green-lagrange-jac]
  type = 'PetscJacobianTester'
  input = 'green-lagrange.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-6
  requirement = 'The Jacobian for the Green-Lagrange strain calculator shall be perfect'
  design = 'ADComputeGreenLagrangeStrain.md'
[../]

[./rspherical_finite_elastic-noad]
  type = 'Exodiff'
  input = 'rspherical_finite_elastic-noad.i'
  exodiff = 'rspherical_finite_elastic_out.e'
  requirement = 'We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation. (non-AD reference)'
  design = 'ComputeRSphericalFiniteStrain.md'
[../]

[./rspherical_finite_elastic]
  type = 'Exodiff'
  input = 'rspherical_finite_elastic.i'
  exodiff = 'rspherical_finite_elastic_out.e'
  prereq = 'rspherical_finite_elastic-noad'
  requirement = 'We shall be able to reproduce finite strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation.'
  design = 'ADComputeRSphericalFiniteStrain.md'
[../]

[./rspherical_finite_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'rspherical_finite_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e1
  cli_args = '-mat_fd_type ds'
  requirement = 'The Jacobian for the AD finite strain elasticity problem in spherical coordinates shall be perfect'
  design = 'ADComputeRSphericalFiniteStrain.md'
[../]

[./rspherical_incremental_small_elastic]
  type = 'Exodiff'
  input = 'rspherical_incremental_small_elastic.i'
  exodiff = 'rspherical_incremental_small_elastic_out.e'
  prereq = 'rspherical_incremental_small_elastic-noad'
  requirement = 'We shall be able to reproduce incremental small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation.'
  design = 'ADComputeRSphericalIncrementalStrain.md'
[../]

[./rspherical_incremental_small_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'rspherical_incremental_small_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-1
  cli_args = '-mat_fd_type ds'
  requirement = 'The Jacobian for the AD incremental small strain elasticity in spherical coordinates problem shall be perfect'
  design = 'ADComputeRSphericalIncrementalStrain.md'
[../]

[./rspherical_small_elastic]
  type = 'Exodiff'
  input = 'rspherical_small_elastic.i'
  exodiff = 'rspherical_small_elastic_out.e'
  prereq = 'rspherical_small_elastic-noad'
  requirement = 'We shall be able to reproduce small strain elasticity results of the hand-coded simulation in spherical coordinates using automatic differentiation.'
  design = 'ADComputeRSphericalSmallStrain.md'
[../]

[./rspherical_small_elastic-jac]
  type = 'PetscJacobianTester'
  input = 'rspherical_small_elastic.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-1
  cli_args = '-mat_fd_type ds'
  requirement = 'The Jacobian for the AD small strain elasticity problem in spherical coordinates shall be perfect'
  design = 'ADComputeRSphericalSmallStrain.md'
[../]

[./lambda_shear]
  type = Exodiff
  input = 'lambda_shear_modulus_test.i'
  exodiff = 'lambda_shear_modulus_test_out.e'
  requirement = 'The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the lambda and shear modulus for an isotropic material using AD formulations.'
[../]

[./youngs_poissons]
  type = Exodiff
  input = 'youngs_modulus_poissons_ratio_test.i'
  exodiff = 'youngs_modulus_poissons_ratio_test_out.e'
  requirement = "The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the Young's modulus and Poisson's ratio for an isotropic material using AD formulations."
[../]

[./bulk_shear]
  type = Exodiff
  input = 'bulk_modulus_shear_modulus_test.i'
  exodiff = 'bulk_modulus_shear_modulus_test_out.e'
  requirement = 'The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from their bulk modulus and shear modulus for an isotropic material using AD formulations.'
[../]

[./axisymmetric_rz]
  type = Exodiff
  input = '2D-axisymmetric_rz_test.i'
  exodiff = '2D-axisymmetric_rz_test_out.e'
  requirement = 'The ComputeElasticityTensor class shall correctly compute the elasticity tensor for an isotropic axisymmetric problem.'
[../]

[./lambda_shear-jac]
  type = PetscJacobianTester
  input = 'lambda_shear_modulus_test.i'
  run_sim = 'True'
  ratio_tol = 1e-8
  difference_tol = 1e-5
  issues = '#12650'
  requirement = 'The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the lambda and shear modulus for an isotropic material using AD formulations and produce a perfect Jacobian.'
[../]

[./youngs_poissons-jac]
  type = PetscJacobianTester
  input = 'youngs_modulus_poissons_ratio_test.i'
  run_sim = 'True'
  ratio_tol = 1e-8
  difference_tol = 1e-5
  issues = '#12650'
  requirement = "The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the Young's modulus and Poisson's ratio for an isotropic material using AD formulations and produce a perfect Jacobian."
[../]

[./bulk_shear-jac]
  type = PetscJacobianTester
  input = 'bulk_modulus_shear_modulus_test.i'
  run_sim = 'True'
  ratio_tol = 1e-8
  difference_tol = 1e-5
  issues = '#12650'
  requirement = 'The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from their bulk modulus and shear modulus for an isotropic material using AD formulations and produce a perfect Jacobian.'
[../]

[./axisymmetric_rz-jac]
  type = PetscJacobianTester
  input = '2D-axisymmetric_rz_test.i'
  run_sim = 'True'
  ratio_tol = 1e-8
  difference_tol = 1e-1
  issues = '#12650'
  requirement = 'The ComputeElasticityTensor class shall correctly compute the elasticity tensor for an isotropic axisymmetric problem and produce a perfect Jacobian.'
[../]

[./num_constants]
  type = 'RunException'
  input = 'num_constants.i'
  expect_err = "Exactly two elastic constants must be defined for material 'elasticity_tensor'"
  design = "ComputeIsotropicElasticityTensor.md"
  issues = "#9438"
  requirement = "The system shall generate an error if a number of elastic constants other than two is supplied for an isotropic elasticity tensor"
[../]

[./youngs_modulus]
  type = 'RunException'
  input = 'youngs_modulus.i'
  expect_err = "Youngs modulus must be positive in material 'elasticity_tensor'"
  design = "ComputeIsotropicElasticityTensor.md"
  issues = "#9438"
  requirement = "The system shall generate an error if a non-positive Youngs modulus is supplied for an isotropic elasticity tensor"
[../]

[./bulk_modulus]
  type = 'RunException'
  input = 'bulk_modulus.i'
  expect_err = "Bulk modulus must be positive in material 'elasticity_tensor'"
  design = "ComputeIsotropicElasticityTensor.md"
  issues = "#9438"
  requirement = "The system shall generate an error if a non-positive bulk modulus is supplied for an isotropic elasticity tensor"
[../]

[./poissons_ratio]
  type = 'RunException'
  input = 'poissons_ratio.i'
  expect_err = "Poissons ratio must be greater than -1 and less than 0.5 in material 'elasticity_tensor'"
  design = "ComputeIsotropicElasticityTensor.md"
  issues = "#9438"
  requirement = "The system shall generate an error if a Poissons ratio outside the range from -1 to 0.5 is supplied for an isotropic elasticity tensor"
[../]

[./shear_modulus]
  type = 'RunException'
  input = 'shear_modulus.i'
  expect_err = "Shear modulus must not be negative in material 'elasticity_tensor'"
  design = "ComputeIsotropicElasticityTensor.md"
  issues = "#9438"
  requirement = "The system shall generate an error if a non-positive shear modulus is supplied for an isotropic elasticity tensor"
[../]

[./elastic_patch]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#458'
[../]

[./elastic_patch_incremental_small]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584'
[../]

[./elastic_patch_total_small]
  prereq = elastic_patch_incremental_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeSmallStrain Materials/stress/type=ComputeLinearElasticStress Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeSmallStrain.md ComputeLinearElasticStress.md'
  issues = '#12584'
[../]

[./elastic_patch_incremental_small_no_disp_mesh]
  prereq = elastic_patch_total_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Mesh/use_displaced_mesh=false Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584 #12580'
[../]

[./elastic_patch_Bbar]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'elastic_patch'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[./elastic_patch_2Procs]
  type = Exodiff
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  min_parallel = 2
  prereq = 'elastic_patch_Bbar'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when running on 2 processors in parallel.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#458'
[../]

[./elastic_patch_2Procs_Bbar]
  type = Exodiff
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  min_parallel = 2
  prereq = 'elastic_patch_2Procs'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[./elastic_patch_quadratic]
  type = Exodiff
  input = 'elastic_patch_quadratic.i'
  exodiff = 'elastic_patch_quadratic_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular 20-noded quadratic hexes.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#620'
[../]

[./lambda_shear]
  type = Exodiff
  input = 'lambda_shear_modulus_test.i'
  exodiff = 'lambda_shear_modulus_test_out.e'
  requirement = 'The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the lambda and shear modulus for an isotropic material.'
[../]

[./youngs_poissons]
  type = Exodiff
  input = 'youngs_modulus_poissons_ratio_test.i'
  exodiff = 'youngs_modulus_poissons_ratio_test_out.e'
  requirement = "The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from the Young's modulus and Poisson's ratio for an isotropic material."
[../]

[./bulk_shear]
  type = Exodiff
  input = 'bulk_modulus_shear_modulus_test.i'
  exodiff = 'bulk_modulus_shear_modulus_test_out.e'
  requirement = 'The ComputeIsotropicElasticityTensor class shall correctly compute the elasticity tensor from their bulk modulus and shear modulus for an isotropic material.'
[../]

[./linear_elastic_material]
  type = 'Exodiff'
  input = 'linear_elastic_material.i'
  exodiff = 'linear_elastic_material_out.e'
  max_parallel = 1
  requirement = 'We shall be able to reproduce linear elastic stress results of the hand-coded simulation using automatic differentiation.'
  design = 'ADComputeLinearElasticStress.md'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./linear_elastic_material-jac]
  type = 'PetscJacobianTester'
  input = 'linear_elastic_material.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-1
  prereq = linear_elastic_material
  requirement = 'The Jacobian for the AD linear elastic stress problem shall be perfect'
  design = 'ADComputeLinearElasticStress.md'
[../]

[./extra_stresses]
  type = 'Exodiff'
  input = 'extra_stresses.i'
  exodiff = 'extra_stresses_out.e'
  requirement = 'We shall be able to introduce extra stresses into the stress calculators using automatic differentiation.'
  design = 'ADComputeLinearElasticStress.md'
[../]

[./extra_stresses-jac]
  type = 'PetscJacobianTester'
  input = 'extra_stresses.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-1
  prereq = extra_stresses
  requirement = 'The Jacobian for the AD linear elastic stress problem shall be perfect'
  design = 'ADComputeLinearElasticStress.md'
[../]

[./tensor]
  type = 'Exodiff'
  input = 'tensor.i'
  exodiff = 'tensor_out.e'
  max_parallel = 1
  requirement = 'We shall be able to reproduce small strain with specified tensors results of the hand-coded simulation using automatic differentiation.'
  design = 'ADComputeLinearElasticStress.md'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./tensor-jac]
  type = 'PetscJacobianTester'
  input = 'tensor.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-4
  prereq = tensor
  requirement = 'The Jacobian for the AD small strain with specified tensors problem shall be perfect'
  design = 'ADComputeLinearElasticStress.md'
[../]

[./applied_strain]
  type = 'Exodiff'
  input = 'applied_strain.i'
  exodiff = 'applied_strain_out.e'
  requirement = 'We shall be able to reproduce eigenstrain results of the hand-coded simulation using automatic differentiation.'
  design = 'ComputeEigenstrain.md'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./applied_strain-jac]
  type = 'PetscJacobianTester'
  input = 'applied_strain.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-1
  prereq = applied_strain
  requirement = 'The Jacobian for the AD eigenstrain problem shall be perfect'
  design = 'ComputeEigenstrain.md'
[../]

[./thermal_expansion]
  type = 'Exodiff'
  input = 'thermal_expansion.i'
  exodiff = 'thermal_expansion_out.e'
  requirement = 'We shall be able to reproduce thermal eigenstrain results of the hand-coded simulation using automatic differentiation.'
  design = 'ComputeEigenstrain.md'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./thermal_expansion-jac]
  type = 'PetscJacobianTester'
  input = 'thermal_expansion.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-4
  prereq = thermal_expansion
  requirement = 'The Jacobian for the AD thermal eigenstrain problem shall be perfect'
  design = 'ComputeEigenstrain.md'
[../]

[./powerlaw_ten]
  type = 'CSVDiff'
  input = 'power_law_creep.i'
  csvdiff = 'power_law_creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten"'
  requirement = "The AD multiple inelastic stress calculator shall provide a correct stress for a single power law creep model (reference computation)"
  design = 'PowerLawCreepStressUpdate.md'
[../]

[./creep]
  type = CSVDiff
  input = creep.i
  csvdiff = creep_out.csv
  design = 'source/materials/PowerLawCreepStressUpdate.md source/materials/ADComputeMultipleInelasticStress.md'
  requirement = 'The PowerLawCreepStressUpdate, called through the ADComputeMultipleInelasticStress, shall compute a creep strain based on an extrenal loading.'
[../]

[./creep-jac]
  type = 'PetscJacobianTester'
  input = 'creep.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e8
  prereq = creep
  requirement = 'The Jacobian for the AD regular creep problem shall be perfect'
  design = 'source/materials/PowerLawCreepStressUpdate.md source/materials/ADComputeMultipleInelasticStress.md'
[../]

[high]
  type = RunApp
  input = 'nonad_bounds.i'
  detail = 'from the high bound.'
  allow_test_objects = true
  cli_args = 'Executioner/num_steps=1 Materials/creep/initial_guess=100'
  expect_out = 'Scalar greater than maximum'
[]

[low]
  type = RunApp
  input = 'nonad_bounds.i'
  detail = 'from the low bound.'
  allow_test_objects = true
  cli_args = 'Executioner/num_steps=1 Materials/creep/initial_guess=-100'
  expect_out = 'Scalar less than minimum'
[]

[power_law_creep_restart2]
  type = 'Exodiff'
  input = 'restart2.i'
  exodiff = 'restart2_out.e'
  detail = 'that shall be restartable with a response that matches the original run.'
  exodiff_opts = '-TM'
  prereq = nonad/restart1
[]

[power_law_creep_restart2]
  type = 'Exodiff'
  input = 'ad_restart2.i'
  exodiff = 'ad_restart2_out.e'
  detail = 'that shall be restartable with a response that matches the original run.'
  exodiff_opts = '-TM'
  prereq = ad/restart1
[]

[power_law_creep-jac]
  type = 'PetscJacobianTester'
  input = 'ad_power_law_creep.i'
  ratio_tol = 5e-6
  difference_tol = 1e6
  cli_args = 'Executioner/num_steps=2 -snes_test_err 1e-11'
  run_sim = True
  detail = 'calculate a perfect Jacobian'
[]

[small_strain-jac]
  type = PetscJacobianTester
  input = 'ad_smallstrain.i'
  ratio_tol = 5e-6
  difference_tol = 1e6
  cli_args = 'Executioner/num_steps=2 -snes_test_err 1e-11'
  run_sim = True
  detail = 'calculate a perfect Jacobian with the small strain formulation'
[]

[./powerlaw_zero]
  type = 'CSVDiff'
  input = 'power_law_creep.i'
  csvdiff = 'power_law_creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_zero"'
  prereq = powerlaw_ten
  requirement = "The AD multiple inelastic stress calculator shall provide a correct stress for a single power law creep model and an additional zero creep power law model"
  design = 'ADComputeMultipleInelasticStress.md'
[../]

[./powerlaw_sum]
  type = 'CSVDiff'
  input = 'power_law_creep.i'
  csvdiff = 'power_law_creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_nine creep_one"'
  prereq = powerlaw_zero
  valgrind = HEAVY
  requirement = "The AD multiple inelastic stress calculator shall provide a correct stress for the linear combination of two power law creep models"
  design = 'ADComputeMultipleInelasticStress.md'
[../]

[./powerlaw_cycle]
  type = 'CSVDiff'
  input = 'power_law_creep.i'
  csvdiff = 'power_law_creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_ten2" Materials/elastic_strain/cycle_models=true'
  prereq = powerlaw_sum
  requirement = "The AD multiple inelastic stress calculator shall provide a correct stress when cycling through two identical power law creep models"
  design = 'ADComputeMultipleInelasticStress.md'
[../]

[./powerlaw_ten_jacobian]
  type = 'PetscJacobianTester'
  input = 'power_law_creep.i'
  run_sim = 'True'
  ratio_tol = 5e-6
  difference_tol = 2e-2
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten" Outputs/csv=false -snes_test_err 1e-9 -mat_fd_type ds'
  requirement = "The AD multiple inelastic stress calculator shall provide a correct jacobian for a single power law creep model"
  design = 'ADComputeMultipleInelasticStress.md'
[../]

[./powerlaw_zero_jacobian]
  type = 'PetscJacobianTester'
  input = 'power_law_creep.i'
  run_sim = 'True'
  ratio_tol = 5e-6
  difference_tol = 2e-2
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_zero" Outputs/csv=false -snes_test_err 1e-9 -mat_fd_type ds'
  requirement = "The AD multiple inelastic stress calculator shall provide a correct jacobian for a single power law creep model and an additional zero creep power law model"
  design = 'ADComputeMultipleInelasticStress.md'
[../]

[./powerlaw_sum_jacobian]
  type = 'PetscJacobianTester'
  input = 'power_law_creep.i'
  run_sim = 'True'
  ratio_tol = 5e-6
  difference_tol = 2e-2
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_nine creep_one" Outputs/csv=false -snes_test_err 1e-9 -mat_fd_type ds'
  requirement = "The AD multiple inelastic stress calculator shall provide a correct jacobian for the linear combination of two power law creep models"
  design = 'ADComputeMultipleInelasticStress.md'
  valgrind = 'none' # too slow especially after #14547
[../]

[./powerlaw_cycle_jacobian]
  type = 'PetscJacobianTester'
  input = 'power_law_creep.i'
  run_sim = 'True'
  ratio_tol = 5e-6
  difference_tol = 2e-2
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_ten2" Materials/elastic_strain/cycle_models=true Outputs/csv=false -snes_test_err 1e-9 -mat_fd_type ds'
  requirement = "The AD multiple inelastic stress calculator shall provide a correct jacobian when cycling through two identical power law creep models"
  design = 'ADComputeMultipleInelasticStress.md'
[../]

[./creep]
  type = CSVDiff
  input = creep.i
  csvdiff = creep_out.csv
  design = 'source/materials/PowerLawCreepStressUpdate.md source/materials/ADComputeMultipleInelasticStress.md'
  requirement = 'The PowerLawCreepStressUpdate, called through the ADComputeMultipleInelasticStress, shall compute a creep strain based on an extrenal loading.'
[../]

[./creep-jac]
  type = 'PetscJacobianTester'
  input = 'creep.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e8
  prereq = creep
  requirement = 'The Jacobian for the AD regular creep problem shall be perfect'
  design = 'source/materials/PowerLawCreepStressUpdate.md source/materials/ADComputeMultipleInelasticStress.md'
[../]

[./exact_spherical]
  type = CSVDiff
  input = exact.i
  csvdiff = exact_spherical_out.csv
  requirement = 'The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.'
[../]

[./exact_spherical-jac]
  type = 'PetscJacobianTester'
  input = 'exact.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  prereq = exact_spherical
  requirement = 'The Jacobian for the AD exact spherical problem shall be perfect'
[../]

[./exact_cylindrical]
  type = CSVDiff
  input = exact.i
  csvdiff = exact_cylindrical_out.csv
  cli_args = 'GlobalParams/pore_shape_model=CYLINDRICAL Outputs/file_base=exact_cylindrical_out'
  prereq = exact_spherical
  requirement = 'The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.'
[../]

[./exact_cylindrical-jac]
  type = 'PetscJacobianTester'
  input = 'exact.i'
  cli_args = "-snes_test_err 1e-11 GlobalParams/pore_shape_model=CYLINDRICAL Outputs/file_base=exact_cylindrical_out"
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  prereq = exact_cylindrical
  requirement = 'The Jacobian for the AD exact cylindrical problem shall be perfect'
[../]

[./lps_single]
  type = CSVDiff
  input = 'lps_single.i'
  csvdiff = 'lps_single_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with LPS spherical formulation that increases the porosity due to an external strain.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./lps_single-jac]
  type = 'PetscJacobianTester'
  input = 'lps_single.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = lps_single
  requirement = 'The Jacobian for the AD lps single problem shall be perfect'
[../]

[./lps_single_split]
  type = CSVDiff
  input = 'lps_single_split.i'
  csvdiff = 'lps_single_split_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and the same stress exponential that is close to combining the models into a single ADViscoplasticityStressUpdate instance.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./lps_single_split-jac]
  type = 'PetscJacobianTester'
  input = 'lps_single_split.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = lps_single_split
  requirement = 'The Jacobian for the AD lps single split problem shall be perfect'
[../]

[./lps_dual]
  type = CSVDiff
  input = 'lps_dual.i'
  csvdiff = 'lps_dual_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and two different stress exponents that increases the porosity due to an external strain.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./lps_dual-jac]
  type = 'PetscJacobianTester'
  input = 'lps_dual.i'
  cli_args = "-snes_test_err 1e-11 Executioner/num_steps=2"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = lps_dual
  requirement = 'The Jacobian for the AD lps dual problem shall be perfect'
[../]

[./gtn_single]
  type = CSVDiff
  input = 'gtn_single.i'
  csvdiff = 'gtn_single_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with GTN formulation that increases the porosity due to an external strain.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./gtn_single-jac]
  type = 'PetscJacobianTester'
  input = 'gtn_single.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = gtn_single
  requirement = 'The Jacobian for the AD gtn single problem shall be perfect'
[../]

[zero]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_zero_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_zero_out Materials/lps/negative_behavior=ZERO'
  detail = 'by setting the porosity to zero.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[initial]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_initial_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_initial_out Materials/lps/negative_behavior=INITIAL_CONDITION'
  detail = 'by setting the porosity to the initial condition.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[exception]
  type = RunException
  input = 'negative_porosity.i'
  expect_err = 'porosity is negative'
  cli_args = 'Materials/lps/negative_behavior=EXCEPTION'
  detail = 'by throwing an exception.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[./3D]
  type = Exodiff
  input = 'pressure_test.i'
  exodiff = 'pressure_test_out.e'
  issues = '#4781 #13260'
  design = 'syntax/BCs/Pressure/index.md'
  requirement = 'The Pressure boundary condition action shall create the objects needed to apply
                   automatic differentiation pressure boundary conditions on a 3D model as
                   demonstrated by correctly computing the response of an elastic small-strain
                   isotropic unit cube with pressure applied on three faces to create a hydrostatic
                   pressure and match non-AD methods.'
[../]

[./3D_Bbar]
  type = Exodiff
  input = 'pressure_test.i'
  exodiff = 'pressure_test_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = '3D'
  issues = '#4781 #8235 #13260'
  design = 'syntax/BCs/Pressure/index.md'
  requirement = 'The Pressure boundary condition action shall create the objects needed to apply
                   automatic differentiation pressure boundary conditions on a 3D model as
                   demonstrated by correctly computing the response of an elastic small-strain
                   isotropic unit cube with pressure applied on three faces to create a hydrostatic
                   pressure using the volumetric locking correction b-bar formulation and match
                   non-AD methods.'
[../]

[./3D-jac]
  type = PetscJacobianTester
  input = 'pressure_test.i'
  run_sim = 'True'
  #ratio_tol = 5e-6
  difference_tol = 5e-7
  cli_args = "Outputs/active=''"
  issues = '#4781 #13260'
  design = 'syntax/BCs/Pressure/index.md'
  requirement = 'The Pressure boundary condition action shall create the objects needed to apply
                   automatic differentiation pressure boundary conditions on a 3D model as
                   demonstrated by correctly computing the response of an elastic small-strain
                   isotropic unit cube with pressure applied on three faces to create a hydrostatic
                   pressure and calculate a perfect Jacobian.'
[../]

[./3D_Bbar-jac]
  type = PetscJacobianTester
  input = 'pressure_test.i'
  run_sim = 'True'
  #ratio_tol = 5e-6
  difference_tol = 5e-7
  cli_args = "GlobalParams/volumetric_locking_correction=true Outputs/active=''"
  issues = '#4781 #8235 #13260'
  design = 'syntax/BCs/Pressure/index.md'
  requirement = 'The Pressure boundary condition action shall create the objects needed to apply
                   automatic differentiation pressure boundary conditions on a 3D model as
                   demonstrated by correctly computing the response of an elastic small-strain
                   isotropic unit cube with pressure applied on three faces to create a hydrostatic
                   pressure using the volumetric locking correction b-bar formulation and calculate
                   a perfect Jacobian.'
[../]

[3D]
  type = Exodiff
  input = 'pressure_test.i'
  exodiff = 'pressure_test_out.e'
  issues = '#4781'
  design = 'syntax/BCs/Pressure/index.md'
  requirement = 'The Pressure boundary condition action shall create the objects needed to apply pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure.'
[]

[3D_Bbar]
  type = Exodiff
  input = 'pressure_test.i'
  exodiff = 'pressure_test_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = '3D'
  issues = '#4781 #8235'
  design = 'syntax/BCs/Pressure/index.md'
  requirement = 'The Pressure boundary condition action shall create the objects needed to apply pressure boundary conditions on a 3D model as demonstrated by correctly computing the response of an elastic small-strain isotropic unit cube with pressure applied on three faces to create a hydrostatic pressure using the volumetric locking correction b-bar formulation.'
[]

[reference]
  type = 'Exodiff'
  input = 'ad_return_mapping_derivative.i'
  exodiff = 'reference.e'
  issues = '#20407'
  design = 'materials/RadialReturnStressUpdate.md'
  requirement = "The return mapping algorithm shall use automatic differentiation to compute the derivative of the yield function with respect to the internal variable, and the solution should be the same as existing hand coded derivative."
[]

[isotropic_plasticity_substepping_error]
  type = 'RunException'
  input = 'isotropic_plasticity_finite_strain.i'
  cli_args = 'Materials/isotropic_plasticity/use_substep=true'
  expect_err = 'Usage of substepping has been requested, but the inelastic model'
  design = 'RadialReturnStressUpdate.md'
  issues = '#14757'
  requirement = 'The system shall return an error if the user requests substepping for a radial return inelastic model that does not implement it yet.'
[]

[./linear-hand-coded]
  type = 'Exodiff'
  input = 'linear-hand-coded.i'
  exodiff = 'linear-out.e'
  absent_out = '3 Nonlinear'
  requirement = 'We shall be able to run a simple linear small-strain problem using a hand-coded Jacobian'
  design = 'ComputeSmallStrain.md'
[../]

[./linear-hand-coded-jac]
  type = 'PetscJacobianTester'
  input = 'linear-hand-coded.i'
  run_sim = 'True'
  ratio_tol = 1e-8
  difference_tol = 1e6 # We have Young's modulus of 1e9 so finite differencing produces a large number
  requirement = 'The Jacobian for the hand-coded problem shall be perfect'
  design = 'ComputeSmallStrain.md'
[../]

[./test]
  type = 'Exodiff'
  input = 'anisotropic_patch_test.i'
  exodiff = 'anisotropic_patch_test_out.e'
  scale_refine = 1
  issues = '#4716 #7555'
  design = 'source/materials/ComputeLinearElasticStress.md source/materials/ComputeSmallStrain.md syntax/Physics/SolidMechanics/QuasiStatic/index.md'
  requirement = 'The mechanics system shall be capable of accurately computing the elastic response of an anisotropic elastic material where 6 components of a symmetric elasticity tensor are output on an irregular patch of elements with total small strain assumptions'
[../]

[./elastic_patch_total_small]
  prereq = elastic_patch_incremental_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeSmallStrain Materials/stress/type=ComputeLinearElasticStress Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeSmallStrain.md ComputeLinearElasticStress.md'
  issues = '#12584'
[../]

[./linear-ad]
  type = 'Exodiff'
  input = 'linear-ad.i'
  exodiff = 'linear-out.e'
  absent_out = '3 Nonlinear'
  prereq = 'linear-hand-coded'
  requirement = 'We shall be able to reproduce the results of the hand-coded simulation using automatic differentiation in the production stress divergence kernel'
  design = 'ADComputeSmallStrain.md'
[../]

[./linear-ad-reverse]
  type = 'Exodiff'
  input = 'linear-ad-reverse-dependency.i'
  exodiff = 'linear-out.e'
  absent_out = '3 Nonlinear'
  prereq = 'linear-ad'
  requirement = 'We shall be able to reproduce the results of the hand-coded simulation using automatic differentiation with reversed stress and strain materials'
  design = 'ADComputeSmallStrain.md'
[../]

[./linear-ad-jac]
  type = 'PetscJacobianTester'
  input = 'linear-ad.i'
  run_sim = 'True'
  ratio_tol = 1e-8
  difference_tol = 1e-4
  requirement = 'The Jacobian for the automatic differentiation problem shall be perfect'
  design = 'ADComputeSmallStrain.md'
[../]

[./linear-ad-jac-reverse]
  type = 'PetscJacobianTester'
  input = 'linear-ad-reverse-dependency.i'
  run_sim = 'True'
  ratio_tol = 1e-8
  difference_tol = 1e6 # We have Young's modulus of 1e9 so finite differencing produces a large number
  requirement = 'The Jacobian for the automatic differentiation problem with reversed stress and strain materials shall be perfect'
  design = 'ADComputeSmallStrain.md'
[../]

[cracking]
  type = Exodiff
  input = cracking.i
  allow_warnings = true #Ignore warning about missing cracked_elasticity_type
  exodiff = cracking_out.e
  custom_cmp = cracking.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in cartesian coordinates using AD and match non-AD methods.'
[]

[cracking_rz]
  type = Exodiff
  input = cracking_rz.i
  exodiff = cracking_rz_out.e
  custom_cmp = cracking_rz.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in rz coordinates using AD and match non-AD methods.'
[]

[cracking_function]
  type = Exodiff
  input = cracking_function.i
  exodiff = cracking_function_out.e
  custom_cmp = cracking_function.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate cracking while the cracking strength is prescribed by an elemental AuxVariable using AD and match non-AD methods.'
[]

[exponential]
  type = Exodiff
  input = cracking_exponential.i
  exodiff = cracking_exponential_out.e
  custom_cmp = cracking_exponential.cmp
  use_old_floor = true
  requirement = 'The MOOSE SolidMechanics module shall simulate exponential stress release using AD and match non-AD methods.'
[]

[rz_exponential]
  type = Exodiff
  input = cracking_rz_exponential.i
  exodiff = cracking_rz_exponential_out.e
  custom_cmp = cracking_rz_exp.cmp
  exodiff_opts = '-steps 0:1200:1'
  valgrind = HEAVY
  requirement = 'The MOOSE SolidMechanics module shall simulate exponential stress relase while using the rz coordinate system using AD and match non-AD methods.'
  method = "!dbg"
[]

[power]
  type = Exodiff
  input = cracking_power.i
  exodiff = cracking_power_out.e
  requirement = 'The MOOSE SolidMechanics module shall demonstrate softening using the power law for smeared cracking using AD and match non-AD methods.'
[]

[multiple_softening]
  type = Exodiff
  input = cracking_multiple_softening.i
  exodiff = cracking_multiple_softening_out.e
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the prescribed softening laws in three directions, power law (x), exponential (y), and abrupt (z) using AD and match non-AD methods.'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[]

[xyz]
  type = Exodiff
  input = cracking_xyz.i
  exodiff = cracking_xyz_out.e
  use_old_floor = true
  custom_cmp = cracking_xyz.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate smeared cracking in the x y and z directions using AD and match non-AD methods.'
[]

[plane_stress]
  type = Exodiff
  input = cracking_plane_stress.i
  exodiff = cracking_plane_stress_out.e
  use_old_floor = true
  custom_cmp = cracking_pln_str.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate smeared cracking under plane stress conditions using AD and match non-AD methods.'
[]

[cracking_rotation]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  max_parallel = 1
  requirement = 'The MOOSE SolidMechanics module shall demonstrate that the smeared cracking model correctly handles finite rotation of cracked elements using AD and match non-AD methods.'
[]

[cracking_rotation_pres_dir_x]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  #Prescribe the first crack to be in x (which doesn't crack), and reorder crack_flags to match original case
  cli_args = 'Materials/cracking_stress/prescribed_crack_directions=x AuxKernels/crack_flags3/component=1 AuxKernels/crack_flags2/component=2'
  max_parallel = 1
  prereq = cracking_rotation
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in x using AD and match non-AD methods.'
[]

[cracking_rotation_pres_dir_z]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  #Prescribe the first crack to be in z (which doesn't crack), and reorder crack_flags to match original case
  cli_args = 'Materials/cracking_stress/prescribed_crack_directions=z AuxKernels/crack_flags3/component=1 AuxKernels/crack_flags2/component=2'
  max_parallel = 1
  prereq = cracking_rotation_pres_dir_x
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in z using AD and match non-AD methods.'
[]

[cracking_rotation_pres_dir_xz]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  #Prescribe the first two cracks to be in x and z (which dosn't crack), and reorder crack_flags to match original case
  cli_args = "Materials/cracking_stress/prescribed_crack_directions='x z' AuxKernels/crack_flags3/component=0 AuxKernels/crack_flags2/component=1 AuxKernels/crack_flags1/component=2"
  max_parallel = 1
  prereq = cracking_rotation_pres_dir_z
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where two cracks are prescribed in x and z using AD and match non-AD methods.'
[]

[ad_multiple_softening_jacobian]
  type = 'PetscJacobianTester'
  input = cracking_multiple_softening.i
  run_sim = 'True'
  cli_args = 'Outputs/exodus=false'
  ratio_tol = 1e-4
  difference_tol = 1
  requirement = 'The MOOSE SolidMechanics module shall compute accurate AD Jacobian of system with multiple softening laws.'
[]

[cracking_err_diagonal]
  prereq = cracking
  type = RunException
  input = cracking.i
  expect_err = "Defaulting to the legacy option of 'DIAGONAL', but the 'FULL' option is preferred"
  requirement = "The ComputeSmearedCrackingStress model shall generate a warning if 'cracked_elasticity_type' is not specified"
[]

[cracking_err_softening]
  prereq = cracking_err_diagonal
  allow_warnings = true #Ignore warning about missing cracked_elasticity_type
  type = RunException
  input = cracking.i
  cli_args = "Materials/elastic_stress/softening_models='abrupt_softening abrupt_softening'"
  expect_err = "Either 1 or 3 softening models must be specified"
  requirement = "The ComputeSmearedCrackingStress model shall generate an error if an invalid number of softening models is specified"
[]

[./mean_complex_jac]
  type = 'PetscJacobianTester'
  input = 'mean_complex.i'
  run_sim = True
  ratio_tol = 1e-7
  difference_tol = 1e-7
  detail = 'using a complex mean thermal expansion coefficient and compute a perfect jacobian'
[../]

[./instantaneous_complex]
  type = CSVDiff
  input = 'instantaneous_complex.i'
  csvdiff = 'instantaneous_complex_out.csv'
  detail = 'using a complex instantaneous thermal expansion coefficient'
[../]

[./instantaneous_complex_jac]
  type = 'PetscJacobianTester'
  input = 'instantaneous_complex.i'
  run_sim = True
  ratio_tol = 1e-7
  difference_tol = 1e-7
  detail = 'using a complex instantaneous thermal expansion coefficient and compute a perfect jacobian'
[../]

[mean_scaling]
  type = CSVDiff
  input = 'mean.i'
  cli_args = 'Outputs/file_base=mean_scaling_out Materials/thermal_expansion_strain/thermal_expansion_scale_factor=1.1'
  csvdiff = 'mean_scaling_out.csv'
  detail = 'using a mean thermal expansion coefficient with a scaling factor for sensitivity studies'
[]

[./mean_complex_jac]
  type = 'PetscJacobianTester'
  input = 'mean_complex.i'
  run_sim = True
  ratio_tol = 1e-7
  difference_tol = 1e-7
  detail = 'using a complex mean thermal expansion coefficient and compute a perfect jacobian'
[../]

[./instantaneous_complex]
  type = CSVDiff
  input = 'instantaneous_complex.i'
  csvdiff = 'instantaneous_complex_out.csv'
  detail = 'using a complex instantaneous thermal expansion coefficient'
[../]

[./instantaneous_complex_jac]
  type = 'PetscJacobianTester'
  input = 'instantaneous_complex.i'
  run_sim = True
  ratio_tol = 1e-7
  difference_tol = 1e-7
  detail = 'using a complex instantaneous thermal expansion coefficient and compute a perfect jacobian'
[../]

[mean_scaling]
  type = CSVDiff
  input = 'mean.i'
  cli_args = 'Outputs/file_base=mean_scaling_out Materials/thermal_expansion_strain/thermal_expansion_scale_factor=1.1'
  csvdiff = 'mean_scaling_out.csv'
  detail = 'using a mean thermal expansion coefficient with a scaling factor for sensitivity studies'
[]

[./mean_complex_jac]
  type = 'PetscJacobianTester'
  input = 'mean_complex.i'
  run_sim = True
  ratio_tol = 1e-7
  difference_tol = 1e-7
  detail = 'using a complex mean thermal expansion coefficient and compute a perfect jacobian'
[../]

[./instantaneous_complex]
  type = CSVDiff
  input = 'instantaneous_complex.i'
  csvdiff = 'instantaneous_complex_out.csv'
  detail = 'using a complex instantaneous thermal expansion coefficient'
[../]

[./instantaneous_complex_jac]
  type = 'PetscJacobianTester'
  input = 'instantaneous_complex.i'
  run_sim = True
  ratio_tol = 1e-7
  difference_tol = 1e-7
  detail = 'using a complex instantaneous thermal expansion coefficient and compute a perfect jacobian'
[../]

[mean_scaling]
  type = CSVDiff
  input = 'mean.i'
  cli_args = 'Outputs/file_base=mean_scaling_out Materials/thermal_expansion_strain/thermal_expansion_scale_factor=1.1'
  csvdiff = 'mean_scaling_out.csv'
  detail = 'using a mean thermal expansion coefficient with a scaling factor for sensitivity studies'
[]

[./exact_spherical]
  type = CSVDiff
  input = exact.i
  csvdiff = exact_spherical_out.csv
  requirement = 'The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.'
[../]

[./exact_spherical-jac]
  type = 'PetscJacobianTester'
  input = 'exact.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  prereq = exact_spherical
  requirement = 'The Jacobian for the AD exact spherical problem shall be perfect'
[../]

[./exact_cylindrical]
  type = CSVDiff
  input = exact.i
  csvdiff = exact_cylindrical_out.csv
  cli_args = 'GlobalParams/pore_shape_model=CYLINDRICAL Outputs/file_base=exact_cylindrical_out'
  prereq = exact_spherical
  requirement = 'The ADViscoplasticityStressUpdate class shall compute a ratio between the gauge stress, equilvalent stress, and hydrostatic stress across a wide swath of exponents and stress states using spherical pore geometry.'
[../]

[./exact_cylindrical-jac]
  type = 'PetscJacobianTester'
  input = 'exact.i'
  cli_args = "-snes_test_err 1e-11 GlobalParams/pore_shape_model=CYLINDRICAL Outputs/file_base=exact_cylindrical_out"
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e4
  prereq = exact_cylindrical
  requirement = 'The Jacobian for the AD exact cylindrical problem shall be perfect'
[../]

[./lps_single]
  type = CSVDiff
  input = 'lps_single.i'
  csvdiff = 'lps_single_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with LPS spherical formulation that increases the porosity due to an external strain.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./lps_single-jac]
  type = 'PetscJacobianTester'
  input = 'lps_single.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = lps_single
  requirement = 'The Jacobian for the AD lps single problem shall be perfect'
[../]

[./lps_single_split]
  type = CSVDiff
  input = 'lps_single_split.i'
  csvdiff = 'lps_single_split_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and the same stress exponential that is close to combining the models into a single ADViscoplasticityStressUpdate instance.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./lps_single_split-jac]
  type = 'PetscJacobianTester'
  input = 'lps_single_split.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = lps_single_split
  requirement = 'The Jacobian for the AD lps single split problem shall be perfect'
[../]

[./lps_dual]
  type = CSVDiff
  input = 'lps_dual.i'
  csvdiff = 'lps_dual_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using two LPS models with spherical formulations and two different stress exponents that increases the porosity due to an external strain.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./lps_dual-jac]
  type = 'PetscJacobianTester'
  input = 'lps_dual.i'
  cli_args = "-snes_test_err 1e-11 Executioner/num_steps=2"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = lps_dual
  requirement = 'The Jacobian for the AD lps dual problem shall be perfect'
[../]

[./gtn_single]
  type = CSVDiff
  input = 'gtn_single.i'
  csvdiff = 'gtn_single_out.csv'
  requirement = 'The ADViscoplasticityStressUpdate class shall compute the viscoplastic response using a single model with GTN formulation that increases the porosity due to an external strain.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[../]

[./gtn_single-jac]
  type = 'PetscJacobianTester'
  input = 'gtn_single.i'
  cli_args = "-snes_test_err 1e-11"
  run_sim = 'True'
  ratio_tol = 3e-7
  difference_tol = 1e8
  prereq = gtn_single
  requirement = 'The Jacobian for the AD gtn single problem shall be perfect'
[../]

[zero]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_zero_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_zero_out Materials/lps/negative_behavior=ZERO'
  detail = 'by setting the porosity to zero.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[initial]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_initial_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_initial_out Materials/lps/negative_behavior=INITIAL_CONDITION'
  detail = 'by setting the porosity to the initial condition.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[exception]
  type = RunException
  input = 'negative_porosity.i'
  expect_err = 'porosity is negative'
  cli_args = 'Materials/lps/negative_behavior=EXCEPTION'
  detail = 'by throwing an exception.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[ad_aniso_plasticity_x_one_ref]
  type = 'CSVDiff'
  input = 'ad_aniso_plasticity_x_one_ref.i'
  csvdiff = 'ad_aniso_plasticity_x_one_ref_out.csv'
  heavy = true
  requirement = 'Anisotropic plasticity and anisotropic elastoplasticity must give almost identical results if elastic behavior is isotropic -- plastic anisotropy'
[]

[ad_aniso_plasticity_x_one]
  type = 'CSVDiff'
  input = 'ad_aniso_plasticity_x_one.i'
  csvdiff = 'ad_aniso_plasticity_x_one_out.csv'
  heavy = true
  requirement = 'Anisotropic plasticity and anisotropic elastoplasticity must give almost identical results if elastic behavior is isotropic -- elastoplastic anisotropy'
[]

[ad_aniso_plasticity_x_one_light]
  type = 'RunApp'
  input = 'ad_aniso_plasticity_x_one.i'
  # rush through purely elastic phase to achieve inelastic deformation in the reduced test time
  cli_args = 'Executioner/num_steps=3 Executioner/TimeStepper/dt=1.0e-4 Executioner/TimeStepper/time_t=\'0 3.43e-5 10\' Executioner/TimeStepper/time_dt=\'1.0e-4 1.0e-7 1.0e-7\''
  requirement = 'The system shall be able to solve anisotropic plasticity and anisotropic elastoplasticity problems with elastoplastic anisotropy'
[]

[ad_uniaxial_x_linear]
  type = 'CSVDiff'
  input = 'ad_uniaxial_x.i'
  csvdiff = 'ad_uniaxial_x_out.csv'
  heavy = true
  requirement = 'Uniaxial tensile test run in x direction with anisotropic elasticity and linear strain hardening with automatic differentiation'
[]

[ad_uniaxial_y_linear]
  type = 'CSVDiff'
  input = 'ad_uniaxial_y.i'
  csvdiff = 'ad_uniaxial_y_out.csv'
  heavy = true
  requirement = 'Uniaxial tensile test run in y direction with anisotropic elasticity and linear strain hardening with automatic differentiation'
[]

[ad_uniaxial_x_non_linear]
  type = 'CSVDiff'
  input = 'ad_uniaxial_x_non_linear.i'
  csvdiff = 'ad_uniaxial_x_non_linear_out.csv'
  heavy = true
  requirement = 'Uniaxial tensile test run in x direction with anisotropic elasticity and non-linear strain hardening with automatic differentiation'
[]

[3D_hoop_strain_comparison]
  type = 'CSVDiff'
  input = 'hoop_strain_comparison.i'
  csvdiff = 'hoop_strain_comparison_out.csv'
  heavy = true
  requirement = 'Compute hoop plastic strain in a cylinder and compare it for two elements located separately in hoop direction'
[]

[3D_hoop_strain_comparison_coarse_xaxis]
  type = 'CSVDiff'
  input = 'hoop_strain_comparison_coarse_xaxis.i'
  csvdiff = 'hoop_strain_comparison_coarse_xaxis_out.csv'
  # Added max_time so that it does not TIMEOUT in debug test
  max_time = 600
  requirement = 'Compute hoop plastic strain in a cylinder oriented along the x axis and compare it for two elements located separately in hoop direction for coarsely meshed model'
[]

[3D_hoop_strain_comparison_coarse_yaxis]
  type = 'CSVDiff'
  input = 'hoop_strain_comparison_coarse_yaxis.i'
  csvdiff = 'hoop_strain_comparison_coarse_yaxis_out.csv'
  # Added max_time so that it does not TIMEOUT in debug test
  max_time = 600
  requirement = 'Compute hoop plastic strain in a cylinder oriented along the y axis and compare it for two elements located separately in hoop direction for coarsely meshed model'
[]

[3D_hoop_strain_comparison_coarse_zaxis]
  type = 'CSVDiff'
  input = 'hoop_strain_comparison_coarse_zaxis.i'
  csvdiff = 'hoop_strain_comparison_coarse_zaxis_out.csv'
  # Added max_time so that it does not TIMEOUT in debug test
  max_time = 600
  requirement = 'Compute hoop plastic strain in a cylinder oriented along the z axis and compare it for two elements located separately in hoop direction for coarsely meshed model'
[]

[anis_plasticity_test]
  type = 'CSVDiff'
  input = 'anis_plasticity_test.i'
  csvdiff = 'anis_plasticity_test_out.csv'
  requirement = 'Anisotropic plasticity must yield same results as finite strain elasticity if yield condition is never met'
[]

[anis_elasticity_test]
  type = 'CSVDiff'
  input = 'anis_elasticity_test.i'
  csvdiff = 'anis_elasticity_test_out.csv'
  requirement = 'Anisotropic plasticity must yield same results as finite strain elasticity if yield condition is never met --elasticity'
[]

[ad_aniso_plasticity_x]
  type = 'CSVDiff'
  abs_zero = 1.0e-9
  rel_err = 1.0e-5
  heavy = true
  input = 'ad_aniso_plasticity_x.i'
  csvdiff = 'ad_aniso_plasticity_x_out.csv'
  requirement = 'Anisotropic plasticity with isotropic elasticity must reproduce simplified verification problem along x axis'
[]

[ad_aniso_plasticity_x_rotate]
  type = 'CSVDiff'
  abs_zero = 1.0e-9
  rel_err = 1.0e-5
  heavy = true
  input = 'ad_aniso_plasticity_x_rotate.i'
  csvdiff = 'ad_aniso_plasticity_x_rotate_out.csv'
  requirement = 'Anisotropic plasticity with hill tensor rotation must produce simplified verification problem along x axis'
[]

[ad_aniso_plasticity_y]
  type = 'CSVDiff'
  abs_zero = 1.0e-9
  rel_err = 1.0e-5
  heavy = true
  input = 'ad_aniso_plasticity_y.i'
  csvdiff = 'ad_aniso_plasticity_y_out.csv'
  requirement = 'Anisotropic plasticity with isotropic elasticity must reproduce simplified verification problem along y axis'
[]

[./test]
  type = 'CSVDiff'
  input = 'orthotropic.i'
  csvdiff = 'orthotropic_out.csv'
  rel_err = 1.0E-4
  abs_zero = 1.0E-4
  requirement = 'The system shall be capable of simulating materials that exhibit orthotropic plasticity with constant hardening and linear strain applied in the x and y directions.'
[../]

[./power_rule]
  type = 'CSVDiff'
  input = 'powerRuleHardening.i'
  csvdiff = 'powerRuleHardening_out.csv'
  rel_err = 1.0E-2
  abs_zero = 1.0E-2
  requirement = 'The system shall be capable of simulating materials that exhibit orthotropic plasticity with power rule hardening and linear strain applied in the x direction.'
[../]

[./ranktwoscalaraux]
  type = 'Exodiff'
  input = 'ranktwoscalaraux.i'
  exodiff = 'ranktwoscalaraux_out.e'
  design = 'RankTwoScalarAux.md'
  issues = '#4774'
  requirement = 'The system shall compute the VonMises value of a RankTwoTensor'
[../]

[./principalstress]
  type = 'Exodiff'
  input = 'principalstress.i'
  exodiff = 'principalstress_out.e'
  design = 'RankTwoScalarAux.md'
  issues = '#5516'
  requirement = 'The system shall allow RankTwoScalarAux to output principal stresses'
[../]

[volumetric_eigenstrain]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain.i'
  csvdiff = 'volumetric_eigenstrain_out.csv'
  requirement = "The system shall correctly compute an eigenstrain tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain."
  design = "source/materials/ComputeVolumetricEigenstrain.md RankTwoScalarAux.md"
  issues = "#8615 #11743"
[]

[ad_volumetric_eigenstrain]
  type = 'CSVDiff'
  input = 'ad_volumetric_eigenstrain.i'
  csvdiff = 'ad_volumetric_eigenstrain_out.csv'
  requirement = "The system shall correctly compute an eigenstrain using AD tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain."
  design = "source/materials/ADComputeVolumetricEigenstrain.md RankTwoScalarAux.md"
  issues = "#8615 #11743 #26880"
[]

[volumetric_mechanical]
  type = 'CSVDiff'
  input = 'volumetric_mechanical.i'
  csvdiff = 'volumetric_mechanical_out.csv'
  requirement = "The volumetric strain computed using RankTwoScalarAux for a unit cube with imposed displacements shall be identical to that obtained by imposing an eigenstrain that causes the same deformation of that model."
  design = "source/materials/ComputeVolumetricEigenstrain.md RankTwoScalarAux.md"
  issues = "#8615 #11743"
[]

[./tensorelasticenergyaux]
  type = 'Exodiff'
  input = 'tensorelasticenergyaux.i'
  exodiff = 'tensorelasticenergyaux_out.e'
  design = 'ElasticEnergyAux.md'
  issues = '#13635'
  requirement = 'The system shall compute the local elastic energy'
[../]

[./elastic_patch]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#458'
[../]

[./elastic_patch_incremental_small]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584'
[../]

[./elastic_patch_total_small]
  prereq = elastic_patch_incremental_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Materials/strain/type=ComputeSmallStrain Materials/stress/type=ComputeLinearElasticStress Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an total small-strain calculation.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeSmallStrain.md ComputeLinearElasticStress.md'
  issues = '#12584'
[../]

[./elastic_patch_incremental_small_no_disp_mesh]
  prereq = elastic_patch_total_small
  type = 'Exodiff'
  input = 'elastic_patch.i'
  cli_args = 'Mesh/use_displaced_mesh=false Materials/strain/type=ComputeIncrementalStrain Kernels/SolidMechanics/use_displaced_mesh=false Outputs/file_base=elastic_patch_small_out'
  exodiff = 'elastic_patch_small_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes using an incremental small-strain calculation with no displaced mesh created.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeIncrementalStrain.md ComputeFiniteStrainElasticStress.md'
  issues = '#12584 #12580'
[../]

[./elastic_patch_Bbar]
  type = 'Exodiff'
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'elastic_patch'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when using volumetric locking correction.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[./elastic_patch_2Procs]
  type = Exodiff
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  min_parallel = 2
  prereq = 'elastic_patch_Bbar'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when running on 2 processors in parallel.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#458'
[../]

[./elastic_patch_2Procs_Bbar]
  type = Exodiff
  input = 'elastic_patch.i'
  exodiff = 'elastic_patch_out.e'
  min_parallel = 2
  prereq = 'elastic_patch_2Procs'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular hexes when employing volumetric locking correction and running on 2 processors in parallel.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md VolumetricLocking.md'
  issues = '#458'
[../]

[./elastic_patch_quadratic]
  type = Exodiff
  input = 'elastic_patch_quadratic.i'
  exodiff = 'elastic_patch_quadratic_out.e'
  requirement = 'The tensor mechanics module shall have the ability to compute spatially uniform stresses under prescribed linearly varying displacements on a set of irregular 20-noded quadratic hexes.'
  design = 'ElasticEnergyAux.md ComputeIsotropicElasticityTensor.md ComputeFiniteStrainElasticStress.md'
  issues = '#620'
[../]

[./2_block_action]
  type = 'Exodiff'
  input = '2_block.i'
  exodiff = '2_block_out.e'

  requirement = "The LineElementAction class shall correctly create the objects required for a mechanics simulation using beam or truss elements."
[../]

[./2_block_common_action]
  type = 'Exodiff'
  input = '2_block_common.i'
  exodiff = '2_block_out.e'
  prereq = '2_block_action'

  requirement = "The LineElementAction class shall correctly set the common parameters in the action subblocks."
[../]

[./beam_action_test1]
  type = 'RunException'
  input = 'beam_action_chk.i'
  expect_err = 'LineElementAction: A vector of displacement variable names should be provided as'

  requirement = "The LineElementAction class shall produce an error when the displacement variables are not provided by the user."
[../]

[./beam_action_test2]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x"
    Physics/SolidMechanics/LineElement/QuasiStatic/block_1/use_displaced_mesh=true Physics/SolidMechanics/LineElement/QuasiStatic/block_1/strain_type=small Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotation_type=small'
  expect_err = 'LineElementAction: Wrong combination of `use_displaced_mesh`, `strain_type` and `rotation_type`.'

  requirement = "The LineElementAction class shall produce an error if the user provided inputs for `strain_type`, `rotation_type` and `use_displaced_mesh` parameters are not compatible."
[../]

[./beam_action_test3]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/save_in="res_x res_y"'
  expect_err = 'LineElementAction: Number of save_in variables should equal to the number of displacement variables'

  requirement = "The LineElementAction class shall produce an error if the number of variables listed in the `save_in` parameter differs from the number of displacement variables."
[../]

[./beam_action_test4]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/diag_save_in="res_x res_y"'
  expect_err = 'LineElementAction: Number of diag_save_in variables should equal to the number of displacement variables'

  requirement = "The LineElementAction class shall produce an error if the number of variables listed in the `diag_save_in` parameter differs from the number of displacement variables."
[../]

[./beam_action_test5]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements=""'
  expect_err = 'LineElementAction: Rotational variable names should be provided for beam elements using `rotations` parameter'

  requirement = "The LineElementAction class shall produce an error if the names for the rotational degrees of freedom are not provided by the user."
[../]

[./beam_action_test6]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations=""'
  expect_err = 'LineElementAction: Number of rotational and displacement variable names provided as input for beam should be same.'

  requirement = "The LineElementAction class shall produce an error if the number of rotational variables provided as input differs from the number of displacement variables."
[../]

[./beam_action_test7]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x"'
  expect_err = 'LineElementAction: `y_orientation`, `area`, `Iy` and `Iz` should be provided for'

  requirement = "The LineElementAction class shall produce an error if the moment of inertia, area and orientation of the beam are not provided as input."
[../]

[./beam_action_test8]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0'
  expect_err = 'LineElementAction: Variable names for translational and rotational velocities and accelerations should be provided as input to perform dynamic simulation using beam elements using `velocities`, `accelerations`, `rotational_velocities`'

  requirement = "The LineElementAction class shall produce an error if translational and rotational velocities and accelerations are not provided as input for dynamic simulations using beam elements."
[../]

[./beam_action_test9]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotational_velocities="rot_vel_x rot_vel_y"'
  expect_err = 'LineElementAction: Number of translational and rotational velocity and acceleration variable names provided as input for the beam should be same as number of displacement variables'

  requirement = "The LineElementAction class shall produce an error if the number of translational and rotational velocities and accelerations differs from the number of displacement variables."
[../]

[./beam_action_test10]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotational_velocities="rot_vel_x"'
  expect_err = 'LineElementAction: Newmark time integration parameters `beta` and `gamma` should be provided as input to perform dynamic simulations using beams.'

  requirement = "The LineElementAction class shall produce an error if Newmark time integration parameters (`beta` and `gamma`) are not provided as input for dynamic simulations using beam elements."
[../]

[./beam_action_test11]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotational_velocities="rot_vel_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/beta=0.25'
  expect_err = 'LineElementAction: Either name of the density material property or a constant density value should be provided as input using `density` for creating the consistent mass/inertia matrix required for dynamic beam simulation.'

  requirement = "The LineElementAction class shall produce an error if density is not provided as input for dynamic beam simulations using beams elements with consistent mass/inertia matrix."
[../]

[./beam_action_test12]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotational_velocities="rot_vel_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/beta=0.25 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/density=1.0'
  expect_err = 'LineElementAction: `nodal_mass` or `nodal_mass_file` should be provided as input to calculate inertial forces on beam due to nodal mass.'

  requirement = "The LineElementAction class shall produce an error if nodal mass is not provided as input for dynamic beam simulations using beam elements with nodal mass matrix."
[../]

[./beam_action_test13]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotational_velocities="rot_vel_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/beta=0.25 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/density=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/nodal_mass=0.1'
  expect_err = 'LineElementAction: `nodal_Ixx`, `nodal_Iyy`, `nodal_Izz` should be provided as input to calculate inertial torque on beam due to nodal inertia.'

  requirement = "The LineElementAction class shall produce an error if nodal inertia is not provided as input for dynamic beam simulations using beam elements with nodal inertia matrix."
[../]

[./beam_action_test14]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotational_velocities="rot_vel_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/beta=0.25 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/density=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/nodal_mass=0.1 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/nodal_Ixx=0.1 Physics/SolidMechanics/LineElement/QuasiStatic/block_all/block="1 2"'
  expect_err = 'LineElementAction: The block restrictions in the LineElement actions must be non-overlapping.'

  requirement = "The LineElementAction class shall produce an error if multiple subblocks specify properties for the same mesh block."
[../]

[./beam_action_test15]
  type = 'RunException'
  input = 'beam_action_chk.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block_1/displacements="disp_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotations="rot_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/area=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/rotational_velocities="rot_vel_x" Physics/SolidMechanics/LineElement/QuasiStatic/block_1/beta=0.25 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/density=1.0 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/nodal_mass=0.1 Physics/SolidMechanics/LineElement/QuasiStatic/block_1/nodal_Ixx=0.1'
  expect_err = 'LineElementAction: No LineElement action can be block unrestricted if more than one LineElement action is specified.'

  requirement = "The LineElementAction class shall produce an error if an action subblock is mesh block restricted while another is not."
[../]

[./beam_action_test16]
  type = 'RunException'
  input = '2_block_common.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/dynamic_nodal_translational_inertia=true'
  expect_err = 'LineElementAction: Variable names for translational and rotational velocities and accelerations should be provided as input to perform dynamic simulation using beam elements'

  requirement = "The LineElementAction class shall produce an error if `dynamic_nodal_translational_inertia` is set to true in the common action block but the subblocks do not have the parameters required for a dynamic beam simulation using beam elements."
[../]

[./add_dynamic_variables_action]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_dyn_variable_action.i'
  exodiff = 'dyn_euler_small_added_mass_out.e'
  prereq = 'dyn_euler_added_mass_gravity_2'
  superlu = true
  requirement = "The LineElementAction shall create the translational and rotational velocities and accelerations required for a dynamic simulation using beam elements."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
[../]

[./dyn_euler_rayleigh_hht_action]
  type = 'Exodiff'
  input = 'dyn_euler_small_rayleigh_hht_action.i'
  exodiff = 'dyn_euler_small_rayleigh_hht_out.e'
  prereq = 'dyn_euler_rayleigh_hht'
  requirement = "The LineElementAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and a consistent mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
  rel_err = 2e-5
[../]

[./dyn_euler_added_mass_inertia_damping_action]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_inertia_damping_action.i'
  exodiff = 'dyn_euler_small_added_mass_inertia_damping_out.e'
  prereq = 'dyn_euler_added_mass_inertia_damping'
  superlu = true
  requirement = "The LineElmentAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and nodal mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
[../]

[./error_16]
  type = 'RunException'
  input = 'dyn_euler_small_rayleigh_hht_action.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/all/add_dynamic_variables=false Outputs/csv=false Outputs/exodus=false'
  expect_err = "LineElementAction: When using 'dynamic_consistent_inertia', 'dynamic_nodal_rotational_inertia' or '_dynamic_nodal_translational_inertia', the velocity and acceleration AuxVariables and the corresponding AuxKernels are automatically set by"

  requirement = "The LineElementAction class shall produce an error if `add_dynamic_variables` option is set to false while `dynamic_consistent_inertia`, `dynamic_nodal_rotational_inertia` or `dynamic_nodal_translational_inertia` options are set to true."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
[../]

[./frictionless_constraint]
  type = 'CSVDiff'
  input = 'frictionless_constraint.i'
  csvdiff = 'frictionless_constraint_out.csv'
  requirement = "The mechanics system shall accurately predict the displacement of a beam element with a frictionless contact constraint."
[../]

[./glued_constraint]
  type = 'CSVDiff'
  input = 'glued_constraint.i'
  csvdiff = 'glued_constraint_out.csv'
  requirement = "The mechanics system shall accurately predict the displacement of a beam element with a glued contact constraint."
[../]

[./frictional_constraint]
  type = 'CSVDiff'
  input = 'frictional_constraint.i'
  csvdiff = 'frictional_constraint_out.csv'
  requirement = "The mechanics system shall accurately predict the displacement of a beam element with a frictional contact constraint."
[../]

[./dyn_euler]
  type = 'Exodiff'
  input = 'dyn_euler_small.i'
  exodiff = 'dyn_euler_small_out.e'
  verification = 'beam_vandv.md'
  requirement = "The mechanics system shall correctly predict the natural frequencies of an Euler-Bernoulli beam modeled using beam elements with consistent mass/inertia."
[../]

[./dyn_timoshenko]
  type = 'Exodiff'
  input = 'dyn_timoshenko_small.i'
  exodiff = 'dyn_timoshenko_small_out.e'
  verification = 'beam_vandv.md'
  requirement = "The mechanics system shall correctly predict the natural frequencies of a Timoshenko beam modeled using beam elements with consistent mass/inertia."
[../]

[./dyn_euler_rayleigh_hht]
  type = 'Exodiff'
  input = 'dyn_euler_small_rayleigh_hht.i'
  exodiff = 'dyn_euler_small_rayleigh_hht_out.e'
  requirement = "The mechanics system shall correctly predict the natural frequencies of an Euler-Bernoulli beam modeled using beam elements in the presence of Rayleigh damping and numerical damping introduced by Hilber-Hughes-Taylor (HHT) time integration."
  rel_err = 2e-5
[../]

[./dyn_euler_rayleigh_hht_ti]
  type = 'Exodiff'
  input = 'dyn_euler_small_rayleigh_hht_ti.i'
  exodiff = 'dyn_euler_small_rayleigh_hht_out.e'
  rel_err = 2.1e-5

  allow_warnings = True
  requirement = "The mechanics system shall correctly predict the natural frequencies of an Euler-Bernoulli beam modeled using beam elements in the presence of Rayleigh damping and numerical damping introduced by Hilber-Hughes-Taylor (HHT) time integration when using the velocity and acceleration computed using the Newmark-Beta time integrator."
  issues = "#12185"
  prereq = 'dyn_euler_rayleigh_hht_action'
[../]

[./dyn_euler_added_mass]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass.i'
  exodiff = 'dyn_euler_small_added_mass_out.e'
  superlu = true
  requirement = "The mechanics system shall correctly predict the natural frequencies of a massless Euler-Bernoulli beam modeled using beam elements with a nodal masses placed at the ends."
  verification = 'beam_vandv.md'
  petsc_version = '>=3.8'
[../]

[./dyn_euler_added_mass_file]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_file.i'
  cli_args = "NodalKernels/x_inertial/nodal_mass_file=nodal_mass.csv"
  exodiff = 'dyn_euler_small_added_mass_out.e'
  prereq = 'dyn_euler_added_mass'
  superlu = true
  requirement = "The mechanics system shall correctly predict the natural frequencies of a massless Euler-Bernoulli beam modeled using beam elements with added nodal masses when the location and values of the masses are provided using a csv file."
[../]

[./dyn_euler_added_mass_gravity]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_gravity.i'
  cli_args = "NodalKernels/force_y2/mass=0.01899772"
  exodiff = 'dyn_euler_small_added_mass_out.e'
  prereq = 'dyn_euler_added_mass_file'
  superlu = true
  requirement = "The mechanics system shall correctly model the response of a beam modeled using beam elements when gravitational force (proportional to nodal mass) is applied to the beam."
[../]

[./dyn_euler_added_mass_gravity_2]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_gravity.i'
  cli_args = "NodalKernels/force_y2/nodal_mass_file=nodal_mass.csv"
  exodiff = 'dyn_euler_small_added_mass_out.e'
  prereq = 'dyn_euler_added_mass_gravity'
  superlu = true
  requirement = "The mechanics system shall correctly model the response of a beam modeled using beam elements under gravitational force when the nodal mass distribution is provided using a csv file."
[../]

[./add_dynamic_variables_action]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_dyn_variable_action.i'
  exodiff = 'dyn_euler_small_added_mass_out.e'
  prereq = 'dyn_euler_added_mass_gravity_2'
  superlu = true
  requirement = "The LineElementAction shall create the translational and rotational velocities and accelerations required for a dynamic simulation using beam elements."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
[../]

[./dyn_euler_added_mass_inertia_damping]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_inertia_damping.i'
  exodiff = 'dyn_euler_small_added_mass_inertia_damping_out.e'
  superlu = true
  requirement = "The mechanics system shall correctly model the response of a beam modeled using beam elements in the presence of nodal mass, nodal inertia and Rayleigh damping."
  verification = 'beam_vandv.md'
  petsc_version = '>=3.8'
[../]

[./dyn_euler_added_mass_inertia_damping_ti]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_inertia_damping_ti.i'
  exodiff = 'dyn_euler_small_added_mass_inertia_damping_out.e'
  superlu = true
  requirement = "The mechanics system shall correctly model the response of a beam modeled using beam elements in the presence of nodal mass, nodal inertia and Rayleigh damping when using the velocity and accelerations computed by the Newmark-Beta time integrator."
  issues = "#12185"
  prereq = "dyn_euler_added_mass_inertia_damping_action"
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./dyn_euler_rayleigh_hht_action]
  type = 'Exodiff'
  input = 'dyn_euler_small_rayleigh_hht_action.i'
  exodiff = 'dyn_euler_small_rayleigh_hht_out.e'
  prereq = 'dyn_euler_rayleigh_hht'
  requirement = "The LineElementAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and a consistent mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
  rel_err = 2e-5
[../]

[./dyn_euler_added_mass_inertia_damping_action]
  type = 'Exodiff'
  input = 'dyn_euler_small_added_mass_inertia_damping_action.i'
  exodiff = 'dyn_euler_small_added_mass_inertia_damping_out.e'
  prereq = 'dyn_euler_added_mass_inertia_damping'
  superlu = true
  requirement = "The LineElmentAction shall correctly create the input blocks required for a dynamic beam simulation using beam elements and nodal mass/inertia matrix in the presence of Rayleigh damping and numerical damping in the form of Hilber-Hughes-Taylor (HHT) time integration."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
[../]

[./dyn_euler_added_mass2]
  type = 'CSVDiff'
  input = 'dyn_euler_small_added_mass2.i'
  csvdiff = 'dyn_euler_small_added_mass2_out.csv'

  requirement = "The mechanics system shall correctly predict the natural frequency of a cantilever beam modeled using beam elements with a mass at the free end."
[../]

[./error_1]
  type = 'RunException'
  input = 'dyn_euler_small.i'
  cli_args = "Kernels/inertial_force_x/rotations='rot_x rot_y' Outputs/csv=false Outputs/exodus=false"
  expect_err = "InertialForceBeam: The number of variables supplied in 'displacements' and 'rotations' must match."

  requirement = "The InertialForceBeam class shall produce an error if the number of variables provided for rotations differs from that provided for displacements."
[../]

[./error_2]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_inertia_damping.i'
  cli_args = "NodalKernels/rot_x_inertial/rotational_velocities='rot_vel_x rot_vel_y' Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalRotationalInertia: rotational_velocities and rotational_accelerations should be same size as rotations."
  superlu = true
  requirement = "The NodalRotatioanlInertia class shall produce an error if the number of rotational velocities and accelerations provided as input differ from the number of rotations."
[../]

[./error_3]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_inertia_damping.i'
  cli_args = "NodalKernels/rot_x_inertial/Ixx=1 NodalKernels/rot_x_inertial/Iyy=1 NodalKernels/rot_x_inertial/Izz=1 NodalKernels/rot_x_inertial/Ixy=1 Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalRotationalInertia: The moment of inertia tensor should be positive definite."
  superlu = true
  requirement = "The NodalRotationalInertia class shall produce an error if the user provided nodal inertia is not positive definite."
[../]

[./error_4]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_inertia_damping.i'
  cli_args = "NodalKernels/rot_x_inertial/x_orientation='2 0 0' NodalKernels/rot_x_inertial/y_orientation='0 1 0' Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalRotationalInertia: x_orientation and y_orientation must be unit vectors."
  superlu = true
  requirement = "The NodalRotatioanlInertia class shall produce an error if the user provided x and y orientations are not unit vectors."
[../]

[./error_5]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_inertia_damping.i'
  cli_args = "NodalKernels/rot_x_inertial/x_orientation='1 0 0' NodalKernels/rot_x_inertial/y_orientation='1 0 0' Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalRotationalInertia: x_orientation and y_orientation should be perpendicular to each other."
  superlu = true
  requirement = "The NodalRotatioanlInertia class shall produce an error if the user provided x and y orientations are not perpendicular to each other."
[../]

[./error_6]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_inertia_damping.i'
  cli_args = "NodalKernels/rot_x_inertial/x_orientation='1 0 0' Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalRotationalInertia: Both x_orientation and y_orientation should be provided if x_orientation or y_orientation is different from global x or y direction, respectively."
  superlu = trues
  requirement = "The NodalRotatioanlInertia class shall produce an error if only x or y orientation is provided as input by the user."
[../]

[./error_7]
  type = 'RunException'
  input = 'dyn_euler_small.i'
  cli_args = "Kernels/inertial_force_x/accelerations='accel_x accel_y' Outputs/csv=false Outputs/exodus=false"
  expect_err = "InertialForceBeam: The number of variables supplied in 'velocities', 'accelerations', 'rotational_velocities' and 'rotational_accelerations' must match the number of displacement variables."

  requirement = "The InertialForceBeam class shall produce an error if the number of translational and rotational velocities and accelerations provided as input differ from the number of displacement variables."
[../]

[./error_8]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_file.i'
  cli_args = "NodalKernels/x_inertial/nodal_mass_file=nodal_mass.csv NodalKernels/x_inertial/mass=2.0 Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalTranslationalInertia: Please provide either mass or nodal_mass_file as input, not both."
  superlu = true
  requirement = "The NodalTranslationalInertia class shall produce an error if nodal mass is provided as input both as a constant value and also using a csv file."
[../]

[./error_9]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_file.i'
  cli_args = "Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalTranslationalInertia: Please provide either mass or nodal_mass_file as input."
  superlu = true
  requirement = "The NodalTranslationalInertia class shall produce an error if nodal mass is not provided as input either as a constant value or using a csv file."
[../]

[./error_10]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_file.i'
  cli_args = "NodalKernels/x_inertial/nodal_mass_file=nodal_mass_col_test.csv Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalTranslationalInertia: The number of columns in"
  superlu = true
  requirement = "The NodalTranslationalInertia class shall produce an error if the number of columns in the nodal mass file is not 4."
[../]

[./error_11]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_file.i'
  cli_args = "NodalKernels/x_inertial/nodal_mass_file=nodal_mass.csv NodalKernels/x_inertial/boundary='right' Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalTranslationalInertia: Out of 2 nodal positions in"
  superlu = true
  requirement = "The NodalTranslationalInertia class shall produce an error if all the nodal positions provided in the nodal mass file cannot be found in the given boundary or mesh block."
[../]

[./error_12]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_gravity.i'
  cli_args = "NodalKernels/force_y2/nodal_mass_file=nodal_mass.csv NodalKernels/force_y2/mass=2.0 Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalGravity: Please provide either mass or nodal_mass_file as input, not both."
  superlu = true
  requirement = "The NodalGravity class shall produce an error if nodal mass is provided as input both as a constant value and also using a csv file."
[../]

[./error_13]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_gravity.i'
  cli_args = "Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalGravity: Please provide either mass or nodal_mass_file as input."
  superlu = true
  requirement = "The NodalGravity class shall produce an error if nodal mass is not provided as input either as a constant value or using a csv file."
[../]

[./error_14]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_gravity.i'
  cli_args = "NodalKernels/force_y2/nodal_mass_file=nodal_mass_col_test.csv Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalGravity: The number of columns in"
  superlu = true
  requirement = "The NodalGravity class shall produce an error if the number of columns in the nodal mass file is not 4."
[../]

[./error_15]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_gravity.i'
  cli_args = "NodalKernels/force_y2/nodal_mass_file=nodal_mass.csv NodalKernels/force_y2/boundary='right' Outputs/csv=false Outputs/exodus=false"
  expect_err = "NodalGravity: Out of 2 nodal positions in"
  superlu = true
  requirement = "The NodalGravity class shall produce an error if all the nodal positions provided in the nodal mass file cannot be found in the given boundary or mesh block."
[../]

[./error_16]
  type = 'RunException'
  input = 'dyn_euler_small_rayleigh_hht_action.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/all/add_dynamic_variables=false Outputs/csv=false Outputs/exodus=false'
  expect_err = "LineElementAction: When using 'dynamic_consistent_inertia', 'dynamic_nodal_rotational_inertia' or '_dynamic_nodal_translational_inertia', the velocity and acceleration AuxVariables and the corresponding AuxKernels are automatically set by"

  requirement = "The LineElementAction class shall produce an error if `add_dynamic_variables` option is set to false while `dynamic_consistent_inertia`, `dynamic_nodal_rotational_inertia` or `dynamic_nodal_translational_inertia` options are set to true."
  design = "C0TimoshenkoBeam.md LineElement/QuasiStatic/index.md"
[../]

[./error_17]
  type = 'RunException'
  input = 'dyn_euler_small_added_mass_inertia_damping_action.i'
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/all/nodal_mass_file=nodal_mass.csv Outputs/csv=false Outputs/exodus=false'
  expect_err = "NodalTranslationalInertia: Please provide either mass or nodal_mass_file as input, not both"
  superlu = true
  requirement = "The NodalTranslationalInertia class shall produce an error if nodal mass is provided as input both as constant value and also using a csv file."
[../]

[./timoshenko_small_strain_y]
  type = 'Exodiff'
  input = 'timoshenko_small_strain_y.i'
  exodiff = 'timoshenko_small_strain_y_out.e'
  verification = 'beam_vandv.md'
  requirement = "The mechanics system shall accurately predict the static bending response of a Timoshenko beam modeled using beam elements under small deformations in the y direction."
[../]

[./timoshenko_small_strain_z]
  type = 'Exodiff'
  input = 'timoshenko_small_strain_z.i'
  exodiff = 'timoshenko_small_strain_z_out.e'

  requirement = "The mechanics system shall accurately predict the static bending response of a Timoshenko beam modeled using beam elements under small deformations in the z direction."
[../]

[./euler_small_strain_y]
  type = 'Exodiff'
  input = 'euler_small_strain_y.i'
  exodiff = 'euler_small_strain_y_out.e'
  verification = 'beam_vandv.md'
  requirement = "The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under small deformations in the y direction."
[../]

[./euler_small_strain_z]
  type = 'Exodiff'
  input = 'euler_small_strain_z.i'
  exodiff = 'euler_small_strain_z_out.e'

  requirement = "The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under small deformations in the z direction."
[../]

[./euler_finite_rot_y]
  type = 'Exodiff'
  input = 'euler_finite_rot_y.i'
  exodiff = 'euler_finite_rot_y_out.e'
  verification = 'beam_vandv.md'
  requirement = "The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under finite deformations in the y direction."
[../]

[./euler_finite_rot_z]
  type = 'Exodiff'
  input = 'euler_finite_rot_z.i'
  exodiff = 'euler_finite_rot_z_out.e'

  requirement = "The mechanics system shall accurately predict the static bending response of a Euler-Bernoulli beam modeled using beam elements under finite deformations in the z direction."
[../]

[./euler_small_y_with_action]
  type = 'Exodiff'
  input = 'euler_small_strain_y_action.i'
  exodiff = 'euler_small_strain_y_out.e'
  prereq = euler_small_strain_y

  requirement = "The LineElementAction class shall accurately create the objects required to model the static bending response of an Euler-Bernoulli beam modeled using beam elements under small deformations."
[../]

[./euler_finite_y_with_action]
  type = 'Exodiff'
  input = 'euler_finite_rot_y_action.i'
  exodiff = 'euler_finite_rot_y_out.e'
  prereq = euler_finite_rot_y

  requirement = "The LineElementAction class shall accurately create the objects required to model the static bending response of an Euler-Bernoulli beam modeled using beam elements under finite deformations."
[../]

[./euler_pipe_axial_disp]
  type = 'CSVDiff'
  input = 'euler_pipe_axial_disp.i'
  csvdiff = 'euler_pipe_axial_disp_out.csv'

  requirement = "The mechanics system shall accurately predict the axial displacement of an Euler-Bernoulli pipe modeled using beam elements."
[../]

[./euler_pipe_axial_force]
  type = 'CSVDiff'
  input = 'euler_pipe_axial_force.i'
  csvdiff = 'euler_pipe_axial_force_out.csv'
  verification = 'beam_vandv.md'
  requirement = "The mechanics system shall accurately predict the axial forces on an Euler-Bernoulli pipe modeled using beam elements."
[../]

[./euler_pipe_bend]
  type = 'CSVDiff'
  input = 'euler_pipe_bend.i'
  csvdiff = 'euler_pipe_bend_out.csv'

  requirement = "The mechanics system shall accurately predict the bending response of an Euler-Bernoulli pipe modeled using beam elements."
[../]

[./error_displacements1]
  type = 'RunException'
  input = 'euler_small_strain_y.i'
  cli_args = 'Materials/strain/rotations="rot_x" Outputs/exodus=false Outputs/csv=false'
  expect_err = "ComputeIncrementalBeamStrain: The number of variables supplied in 'displacements' and 'rotations' must match."

  requirement = "The ComputeIncrementalBeamStrain class shall produce an error if the number of supplied displacements and rotations do not match."
[../]

[./error_displacements2]
  type = 'RunException'
  input = 'euler_small_strain_y.i'
  cli_args = 'Kernels/solid_disp_x/rotations="rot_x" Outputs/exodus=false Outputs/csv=false'
  expect_err = "StressDivergenceBeam: The number of displacement and rotation variables should be same."

  requirement = "The StressDivergenceBeam class shall produce an error if the number of supplied displacements and rotations do not match."
[../]

[./error_large_strain]
  type = 'RunException'
  input = 'euler_small_strain_y.i'
  cli_args = 'Materials/strain/large_strain=true Materials/strain/Ay=1.0 Outputs/exodus=false Outputs/csv=false'
  expect_err = 'ComputeIncrementalBeamStrain: Large strain calculation does not currently support asymmetric beam configurations with non-zero first or third moments of area.'

  requirement = "The ComputeIncrementalBeamStrain class shall produce an error if large strain calculation is requested for asymmetric beam configurations with non-zero first or third moments of area."
[../]

[./error_y_orientation]
  type = 'RunException'
  input = 'euler_small_strain_y.i'
  cli_args = 'Materials/strain/y_orientation="0.5 0.5 0.0" Outputs/exodus=false Outputs/csv=false'
  expect_err = 'ComputeIncrementalBeamStrain: y_orientation should be perpendicular to the axis of the beam.'

  requirement = "The ComputeIncrementalBeamStrain class shall produce an error if the y orientation provided is not perpendicular to the beam axis."
[../]

[./torsion_1]
  type = 'Exodiff'
  input = 'torsion_1.i'
  exodiff = 'torsion_1_out.e'
  verification = 'beam_vandv.md'
  requirement = "The mechanics system shall accurately predict the torsional response of a beam modeled using beam elements with auto-calculated polar moment of inertia."
[../]

[./torison_2]
  type = 'Exodiff'
  input = 'torsion_2.i'
  exodiff = 'torsion_2_out.e'

  requirement = "The mechanics system shall accurately predict the torsional response of a beam modeled using beam elements with user provided polar moment of inertia."
[../]

[./orientation_yz]
  input = 'euler_small_strain_orientation_yz.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_yz_out.csv'
  detail = "oriented on the YZ plane at a 45 deg. angle."
[../]

[./orientation_yz_force_yz]
  input = 'euler_small_strain_orientation_yz_force_yz.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_yz_force_yz_out.csv'
  detail = "oriented on the YZ plane at a 45 deg. angle and has in-plane loading."
[../]

[./orientation_yz_force_yz_cross_section]
  input = 'euler_small_strain_orientation_yz_force_yz_cross_section.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_yz_force_yz_cross_section_out.csv'
  detail = "oriented on the YZ plane at a 45 deg. angle and has in-plane loading with non-symmetric cross section geometry."
[../]

[./orientation_yz_cross_section]
  input = 'euler_small_strain_orientation_yz_cross_section.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_yz_cross_section_out.csv'
  detail = "oriented on the YZ plane at a 45 deg. angle and has in-plane loading and the cross section geometry is non-symmetric."
[../]

[./orientation_xz]
  input = 'euler_small_strain_orientation_xz.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_xz_out.csv'
  detail = "oriented on the XZ plane at a 45 deg. angle."
[../]

[./orientation_xz_force_xz]
  input = 'euler_small_strain_orientation_xz_force_xz.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_xz_force_xz_out.csv'
  detail = "oriented on the XZ plane at a 45 deg. angle, and the external loading takes place on the same plane."
[../]

[./orientation_xy]
  input = 'euler_small_strain_orientation_xy.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_xy_out.csv'
  detail = "oriented on the XY plane at a 45 deg. angle."
[../]

[./orientation_xy_force_xy]
  input = 'euler_small_strain_orientation_xy_force_xy.i'
  type = 'CSVDiff'
  csvdiff = 'euler_small_strain_orientation_xy_force_xy_out.csv'
  detail = "oriented on the XY plane at a 45 deg. angle, and the external loading takes place on the same plane."
[../]

[./thermal_eigenstrain]
  type = 'Exodiff'
  input = 'thermal_expansion_small.i'
  exodiff = 'thermal_expansion_small_out.e'

  requirement = "The ComputeThermalExpansionEigenstrainBeam class shall correctly calculate eigenstrains due to changes in temperature."
  design = "ComputeThermalExpansionEigenstrainBeam.md"
  issues = "#10313"
[../]

[./eigenstrain_from_var]
  type = 'Exodiff'
  input = 'eigenstrain_from_var.i'
  exodiff = 'eigenstrain_from_var_out.e'

  requirement = "The ComputeEigenstrainBeamFromVariable class shall correctly transfer eigenstrains from auxvariables into eigenstrain material property."
  design = "ComputeEigenstrainBeamFromVariable.md"
  issues = "#10313"
[../]

[./eigenstrain_from_var_test1]
  type = 'RunException'
  input = 'eigenstrain_from_var.i'
  cli_args = "Materials/thermal/displacement_eigenstrain_variables='thermal_eig zero1' Outputs/csv=false Outputs/exodus=false"
  expect_err = "ComputeEigenstrainBeamFromVariable: If the displacement or rotational eigenstrains are provided, it should contain 3 variables corresponding to the three components in the global coordinate system."

  requirement = "The ComputeEigenstrainBeamFromVariable class shall report an error if less than 3 displacement or rotational eigenstrains are provided by the user."
  design = "ComputeEigenstrainBeamFromVariable.md"
  issues = "#10313"
[../]

[./except1]
  type = 'RunException'
  input = 'except1.i'
  expect_err = 'CappedWeakPlaneStressUpdate: Weak-plane friction and dilation angles must lie in \[0, Pi/2\]'
  requirement = "The CappedWeakPlaneStressUpdate model shall generate an error if the friction angle is negative"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./except2]
  type = 'RunException'
  input = 'except2.i'
  expect_err = 'CappedWeakPlaneStressUpdate: Weak-plane friction and dilation angles must lie in \[0, Pi/2\]'
  requirement = "The CappedWeakPlaneStressUpdate model shall generate an error if the dilation angle is negative"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./except3]
  type = 'RunException'
  input = 'except3.i'
  expect_err = 'CappedWeakPlaneStressUpdate: Weak-plane friction angle must not be less than dilation angle'
  requirement = "The CappedWeakPlaneStressUpdate model shall generate an error if the friction angle is less than the dilation angle"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./except4]
  type = 'RunException'
  input = 'except4.i'
  expect_err = 'CappedWeakPlaneStressUpdate: Weak-plane cohesion must not be negative'
  requirement = "The CappedWeakPlaneStressUpdate model shall generate an error if the cohesion is negative"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./except5]
  type = 'RunException'
  input = 'except5.i'
  expect_err = 'CappedWeakPlaneStressUpdate: Weak plane tensile strength plus compressive strength must be greater than smoothing_tol'
  requirement = "The CappedWeakPlaneStressUpdate model shall generate an error if the sum of the tensile and compressive strength is less than smoothing_tol"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./except6]
  type = 'RunException'
  input = 'except6.i'
  expect_err = 'CappedWeakInclinedPlaneStressUpdate: normal_vector must not have zero length'
  requirement = "The CappedWeakPlaneStressUpdate model shall generate an error if the normal vector has zero length"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small1]
  type = 'CSVDiff'
  input = 'small_deform1.i'
  csvdiff = 'small_deform1.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly compute stresses in the elastic regime"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small2]
  type = 'CSVDiff'
  input = 'small_deform2.i'
  csvdiff = 'small_deform2.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent tensile failure with the Lame coefficient lambda=0"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small3]
  type = 'CSVDiff'
  input = 'small_deform3.i'
  csvdiff = 'small_deform3.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent tensile failure with the Lame coefficient lambda=4"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small4]
  type = 'CSVDiff'
  input = 'small_deform4.i'
  csvdiff = 'small_deform4.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent compression failure"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small5]
  type = 'CSVDiff'
  input = 'small_deform5.i'
  csvdiff = 'small_deform5.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent shear failure"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small6]
  type = 'CSVDiff'
  input = 'small_deform6.i'
  csvdiff = 'small_deform6.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent both tensile and shear failure"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small7]
  type = 'CSVDiff'
  input = 'small_deform7.i'
  csvdiff = 'small_deform7.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent tensile behavior with hardening"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small8]
  type = 'CSVDiff'
  input = 'small_deform8.i'
  csvdiff = 'small_deform8.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent compression behavior with hardening"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small9]
  type = 'CSVDiff'
  input = 'small_deform9.i'
  csvdiff = 'small_deform9.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent shear behavior with hardening"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small10]
  type = 'CSVDiff'
  input = 'small_deform10.i'
  csvdiff = 'small_deform10.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent hardening under combined tension and shear"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./small11]
  type = 'CSVDiff'
  input = 'small_deform11.i'
  csvdiff = 'small_deform11.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent hardening under combined tension and shear with an initial stress"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./pull_push]
  type = Exodiff
  input = 'pull_push.i'
  exodiff = 'pull_push.e'
  abs_zero = 1E-2
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent the behavior of a column of elements that is pulled, then pushed"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./pull_push_h]
  type = Exodiff
  input = 'pull_push_h.i'
  exodiff = 'pull_push_h.e'
  abs_zero = 1E-2
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent the behavior of a column of elements that is pulled, then pushed, with tensile hardening"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7784"
[../]

[./cwp_beam]
  type = Exodiff
  input = 'beam.i'
  exodiff = 'beam.e'
  #heavy = true  # uncomment if this test takes too long on INL computers
  abs_zero = 1E-4
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent the behavior of a beam with its ends fully clamped"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7960"
[../]

[./pull_and_shear_1step]
  type = Exodiff
  input = 'pull_and_shear_1step.i'
  exodiff = 'pull_and_shear_1step.e'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent the tensile failure of a single layer of elements in 1 nonlinear step"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7960"
  custom_cmp = 'pull_and_shear_1step.cmp'
[../]

[./pull_and_shear]
  type = Exodiff
  input = 'pull_and_shear.i'
  exodiff = 'pull_and_shear.e'
  #heavy = true  # uncomment if this test takes too long on INL computers
  abs_zero = 1E-4
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent a dynamic problem with plasticity in which a column of material is pulled in tension"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7960"
[../]

[./push_and_shear]
  type = Exodiff
  input = 'push_and_shear.i'
  exodiff = 'push_and_shear.e'
  abs_zero = 1E-4
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent a dynamic problem with plasticity in which a column of material is pushed in compression"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7960"
[../]

[./throw_test]
  type = 'RunException'
  input = 'throw_test.i'
  expect_err = "Solve failed and timestep already at or below dtmin"
  recover = false
  requirement = "The system shall permit exceptions to be thrown from material models with stateful properties without reading/writing to/from uninitialized memory"
  design = "CappedWeakPlaneStressUpdate.md"
  issues = "#7960"
[../]

[./small_inclined2]
  type = 'CSVDiff'
  input = 'small_deform_inclined2.i'
  csvdiff = 'small_deform_inclined2.csv'
  requirement = "The CappedWeakInclinedPlaneStressUpdate model shall correctly represent tensile failure with a specified normal=(1,0,0)"
  design = "CappedWeakInclinedPlaneStressUpdate.md"
  issues = "#8303"
[../]

[./small_inclined3]
  type = 'CSVDiff'
  input = 'small_deform_inclined3.i'
  csvdiff = 'small_deform_inclined3.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent tensile failure with a specified normal=(0,1,0)"
  design = "CappedWeakInclinedPlaneStressUpdate.md"
  issues = "#8303"
[../]

[./small_inclined5]
  type = 'CSVDiff'
  input = 'small_deform_inclined5.i'
  csvdiff = 'small_deform_inclined5.csv'
  requirement = "The CappedWeakPlaneStressUpdate model shall correctly represent shear failure with a specified normal=(1,0,0)"
  design = "CappedWeakInclinedPlaneStressUpdate.md"
  issues = "#8303"
[../]

[./small_cosserat1]
  type = 'CSVDiff'
  input = 'small_deform_cosserat1.i'
  csvdiff = 'small_deform_cosserat1.csv'
  requirement = "The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a first set of loading conditions"
  design = "CappedWeakPlaneCosseratStressUpdate.md"
  issues = "#8431"
[../]

[./small_cosserat2]
  type = 'CSVDiff'
  input = 'small_deform_cosserat2.i'
  csvdiff = 'small_deform_cosserat2.csv'
  requirement = "The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a second set of loading conditions"
  design = "CappedWeakPlaneCosseratStressUpdate.md"
  issues = "#8431"
[../]

[./small_cosserat3]
  type = 'CSVDiff'
  input = 'small_deform_cosserat3.i'
  csvdiff = 'small_deform_cosserat3.csv'
  requirement = "The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a third set of loading conditions"
  design = "CappedWeakPlaneCosseratStressUpdate.md"
  issues = "#8431"
[../]

[./small_cosserat4]
  type = 'CSVDiff'
  input = 'small_deform_cosserat4.i'
  csvdiff = 'small_deform_cosserat4.csv'
  requirement = "The CappedWeakPlaneCosseratStressUpdate model shall correctly represent plastic behavior under a fourth set of loading conditions"
  design = "CappedWeakPlaneCosseratStressUpdate.md"
  issues = "#8431"
[../]

[./implicit]
  type = 'CSVDiff'
  input = '1d_consistent_implicit.i'
  csvdiff = '1d_consistent_implicit_out.csv'
  requirement = "The NewmarkBeta timeintegrator shall correctly calculate the response of a 1D mesh. "
[../]

[./explicit]
  type = 'CSVDiff'
  input = '1d_consistent_explicit.i'
  csvdiff = '1d_consistent_explicit_out.csv'
  requirement = "The CentralDifference timeintegrator shall correctly calculate the response of a 1D mesh when the the consistent mass matrix option is used."
[../]

[./implicit]
  type = 'CSVDiff'
  input = '2d_consistent_implicit.i'
  csvdiff = '2d_consistent_implicit_out.csv'
  requirement = "The NewmarkBeta timeintegrator shall correctly calculate the response of a 2D mesh. "
[../]

[./explicit]
  type = 'CSVDiff'
  input = '2d_consistent_explicit.i'
  csvdiff = '2d_consistent_explicit_out.csv'
  requirement = "The CentralDifference timeintegrator shall correctly calculate the response of a 2D mesh when the the consistent mass matrix option is used."
[../]

[implicit]
  type = 'CSVDiff'
  input = '3d_consistent_implicit.i'
  csvdiff = '3d_consistent_implicit_out.csv'
  requirement = "The NewmarkBeta timeintegrator shall correctly calculate the response of a 3D mesh. "
[]

[explicit]
  type = 'CSVDiff'
  input = '3d_consistent_explicit.i'
  csvdiff = '3d_consistent_explicit_out.csv'
  requirement = "The CentralDifference timeintegrator shall correctly calculate the response of a 3D mesh when the the consistent mass matrix option is used."
[]

[explicit_mass_scaling]
  type = 'Exodiff'
  input = '3d_consistent_explicit_mass_scaling.i'
  exodiff = '3d_consistent_explicit_mass_scaling_out.e'
  requirement = "The central difference time integrator time step can be increased by selecting density scaling."
[]

[explicit_nodalmass]
  type = 'CSVDiff'
  input = '1d_nodalmass_explicit.i'
  csvdiff = '1d_nodalmass_explicit_out.csv'
  requirement = "The system shall include central difference time integration that correctly calculates the response of a 1D mesh with nodal masses equal to those of a corresponding lumped mass system."
[]

[implicit_nodalmass]
  type = 'CSVDiff'
  input = '1d_nodalmass_implicit.i'
  csvdiff = '1d_nodalmass_implicit_out.csv'
  requirement = "The system shall include Newmark-beta time integration that correctly calculate the response of a 1D mesh with nodal masses equal to those of a corresponding lumped mass system."
[]

[explicit_lumped]
  type = 'CSVDiff'
  input = '1d_lumped_explicit.i'
  cli_args = Outputs/file_base=1d_nodalmass_explicit_out
  csvdiff = '1d_nodalmass_explicit_out.csv'
  prereq = explicit_nodalmass
  requirement = "The system shall include a central difference time integration that when used with the lumped mass shall correctly calculate the response of a 1D mesh and produce results that are identical to those calculated using equivalent nodal masses."
[]

[explicit_constant_mass]
  type = 'CSVDiff'
  input = '1d_lumped_explicit.i'
  cli_args = 'Outputs/file_base=1d_nodalmass_explicit_out Executioner/TimeIntegrator/use_constant_mass=true'
  csvdiff = '1d_nodalmass_explicit_out.csv'
  prereq = explicit_nodalmass
  requirement = "The system shall include central difference time integration that when used with the constant mass option shall correctly calculate the response of a 1D mesh and produce results that are identical to those calculated using equivalent nodal masses."
[]

[explicit_nodalmass]
  type = 'CSVDiff'
  input = '2d_nodalmass_explicit.i'
  csvdiff = '2d_nodalmass_explicit_out.csv'
  requirement = "The system shall include central difference time integration that correctly calculates the response of a 2D mesh with nodal masses equal to those of a corresponding lumped mass system."
[]

[implicit_nodalmass]
  type = 'CSVDiff'
  input = '2d_nodalmass_implicit.i'
  csvdiff = '2d_nodalmass_implicit_out.csv'
  requirement = "The system shall include Newmark-beta time integration that correctly calculates the response of a 2D mesh with nodal masses equal to those of a corresponding lumped mass system."
[]

[explicit_lumped]
  type = 'CSVDiff'
  input = '2d_lumped_explicit.i'
  cli_args = Outputs/file_base=2d_nodalmass_explicit_out
  csvdiff = '2d_nodalmass_explicit_out.csv'
  prereq = explicit_nodalmass
  requirement = "The system syall include central difference time integration that when used with the lumped mass option shall correctly calculate the response of a 2D mesh and produce results that are identical to those calculated using equivalent nodal masses."
[]

[explicit_constant_mass]
  type = 'CSVDiff'
  input = '2d_lumped_explicit.i'
  cli_args = 'Outputs/file_base=2d_nodalmass_explicit_out Executioner/TimeIntegrator/use_constant_mass=true'
  csvdiff = '2d_nodalmass_explicit_out.csv'
  prereq = explicit_nodalmass
  requirement = "The system syall include central difference time integration that when used with the constant mass option shall correctly calculate the response of a 2D mesh and produce results that are identical to those calculated using equivalent nodal masses."
[]

[explicit_nodalmass]
  type = 'CSVDiff'
  input = '3d_nodalmass_explicit.i'
  csvdiff = '3d_nodalmass_explicit_out.csv'
  requirement = "The system shall include central difference time integration that correctly calculates the response of a 3D mesh with nodal masses equal to those of a corresponding lumped mass system."
[]

[implicit_nodalmass]
  type = 'CSVDiff'
  input = '3d_nodalmass_implicit.i'
  csvdiff = '3d_nodalmass_implicit_out.csv'
  requirement = "The system shall include Newmar-beta time integration that correctly calculates the response of a 3D mesh with nodal masses equal to those of a corresponding lumped mass system."
[]

[explicit_lumped]
  type = 'CSVDiff'
  input = '3d_lumped_explicit.i'
  cli_args = Outputs/file_base=3d_nodalmass_explicit_out
  csvdiff = '3d_nodalmass_explicit_out.csv'
  prereq = explicit_nodalmass
  requirement = "The system shall include central difference time integration that when used with the lumped mass option shall correctly calculate the response of a 3D mesh and produce results that are identical to those calculated using equivalent nodal masses."
[]

[explicit_constant_mass]
  type = 'CSVDiff'
  input = '3d_lumped_explicit.i'
  cli_args = 'Outputs/file_base=3d_nodalmass_explicit_out Executioner/TimeIntegrator/use_constant_mass=true'
  csvdiff = '3d_nodalmass_explicit_out.csv'
  prereq = explicit_nodalmass
  requirement = "The system shall include central difference time integration that when used with the constant mass option shall correctly calculate the response of a 3D mesh and produce results that are identical to those calculated using equivalent nodal masses."
[]

[jacobian_small_strain]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_small_strain_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_small_strain_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[jacobian_total_lagrangian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_total_lagrangian_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_jacobian_total_lagrangian_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[small_strain_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_small_strain_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_small_strain_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[total_lagrangian_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_total_lagrangian_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_total_lagrangian_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[multiple_action_and_materials]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = 'czm_multiple_action_and_materials_out.e'
  detail = "The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries"
  cli_args = "Physics/SolidMechanics/CohesiveZone/strain=FINITE"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_different_strain]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'All blocks of the CohesiveZoneAction should have the same strain formulation'
  detail = "The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik_23/strain=SMALL"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_overlapping_boundary]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'The boundary restrictions in the CohesiveZoneAction actions must be non-overlapping.'
  detail = "The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/boundary='Block0_Block1' Physics/SolidMechanics/CohesiveZone/czm_ik_23/boundary='Block0_Block1'"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_common_outputs]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_common_output_out.e
  detail = "The system shall use the common block generate output and additional outputs for all CZM blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/additional_generate_output='normal_traction tangent_traction normal_jump tangent_jump'  Physics/SolidMechanics/CohesiveZone/material_output_order=FIRST Outputs/file_base=czm_multiple_action_common_output_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_additional_outputs_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_additional_outputs_on_different_block_out.e
  detail = "The system shall add additional outputs requested within each block"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/czm_ik_012/additional_generate_output='normal_traction tangent_traction' Physics/SolidMechanics/CohesiveZone/czm_ik_23/additional_generate_output='normal_jump tangent_jump' Outputs/file_base=czm_multiple_action_additional_outputs_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_differnt_outputs_orders_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_differnt_outputs_orders_on_different_block_out.e
  detail = "The system shall be able to use different output orders on different blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/material_output_order=CONSTANT Physics/SolidMechanics/CohesiveZone/czm_ik_23/material_output_order=FIRST Outputs/file_base=czm_multiple_action_differnt_outputs_orders_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[action_3D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_small_strain_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_small_strain_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[action_3D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_total_lagrangian_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3 Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'  Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_total_lagrangian_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[czm_incremental_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_incremental_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental  Outputs/file_base=czm_incremental_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material."
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_total_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_total_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Outputs/file_base=czm_total_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material."
  mesh_mode = 'REPLICATED'
  recover = false
[]

[jacobian_small_strain]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_small_strain_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_small_strain_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[jacobian_total_lagrangian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_total_lagrangian_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_jacobian_total_lagrangian_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[small_strain_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_small_strain_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_small_strain_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[total_lagrangian_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_total_lagrangian_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_total_lagrangian_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[multiple_action_and_materials]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = 'czm_multiple_action_and_materials_out.e'
  detail = "The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries"
  cli_args = "Physics/SolidMechanics/CohesiveZone/strain=FINITE"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_different_strain]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'All blocks of the CohesiveZoneAction should have the same strain formulation'
  detail = "The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik_23/strain=SMALL"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_overlapping_boundary]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'The boundary restrictions in the CohesiveZoneAction actions must be non-overlapping.'
  detail = "The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/boundary='Block0_Block1' Physics/SolidMechanics/CohesiveZone/czm_ik_23/boundary='Block0_Block1'"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_common_outputs]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_common_output_out.e
  detail = "The system shall use the common block generate output and additional outputs for all CZM blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/additional_generate_output='normal_traction tangent_traction normal_jump tangent_jump'  Physics/SolidMechanics/CohesiveZone/material_output_order=FIRST Outputs/file_base=czm_multiple_action_common_output_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_additional_outputs_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_additional_outputs_on_different_block_out.e
  detail = "The system shall add additional outputs requested within each block"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/czm_ik_012/additional_generate_output='normal_traction tangent_traction' Physics/SolidMechanics/CohesiveZone/czm_ik_23/additional_generate_output='normal_jump tangent_jump' Outputs/file_base=czm_multiple_action_additional_outputs_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_differnt_outputs_orders_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_differnt_outputs_orders_on_different_block_out.e
  detail = "The system shall be able to use different output orders on different blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/material_output_order=CONSTANT Physics/SolidMechanics/CohesiveZone/czm_ik_23/material_output_order=FIRST Outputs/file_base=czm_multiple_action_differnt_outputs_orders_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[action_3D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_small_strain_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_small_strain_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[action_3D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_total_lagrangian_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3 Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'  Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_total_lagrangian_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[czm_incremental_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_incremental_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental  Outputs/file_base=czm_incremental_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material."
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_total_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_total_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Outputs/file_base=czm_total_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material."
  mesh_mode = 'REPLICATED'
  recover = false
[]

[jacobian_small_strain]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_small_strain_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_small_strain_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[jacobian_total_lagrangian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_total_lagrangian_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_jacobian_total_lagrangian_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[small_strain_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_small_strain_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_small_strain_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[total_lagrangian_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_total_lagrangian_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_total_lagrangian_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[multiple_action_and_materials]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = 'czm_multiple_action_and_materials_out.e'
  detail = "The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries"
  cli_args = "Physics/SolidMechanics/CohesiveZone/strain=FINITE"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_different_strain]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'All blocks of the CohesiveZoneAction should have the same strain formulation'
  detail = "The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik_23/strain=SMALL"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_overlapping_boundary]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'The boundary restrictions in the CohesiveZoneAction actions must be non-overlapping.'
  detail = "The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/boundary='Block0_Block1' Physics/SolidMechanics/CohesiveZone/czm_ik_23/boundary='Block0_Block1'"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_common_outputs]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_common_output_out.e
  detail = "The system shall use the common block generate output and additional outputs for all CZM blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/additional_generate_output='normal_traction tangent_traction normal_jump tangent_jump'  Physics/SolidMechanics/CohesiveZone/material_output_order=FIRST Outputs/file_base=czm_multiple_action_common_output_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_additional_outputs_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_additional_outputs_on_different_block_out.e
  detail = "The system shall add additional outputs requested within each block"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/czm_ik_012/additional_generate_output='normal_traction tangent_traction' Physics/SolidMechanics/CohesiveZone/czm_ik_23/additional_generate_output='normal_jump tangent_jump' Outputs/file_base=czm_multiple_action_additional_outputs_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_differnt_outputs_orders_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_differnt_outputs_orders_on_different_block_out.e
  detail = "The system shall be able to use different output orders on different blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/material_output_order=CONSTANT Physics/SolidMechanics/CohesiveZone/czm_ik_23/material_output_order=FIRST Outputs/file_base=czm_multiple_action_differnt_outputs_orders_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[action_3D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_small_strain_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_small_strain_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[action_3D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_total_lagrangian_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3 Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'  Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_total_lagrangian_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[czm_incremental_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_incremental_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental  Outputs/file_base=czm_incremental_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material."
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_total_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_total_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Outputs/file_base=czm_total_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material."
  mesh_mode = 'REPLICATED'
  recover = false
[]

[jacobian_small_strain]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_small_strain_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_small_strain_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[jacobian_total_lagrangian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_total_lagrangian_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_jacobian_total_lagrangian_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[small_strain_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_small_strain_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_small_strain_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[total_lagrangian_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_total_lagrangian_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_total_lagrangian_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[multiple_action_and_materials]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = 'czm_multiple_action_and_materials_out.e'
  detail = "The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries"
  cli_args = "Physics/SolidMechanics/CohesiveZone/strain=FINITE"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_different_strain]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'All blocks of the CohesiveZoneAction should have the same strain formulation'
  detail = "The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik_23/strain=SMALL"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_overlapping_boundary]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'The boundary restrictions in the CohesiveZoneAction actions must be non-overlapping.'
  detail = "The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/boundary='Block0_Block1' Physics/SolidMechanics/CohesiveZone/czm_ik_23/boundary='Block0_Block1'"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_common_outputs]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_common_output_out.e
  detail = "The system shall use the common block generate output and additional outputs for all CZM blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/additional_generate_output='normal_traction tangent_traction normal_jump tangent_jump'  Physics/SolidMechanics/CohesiveZone/material_output_order=FIRST Outputs/file_base=czm_multiple_action_common_output_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_additional_outputs_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_additional_outputs_on_different_block_out.e
  detail = "The system shall add additional outputs requested within each block"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/czm_ik_012/additional_generate_output='normal_traction tangent_traction' Physics/SolidMechanics/CohesiveZone/czm_ik_23/additional_generate_output='normal_jump tangent_jump' Outputs/file_base=czm_multiple_action_additional_outputs_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_differnt_outputs_orders_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_differnt_outputs_orders_on_different_block_out.e
  detail = "The system shall be able to use different output orders on different blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/material_output_order=CONSTANT Physics/SolidMechanics/CohesiveZone/czm_ik_23/material_output_order=FIRST Outputs/file_base=czm_multiple_action_differnt_outputs_orders_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[action_3D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_small_strain_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_small_strain_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[action_3D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_total_lagrangian_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3 Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'  Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_total_lagrangian_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[czm_incremental_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_incremental_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental  Outputs/file_base=czm_incremental_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material."
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_total_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_total_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Outputs/file_base=czm_total_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material."
  mesh_mode = 'REPLICATED'
  recover = false
[]

[jacobian_small_strain]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_small_strain_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_small_strain_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[jacobian_total_lagrangian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_total_lagrangian_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_jacobian_total_lagrangian_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[small_strain_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_small_strain_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_small_strain_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[total_lagrangian_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_total_lagrangian_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_total_lagrangian_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[multiple_action_and_materials]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = 'czm_multiple_action_and_materials_out.e'
  detail = "The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries"
  cli_args = "Physics/SolidMechanics/CohesiveZone/strain=FINITE"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_different_strain]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'All blocks of the CohesiveZoneAction should have the same strain formulation'
  detail = "The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik_23/strain=SMALL"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_overlapping_boundary]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'The boundary restrictions in the CohesiveZoneAction actions must be non-overlapping.'
  detail = "The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/boundary='Block0_Block1' Physics/SolidMechanics/CohesiveZone/czm_ik_23/boundary='Block0_Block1'"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_common_outputs]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_common_output_out.e
  detail = "The system shall use the common block generate output and additional outputs for all CZM blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/additional_generate_output='normal_traction tangent_traction normal_jump tangent_jump'  Physics/SolidMechanics/CohesiveZone/material_output_order=FIRST Outputs/file_base=czm_multiple_action_common_output_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_additional_outputs_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_additional_outputs_on_different_block_out.e
  detail = "The system shall add additional outputs requested within each block"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/czm_ik_012/additional_generate_output='normal_traction tangent_traction' Physics/SolidMechanics/CohesiveZone/czm_ik_23/additional_generate_output='normal_jump tangent_jump' Outputs/file_base=czm_multiple_action_additional_outputs_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_differnt_outputs_orders_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_differnt_outputs_orders_on_different_block_out.e
  detail = "The system shall be able to use different output orders on different blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/material_output_order=CONSTANT Physics/SolidMechanics/CohesiveZone/czm_ik_23/material_output_order=FIRST Outputs/file_base=czm_multiple_action_differnt_outputs_orders_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[action_3D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_small_strain_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_small_strain_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[action_3D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_total_lagrangian_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3 Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'  Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_total_lagrangian_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[czm_incremental_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_incremental_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental  Outputs/file_base=czm_incremental_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material."
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_total_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_total_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Outputs/file_base=czm_total_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material."
  mesh_mode = 'REPLICATED'
  recover = false
[]

[jacobian_small_strain]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_small_strain_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_small_strain_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[jacobian_total_lagrangian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_total_lagrangian_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_jacobian_total_lagrangian_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[small_strain_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_small_strain_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_small_strain_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[total_lagrangian_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_total_lagrangian_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_total_lagrangian_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[multiple_action_and_materials]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = 'czm_multiple_action_and_materials_out.e'
  detail = "The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries"
  cli_args = "Physics/SolidMechanics/CohesiveZone/strain=FINITE"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_different_strain]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'All blocks of the CohesiveZoneAction should have the same strain formulation'
  detail = "The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik_23/strain=SMALL"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_overlapping_boundary]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'The boundary restrictions in the CohesiveZoneAction actions must be non-overlapping.'
  detail = "The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/boundary='Block0_Block1' Physics/SolidMechanics/CohesiveZone/czm_ik_23/boundary='Block0_Block1'"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_common_outputs]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_common_output_out.e
  detail = "The system shall use the common block generate output and additional outputs for all CZM blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/additional_generate_output='normal_traction tangent_traction normal_jump tangent_jump'  Physics/SolidMechanics/CohesiveZone/material_output_order=FIRST Outputs/file_base=czm_multiple_action_common_output_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_additional_outputs_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_additional_outputs_on_different_block_out.e
  detail = "The system shall add additional outputs requested within each block"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/czm_ik_012/additional_generate_output='normal_traction tangent_traction' Physics/SolidMechanics/CohesiveZone/czm_ik_23/additional_generate_output='normal_jump tangent_jump' Outputs/file_base=czm_multiple_action_additional_outputs_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_differnt_outputs_orders_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_differnt_outputs_orders_on_different_block_out.e
  detail = "The system shall be able to use different output orders on different blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/material_output_order=CONSTANT Physics/SolidMechanics/CohesiveZone/czm_ik_23/material_output_order=FIRST Outputs/file_base=czm_multiple_action_differnt_outputs_orders_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[action_3D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_small_strain_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_small_strain_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[action_3D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_total_lagrangian_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3 Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'  Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_total_lagrangian_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[czm_incremental_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_incremental_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental  Outputs/file_base=czm_incremental_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material."
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_total_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_total_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Outputs/file_base=czm_total_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material."
  mesh_mode = 'REPLICATED'
  recover = false
[]

[jacobian_small_strain]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_small_strain_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_small_strain_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[jacobian_total_lagrangian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_total_lagrangian_out.csv'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparation Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_jacobian_total_lagrangian_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall converge quadratically when using the hand-coded Jacobian"
[]

[small_strain_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_small_strain_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2   Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_small_strain_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The small strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[total_lagrangian_incremental]
  type = Exodiff
  input = 'czm_patch_test_base.i'
  exodiff = czm_total_lagrangian_incremental_out.e
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental Materials/czm_mat/normal_stiffness=100e2 Materials/czm_mat/tangent_stiffness=70e2 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Outputs/file_base=czm_total_lagrangian_incremental_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The finite strain cohesive zone model shall return the same results of the total formulation when using an incremental material"
  allow_test_objects = true
[]

[multiple_action_and_materials]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = 'czm_multiple_action_and_materials_out.e'
  detail = "The system shall allow using multiple CohesiveZoneAction and different cohesive materials for different boundaries"
  cli_args = "Physics/SolidMechanics/CohesiveZone/strain=FINITE"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_different_strain]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'All blocks of the CohesiveZoneAction should have the same strain formulation'
  detail = "The system shall report an error when different strains are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/strain=FINITE Physics/SolidMechanics/CohesiveZone/czm_ik_23/strain=SMALL"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_overlapping_boundary]
  type = RunException
  input = 'czm_multiple_action_and_materials.i'
  expect_err = 'The boundary restrictions in the CohesiveZoneAction actions must be non-overlapping.'
  detail = "The system shall report an error when overlapping boundaries are provided in different blocks of the CohesiveZoneAction"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/boundary='Block0_Block1' Physics/SolidMechanics/CohesiveZone/czm_ik_23/boundary='Block0_Block1'"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_common_outputs]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_common_output_out.e
  detail = "The system shall use the common block generate output and additional outputs for all CZM blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/additional_generate_output='normal_traction tangent_traction normal_jump tangent_jump'  Physics/SolidMechanics/CohesiveZone/material_output_order=FIRST Outputs/file_base=czm_multiple_action_common_output_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_multiple_action_additional_outputs_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_additional_outputs_on_different_block_out.e
  detail = "The system shall add additional outputs requested within each block"
  cli_args = "Physics/SolidMechanics/CohesiveZone/generate_output='traction_x traction_y traction_z jump_x jump_y jump_z' Physics/SolidMechanics/CohesiveZone/czm_ik_012/additional_generate_output='normal_traction tangent_traction' Physics/SolidMechanics/CohesiveZone/czm_ik_23/additional_generate_output='normal_jump tangent_jump' Outputs/file_base=czm_multiple_action_additional_outputs_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[multiple_action_differnt_outputs_orders_on_different_block]
  type = Exodiff
  input = 'czm_multiple_action_and_materials.i'
  exodiff = czm_multiple_action_differnt_outputs_orders_on_different_block_out.e
  detail = "The system shall be able to use different output orders on different blocks"
  cli_args = "Physics/SolidMechanics/CohesiveZone/czm_ik_012/material_output_order=CONSTANT Physics/SolidMechanics/CohesiveZone/czm_ik_23/material_output_order=FIRST Outputs/file_base=czm_multiple_action_differnt_outputs_orders_on_different_block_out"
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[action_3D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_small_strain_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using the PureElasticTractionSeparation model, and only compute a normal gap under purely normal loading.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_small_strain_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_small_strain_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_small_strain_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_small_strain_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x'"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the small strain formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[action_3D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_3D_total_lagrangian_normal_out.e
  cli_args = 'BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=czm_action_3D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/nz=2 Mesh/msh/dim=3 Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE'
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 3D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_2D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_2D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/inactive='left_z right_z' Outputs/out/file_base=czm_action_2D_total_lagrangian_normal_out Mesh/msh/nx=2 Mesh/msh/ny=2 Mesh/msh/dim=2 Mesh/subdomain_1/top_right='0.5 1 0' Mesh/subdomain_2/top_right='1 1 0' GlobalParams/displacements='disp_x disp_y' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x disp_y' Materials/czm_mat/displacements='disp_x disp_y'  Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 2D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
  abs_zero = 1e-6
[]

[action_1D_total_lagrangian_normal]
  type = Exodiff
  input = czm_multiple_dimension_base.i
  exodiff = czm_action_1D_total_lagrangian_normal_out.e
  cli_args = "BCs/right_x/function=1*t BCs/inactive='left_y right_y left_z right_z' Outputs/out/file_base=czm_action_1D_total_lagrangian_normal_out Mesh/msh/nx=2  Mesh/msh/dim=1 Mesh/subdomain_1/top_right='0.5 0 0' Mesh/subdomain_2/top_right='1 0 0' GlobalParams/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/generate_output='traction_x normal_traction tangent_traction jump_x normal_jump tangent_jump' Materials/czm_mat/displacements='disp_x' Physics/SolidMechanics/CohesiveZone/czm1/strain=FINITE"
  detail = 'The system shall allow for cohesive zone laws to represent the traction-separation behavior at an interface between two bodies represented by continuum elements in 1D using an elastic traction sepration law, and only compute a normal gap under purely normal loading when using the total Lagrangian formulation.'
  mesh_mode = 'REPLICATED'
  recover = false
[]

[czm_incremental_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_incremental_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Materials/czm_mat/type=PureElasticTractionSeparationIncremental  Outputs/file_base=czm_incremental_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using an incremental material."
  mesh_mode = 'REPLICATED'
  recover = false
  allow_test_objects = true
[]

[czm_total_stretch_rotate_total_lagrangian]
  type = Exodiff
  input = 'stretch_rotate_large_deformation.i'
  exodiff = 'czm_total_stretch_rotate_total_lagrangian_out.e'
  cli_args = "Outputs/file_base=czm_total_stretch_rotate_total_lagrangian_out"
  detail = "The CZMInterfaceKernelTotalLagrangian should properly account for large area changes and interface rotations when using a total strain material."
  mesh_mode = 'REPLICATED'
  recover = false
[]

[normal]
  type = Exodiff
  input = 'bilinear_mixed.i'
  exodiff = bilinear_mixed_normal_out.e
  cli_args = "Outputs/file_base=bilinear_mixed_normal_out"
  abs_zero = 1e-6
  rel_err = 1e-5
  detail = "under mode I loading."
[]

[scale_strength_normal]
  type = Exodiff
  input = 'bilinear_mixed_scale_strength.i'
  exodiff = bilinear_mixed_scale_strength_out.e
  abs_zero = 1e-6
  rel_err = 1e-5
  detail = "under mode I loading with scaled normal strength."
[]

[shear]
  type = Exodiff
  input = 'bilinear_mixed.i'
  exodiff = bilinear_mixed_shear_out.e
  cli_args = "Outputs/file_base=bilinear_mixed_shear_out BCs/fix_top/variable=disp_y BCs/top/variable=disp_x"
  abs_zero = 1e-6
  rel_err = 1e-5
  detail = "under mode II loading."
[]

[normal_lag]
  type = Exodiff
  input = 'bilinear_mixed.i'
  exodiff = bilinear_mixed_lag_out.e
  cli_args = "Materials/czm/lag_displacement_jump=true Outputs/file_base=bilinear_mixed_lag_out"
  abs_zero = 1e-5
  rel_err = 1e-5
  detail = "under mode I loading by lagging the seperation state."
[]

[normal_power_law]
  type = Exodiff
  input = 'bilinear_mixed.i'
  exodiff = bilinear_mixed_normal_power_law_out.e
  cli_args = "Materials/czm/mixed_mode_criterion=POWER_LAW Outputs/file_base=bilinear_mixed_normal_power_law_out"
  abs_zero = 1e-6
  rel_err = 1e-5
  detail = "under mode I loading with power law propagation criterion."
[]

[jacobian]
  type = CSVDiff
  input = 'czm_patch_test_base.i'
  csvdiff = 'czm_jacobian_3DC_out.csv'
  cli_args = "Materials/czm_mat/type=SalehaniIrani3DCTraction Materials/czm_mat/normal_gap_at_maximum_normal_traction=0.05 Materials/czm_mat/tangential_gap_at_maximum_shear_traction=0.01 Materials/czm_mat/maximum_normal_traction=100 Materials/czm_mat/maximum_shear_traction=70 Physics/SolidMechanics/CohesiveZone/czm_ik/strain=SMALL Physics/SolidMechanics/CohesiveZone/czm_ik/generate_output='traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL  Physics/SolidMechanics/QuasiStatic/all/use_finite_deform_jacobian=false Materials/stress/type=ADComputeLinearElasticStress Outputs/file_base=czm_jacobian_3DC_out Outputs/exodus=true"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The system shall converge quadratically when using the handcoded Jacobian of the 3DC traction separation model"
[]

[normal_load]
  type = Exodiff
  input = 'czm_traction_separation_base.i'
  exodiff = '3DC_normal_load_out.e'
  cli_args = "Materials/czm_mat/type=SalehaniIrani3DCTraction Materials/czm_mat/normal_gap_at_maximum_normal_traction=1 Materials/czm_mat/tangential_gap_at_maximum_shear_traction=1 Materials/czm_mat/maximum_normal_traction=10 Materials/czm_mat/maximum_shear_traction=7 Outputs/file_base=czm_jacobian_3DC_out BCs/right_x/function=1*t BCs/right_y/function=0*t BCs/right_z/function=0*t Outputs/out/file_base=3DC_normal_load_out"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The 3DC traction separation shall produce only a normal traction when a normal displacement jump is applied."
  abs_zero = 1e-6
[]

[shear_load_y]
  type = Exodiff
  input = 'czm_traction_separation_base.i'
  exodiff = '3DC_shear_load_y_out.e'
  cli_args = "Materials/czm_mat/type=SalehaniIrani3DCTraction Materials/czm_mat/normal_gap_at_maximum_normal_traction=1 Materials/czm_mat/tangential_gap_at_maximum_shear_traction=1 Materials/czm_mat/maximum_normal_traction=10 Materials/czm_mat/maximum_shear_traction=7 Outputs/file_base=czm_jacobian_3DC_out BCs/right_x/function=0*t BCs/right_y/function=1*t BCs/right_z/function=0*t Outputs/out/file_base=czm_3DC_load_shear_y_out Executioner/dt=0.25  Outputs/out/file_base=3DC_shear_load_y_out"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The 3DC traction separation shall produce only a shear traction y when a only a displacement jump along y is applied."
  abs_zero = 1e-6
[]

[shear_load_z]
  type = Exodiff
  input = 'czm_traction_separation_base.i'
  exodiff = '3DC_shear_load_z_out.e'
  cli_args = "Materials/czm_mat/type=SalehaniIrani3DCTraction Materials/czm_mat/normal_gap_at_maximum_normal_traction=1 Materials/czm_mat/tangential_gap_at_maximum_shear_traction=1 Materials/czm_mat/maximum_normal_traction=10 Materials/czm_mat/maximum_shear_traction=7 Outputs/file_base=czm_jacobian_3DC_out BCs/right_x/function=0*t BCs/right_y/function=0*t BCs/right_z/function=1*t Outputs/out/file_base=czm_3DC_load_shear_z_out Executioner/dt=0.25 Executioner/dt=0.25  Outputs/out/file_base=3DC_shear_load_z_out"
  mesh_mode = 'REPLICATED'
  recover = false
  detail = "The 3DC traction separation shall produce only a shear traction z when a only a displacement jump along z is applied."
  abs_zero = 1e-6
[]

[AD_solution]
  type = Exodiff
  input = 'ad_czm.i'
  cli_args = 'Outputs/file_base=ad_czm_small_strain'
  exodiff = 'ad_czm_small_strain.e'
  mesh_mode = REPLICATED
  recover = false
  detail = "The solution obtained using AD CZM shall match"
  abs_zero = 1e-6
[]

[non_AD_solution]
  type = Exodiff
  input = 'ad_czm.i'
  cli_args = 'Outputs/file_base=ad_czm_small_strain Physics/SolidMechanics/CohesiveZone/interface/use_automatic_differentiation=false Materials/czm_mat/type=PureElasticTractionSeparation'
  exodiff = 'ad_czm_small_strain.e'
  mesh_mode = REPLICATED
  recover = false
  detail = "the non-AD solution"
  abs_zero = 1e-6
[]

[AD_solution]
  type = Exodiff
  input = 'ad_czm.i'
  cli_args = 'Outputs/file_base=ad_czm_total_lagrangian Physics/SolidMechanics/CohesiveZone/interface/strain=FINITE'
  exodiff = 'ad_czm_total_lagrangian.e'
  mesh_mode = REPLICATED
  recover = false
  detail = "The solution obtained using AD CZM shall match"
  abs_zero = 1e-6
[]

[non_AD_solution]
  type = Exodiff
  input = 'ad_czm.i'
  cli_args = 'Outputs/file_base=ad_czm_total_lagrangian Physics/SolidMechanics/CohesiveZone/interface/strain=FINITE Physics/SolidMechanics/CohesiveZone/interface/use_automatic_differentiation=false Materials/czm_mat/type=PureElasticTractionSeparation'
  exodiff = 'ad_czm_total_lagrangian.e'
  mesh_mode = REPLICATED
  recover = false
  detail = "the non-AD solution"
  abs_zero = 1e-6
[]

[combined]
  type = 'Exodiff'
  input = 'combined_creep_plasticity.i'
  exodiff = 'combined_creep_plasticity_out.e'
  abs_zero = 1e-09
  method = 'OPT OPROF' # Test is too big for debug, but kept as is to match the published journal soln
  valgrind = HEAVY
  requirement = "MOOSE tensor mechanics module shall solve a combined creep
                   and plasticity 1-d bar problem."
[]

[combined_start_time]
  type = 'Exodiff'
  input = 'combined_creep_plasticity_start_time.i'
  exodiff = 'combined_creep_plasticity_start_time_out.e'
  abs_zero = 1e-09
  method = 'OPT OPROF' # Test is too big for debug, but kept as is to match the published journal soln
  custom_cmp = start_time.cmp
  valgrind = HEAVY
  requirement = "MOOSE tensor mechanics module shall solve a combined creep
                   and plasticity 1-d bar problem with a non-zero start time."
[]

[stress_prescribed]
  type = 'Exodiff'
  input = 'combined_stress_prescribed.i'
  exodiff = 'combined_stress_prescribed_out.e'
  rel_err = 1e-5
  abs_zero = 1e-09
  superlu = true
  requirement = "MOOSE tensor mechanics module shall solve a combined creep
                   and plasticity 3D cube problem with a time-varying pressure
                   BC."
[]

[stress_relaxation]
  type = 'Exodiff'
  input = 'combined_stress_relaxation.i'
  exodiff = 'combined_stress_relaxation_out.e'
  abs_zero = 1e-09
  requirement = "MOOSE tensor mechanics module shall solve a combined creep
                   and plasticity 3D cube problem with a constant displacement
                   BC and stress relaxation."
[]

[creepWithPlasticity]
  type = 'Exodiff'
  input = 'creepWithPlasticity.i'
  exodiff = 'creepWithPlasticity_out.e'
  abs_zero = 1e-09
  method = 'OPT OPROF' # Test is too big for debug, but kept as is to match the published journal soln
  valgrind = HEAVY
  requirement = "MOOSE tensor mechanics module shall solve a combined creep
                   and plasticity 1-d bar problem with the creep and plasticity models tightly coupled."
[]

[isotropic_plasticity_incremental]
  type = Exodiff
  input = 'isotropic_plasticity_incremental_strain.i'
  exodiff = 'isotropic_plasticity_incremental_strain_out.e'
  compiler = 'CLANG GCC'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation.'
[]

[isotropic_plasticity_incremental_base_name]
  type = Exodiff
  input = 'isotropic_plasticity_incremental_strain.i'
  cli_args = "Materials/isotropic_plasticity/base_name=base
                Physics/SolidMechanics/QuasiStatic/all/generate_output=''"
  exodiff = 'isotropic_plasticity_incremental_strain_out.e'
  exodiff_opts = '-allow_name_mismatch'
  compiler = 'CLANG GCC'
  prereq = isotropic_plasticity_incremental
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation while prescribing a base name for the isotropic plasticity material properties.'
[]

[isotropic_plasticity_incremental_Bbar]
  type = Exodiff
  input = 'isotropic_plasticity_incremental_strain.i'
  exodiff = 'isotropic_plasticity_incremental_strain_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'isotropic_plasticity_incremental_base_name'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation and using the b-bar element volume correction.'
[]

[isotropic_plasticity_finite]
  type = Exodiff
  input = 'isotropic_plasticity_finite_strain.i'
  exodiff = 'isotropic_plasticity_finite_strain_out.e'
  compiler = 'CLANG GCC'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation.'
[]

[isotropic_plasticity_finite_Bbar]
  type = Exodiff
  input = 'isotropic_plasticity_finite_strain.i'
  exodiff = 'isotropic_plasticity_finite_strain_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'isotropic_plasticity_finite'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation and using the b-bar element volume correction.'
[]

[affine_plasticity]
  type = Exodiff
  input = 'affine_plasticity.i'
  exodiff = 'affine_plasticity_out.e'
  custom_cmp = 'affine_plasticity.exodiff'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213.'
[]

[scalar_damage_material]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  csvdiff = 'scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material."
[]

[ad_scalar_damage_material]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  csvdiff = 'ad_scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation."
[]

[scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=scalar_material_damage_old_out'
  csvdiff = 'scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index."
[]

[ad_scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=ad_scalar_material_damage_old_out'
  csvdiff = 'ad_scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index when using automatic differentiation."
[]

[scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1."
[]

[ad_scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1 also when using automatic differentiation."
[]

[scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress"
[]

[ad_scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation"
[]

[combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  csvdiff = 'combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models."
[]

[combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=combined_scalar_damage_mult_out'
  csvdiff = 'combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models."
[]

[combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_sub_out'
  csvdiff = 'combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model"
[]

[combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_combined_out'
  csvdiff = 'combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models."
[]

[ad_combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  csvdiff = 'ad_combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=ad_combined_scalar_damage_mult_out'
  csvdiff = 'ad_combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_sub_out'
  csvdiff = 'ad_combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_combined_out'
  csvdiff = 'ad_combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation."
[]

[scalar_damage_material_inelastic]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep.i'
  csvdiff = 'scalar_material_damage_creep_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation."
[]

[scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep_power.i'
  csvdiff = 'scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation."
[]

[ad_scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage_creep_power.i'
  csvdiff = 'ad_scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation."
[]

[multiple_inelastic_bad_damage_model]
  type = RunException
  input = ad_scalar_material_damage_creep_power.i
  expect_err = "Damage Model.*damage_index.*is not compatible with ADComputeMultipleInelasticStress"
  requirement = "The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object."
  issues = '#20722'
  cli_args = 'Materials/stress/damage_model=damage_index'
  allow_warnings = True
[]

[nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'nonlocal_scalar_damage.i'
  csvdiff = 'nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model."
  issues = '#21786'
[]

[ad_nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'ad_nonlocal_scalar_damage.i'
  csvdiff = 'ad_nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation."
  issues = '#21786'
[]

[./coupled_pressure]
  type = Exodiff
  input = 'coupled_pressure_test.i'
  exodiff = 'coupled_pressure_test_out.e'
  custom_cmp = 'coupled_pressure_test.exodiff'
  requirement = "The system shall allow to apply a pressure boundary condition from a variable"
  design = 'CoupledPressureBC.md'
  issues = '#11558'
[../]

[crack_front_stress]
  type = 'CSVDiff'
  input = 'crack_front_nonlocal_stress.i'
  csvdiff = 'crack_front_nonlocal_stress_out_CrackFrontNonlocalStress_0001.csv'
  requirement = 'The system shall compute the average stress at each crack point in a 3D domain.'
[]

[screen_output_test]
  type = 'RunApp'
  input = 'crack_loop.i'
  expect_out = '^1       0 .*\n^2       116 .*\n^3       112 .*\n^4       108 .*\n^5       104 .*\n^6       100 .*\n^7       96 .*\n^8       92 .*\n^9       88 .*\n^10      84 .*\n^11      77 .*\n^12      76 .*\n^13      72 .*\n^14      68 .*\n^15      64 .*\n^16      57 .*\n^17      56 .*\n^18      52 .*\n^19      48 .*\n^20      44 .*\n^21      40 .*\n^22      36 .*\n^23      32 .*\n^24      28 .*\n^25      24 .*\n^26      20 .*\n^27      16 .*\n^28      12 .*\n^29      8 .*\n^30      1 '
  no_error_deprecated = true
  requirement = 'The system shall report crack front data for a curved crack front to the console.'
[]

[./ten]
  type = 'CSVDiff'
  input = 'creep.i'
  csvdiff = 'creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten"'
  requirement = 'The system shall compute the proper stress update using the radial return isotropic power law creep model.'
[../]

[./zero]
  type = 'CSVDiff'
  input = 'creep.i'
  csvdiff = 'creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_zero"'
  requirement = "The system shall compute the proper stress update using multiple radial return isotropic power law creep models where one of the models returns zero."
  prereq = ten
[../]

[./sum]
  type = 'CSVDiff'
  input = 'creep.i'
  csvdiff = 'creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_nine creep_one"'
  requirement = "The system shall compute the sum of multiple stress updates using multiple radial return isotropic power law creep models."
  prereq = zero
[../]

[./cycle]
  type = 'CSVDiff'
  input = 'creep.i'
  csvdiff = 'creep_out.csv'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_ten2" Materials/elastic_strain/cycle_models=true'
  requirement = "The system shall support the cycling of multiple creep models when computing stress updates."
  prereq = sum
[../]

[./ten_jacobian]
  type = 'AnalyzeJacobian'
  input = 'creep.i'
  petsc_version = '<3.9.0 || >=3.9.4'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten"'
  requirement = "The system shall produce the correct Jacobians for radial return isotropic power law creep models."
[../]

[./zero_jacobian]
  type = 'AnalyzeJacobian'
  input = 'creep.i'
  petsc_version = '<3.9.0 || >=3.9.4'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_zero"'
  prereq = ten_jacobian
  requirement = "The system shall produce the correct Jacobians for radial return isotropic power law creep models when one of the models returns zero."
[../]

[./sum_jacobian]
  type = 'AnalyzeJacobian'
  input = 'creep.i'
  petsc_version = '<3.9.0 || >=3.9.4'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_nine creep_one"'
  prereq = zero_jacobian
  requirement = "The system shall produce the correct Jacobians for summed radial return isotropic power law creep models."
[../]

[./cycle_jacobian]
  type = 'AnalyzeJacobian'
  input = 'creep.i'
  petsc_version = '<3.9.0 || >=3.9.4'
  cli_args = 'Materials/elastic_strain/inelastic_models="creep_ten creep_ten2" Materials/elastic_strain/cycle_models=true'
  prereq = sum_jacobian
  requirement = "The systam shall produce the correct Jacobians for cyclic creep model evaluation."
[../]

[./uniform]
  type = 'CSVDiff'
  input = 'crit_time_solid_uniform.i'
  csvdiff = 'crit_time_solid_uniform_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-5

  detail = "uniform properties and"
[../]

[./variable]
  type = 'CSVDiff'
  input = 'crit_time_solid_variable.i'
  csvdiff = 'crit_time_solid_variable_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-5

  detail = "variable properties."
[../]

[./timoshenko_smallstrain_critstep]
  type = 'CSVDiff'
  input = 'timoshenko_smallstrain_critstep.i'
  csvdiff = 'timoshenko_smallstrain_critstep_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-5
  requirement = "The system shall correctly compute the critical time step for a beam."
  design = "CriticalTimeStep.md"
[../]

[./except1]
  type = 'RunException'
  input = 'non-isotropic_error_test.i'
  expect_err = 'CriticalTimeStep can only be used with elasticity tensor materials that guarantee isotropic tensors.'
  requirement = "The system shall produce an error if the input elasticity tensor is non-isotropic."
[../]

[test_one_step]
  type = 'CSVDiff'
  input = 'test_one_step.i'
  cli_args = "VectorPostprocessors/section_output/positions='10.0 18.0'"
  csvdiff = 'test_one_step_out_section_output_0001.csv'
  requirement = 'The system shall compute the average of the nodal displacements of a cross section defined by the user via a nodal vector.'
[]

[test_one_step_auto_positions]
  type = 'CSVDiff'
  input = 'test_one_step.i'
  cli_args = 'Outputs/file_base=test_one_step_auto_out'
  csvdiff = 'test_one_step_auto_out_section_output_0001.csv'
  requirement = 'The system shall compute the average of the nodal displacements of a cross section defined by the user via a nodal vector at automatically determined positions.'
[]

[test_adapt]
  type = 'CSVDiff'
  input = 'test_adapt.i'
  csvdiff = 'test_adapt_out_section_output_0001.csv test_adapt_out_section_output_0002.csv'
  requirement = 'The system shall compute the average of the nodal displacements of a cross section at automatically located points that are updated with mesh adaptivity.'
[]

[test_adapt_err]
  type = 'RunException'
  input = 'test_adapt.i'
  cli_args = 'VectorPostprocessors/section_output/require_equal_node_counts=true Outputs/file_base=test_adapt_err_out'
  expect_err = "Node counts do not match for all axial positions. If this behavior is desired to accommodate nonuniform meshes, set 'require_equal_node_counts=false'"
  requirement = 'The system shall compute the average of the nodal displacements of a cross section at automatically located points that are updated with mesh adaptivity.'
[]

[test_one_step_empty_positions_err]
  type = 'RunException'
  input = 'test_one_step.i'
  cli_args = "VectorPostprocessors/section_output/positions='' Outputs/file_base=err_pos_out"
  expect_err = "If 'positions' is specified, at least one value must be provided"
  requirement = 'The system shall generate an error if the user defines an empty set of positions in AverageSectionValueSampler.'
[]

[test_one_step_nonexistent_variable]
  type = 'RunException'
  input = 'test_one_step.i'
  cli_args = "VectorPostprocessors/section_output/variables='dummy' Outputs/file_base=err_var_out"
  expect_err = "One or more of the specified variables do not exist in this system."
  requirement = 'The system shall generate an error if the user specifies a nonexistent variable in AverageSectionValueSampler.'
[]

[test_one_step_heavy]
  type = 'CSVDiff'
  input = 'test_one_step.i'
  cli_args = "VectorPostprocessors/section_output/positions='10.0 18.0' Executioner/end_time=2.0"
  csvdiff = 'test_one_step_out_section_output_0001.csv test_one_step_out_section_output_0002.csv test_one_step_out_section_output_0003.csv test_one_step_out_section_output_0004.csv'
  heavy = true
  requirement = 'The system shall compute the average of the nodal displacements of a cross section defined by the user via a nodal vector at multiple steps.'
[]

[test_one_step_two_ducts]
  type = 'CSVDiff'
  input = 'test_one_step_two_ducts.i'
  csvdiff = 'test_one_step_two_ducts_out_section_output_0001.csv test_one_step_two_ducts_out_section_output_two_0001.csv'
  requirement = 'The system shall compute the average of the nodal displacements of a cross section defined by the user via two nodal vector and two reference points for two respective ducts.'
[]

[test_therm_exp]
  type = 'CSVDiff'
  input = 'test_therm_exp.i'
  csvdiff = 'test_therm_exp_out_section_output_0001.csv'
  requirement = 'The system shall compute the average of the nodal displacements of a cross section with mechanically and thermally induced deformation.'
[]

[test_therm_exp_symm]
  type = 'CSVDiff'
  input = 'test_therm_exp_symm.i'
  csvdiff = 'test_therm_exp_symm_out_section_output_0001.csv'
  ignore_columns = 'node_count'
  rel_err = 5e-3
  requirement = 'The system shall compute the average of the nodal displacements of a cross section with mechanically and thermally induced deformation with a symmetry plane not aligned with a Cartesian coordinate, and match a reference solution without the symmetry plane.'
[]

[thermal_eigenstrain]
  type = 'CSVDiff'
  input = 'thermal_eigenstrain_test.i'
  csvdiff = 'thermal_eigenstrain_test_out.csv'
  allow_warnings = true
  issues = '#17734'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall produce correct thermal deformation gradient values with changing temperature'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[multiple_eigenstrains]
  type = 'CSVDiff'
  input = 'multiple_eigenstrains_test.i'
  csvdiff = 'multiple_eigenstrains_test_out.csv'
  allow_warnings = true
  issues = '#17734'
  requirement = 'The system shall produce correct deformation gradient values for the total and individual eigenstrains'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[thermal_eigenstrain_011orientation]
  type = 'CSVDiff'
  input = 'thermal_eigenstrain_test.i'
  csvdiff = 'thermal_eigenstrain_test_011orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=120.0 Materials/elasticity_tensor/euler_angle_2=125.264 Materials/elasticity_tensor/euler_angle_3=45.0 Outputs/file_base=thermal_eigenstrain_test_011orientation_out Outputs/execute_on=FINAL'
  allow_warnings = true
  issues = '#17734'
  requirement = 'The system shall produce correct thermal deformation gradient values with changing temperature under a 011 loading orientation'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[hcp_thermal_eigenstrain]
  type = 'CSVDiff'
  input = 'hcp_thermal_eigenstrain.i'
  csvdiff = 'hcp_thermal_eigenstrain_out.csv'
  cli_args = 'Outputs/execute_on=FINAL'
  allow_warnings = true
  issues = '#17734'
  requirement = 'The system shall produce correct thermal deformation gradient values with changing temperature for an anisotropic HCP crystal lattice'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md'
[]

[thermal_eigenstrain]
  type = 'CSVDiff'
  input = 'thermal_eigenstrain_test.i'
  csvdiff = 'thermal_eigenstrain_test_out.csv'
  allow_warnings = true
  issues = '#17734'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall produce correct thermal deformation gradient values with changing temperature'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[thermal_eigenstrain_restart]
  type = 'CSVDiff'
  input = 'thermal_eigenstrain_test.i'
  csvdiff = 'thermal_eigenstrain_test_restart_out.csv'
  allow_warnings = true
  cli_args = 'Problem/restart_file_base=thermal_eigenstrain_test_out_cp/LATEST Outputs/file_base=thermal_eigenstrain_test_restart_out
               Executioner/end_time=15'
  issues = '#26458'
  requirement = 'The system shall produce correct thermal deformation gradient values when the simulation is restarted'
  design = '/ComputeMultipleCrystalPlasticityStress.md'
  prereq = 'thermal_eigenstrain'
[]

[multiple_eigenstrains]
  type = 'CSVDiff'
  input = 'multiple_eigenstrains_test.i'
  csvdiff = 'multiple_eigenstrains_test_out.csv'
  allow_warnings = true
  issues = '#17734'
  requirement = 'The system shall produce correct deformation gradient values for the total and individual eigenstrains'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[thermal_eigenstrain_011orientation]
  type = 'CSVDiff'
  input = 'thermal_eigenstrain_test.i'
  csvdiff = 'thermal_eigenstrain_test_011orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=120.0 Materials/elasticity_tensor/euler_angle_2=125.264 Materials/elasticity_tensor/euler_angle_3=45.0 Outputs/file_base=thermal_eigenstrain_test_011orientation_out Outputs/execute_on=FINAL'
  allow_warnings = true
  issues = '#17734'
  requirement = 'The system shall produce correct thermal deformation gradient values with changing temperature under a 011 loading orientation'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[hcp_thermal_eigenstrain]
  type = 'CSVDiff'
  input = 'hcp_thermal_eigenstrain.i'
  csvdiff = 'hcp_thermal_eigenstrain_out.csv'
  cli_args = 'Outputs/execute_on=FINAL'
  allow_warnings = true
  issues = '#17734'
  requirement = 'The system shall produce correct thermal deformation gradient values with changing temperature for an anisotropic HCP crystal lattice'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md'
[]

[volumetric_eigenstrain_increase]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_increase.i'
  csvdiff = 'volumetric_eigenstrain_increase_out.csv'
  issues = '#25932'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall produce a positive isotropic eigenstrain in response to an increasing number density and shall demonstrate an applied shear stress on the slip systems with a z-component in response to the BCs on displacement in the z-direction.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[volumetric_eigenstrain_increase_restart]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_increase.i'
  csvdiff = 'volumetric_eigenstrain_increase_restart_out.csv'
  cli_args = 'Problem/restart_file_base=volumetric_eigenstrain_increase_out_cp/LATEST Outputs/file_base=volumetric_eigenstrain_increase_restart_out Executioner/end_time=7.5'
  issues = '#26458'
  requirement = 'The system shall continue the isotropic eigenstrain response calculation upon simulation restart.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[hcp_volumetric_eigenstrain_decrease]
  type = 'CSVDiff'
  input = 'hcp_volumetric_eigenstrain_decrease.i'
  csvdiff = 'hcp_volumetric_eigenstrain_decrease_out.csv'
  issues = '#25932'
  requirement = 'The system shall produce a negative isotropic eigenstrain in response to an decreasing average radius and shall demonstrate an applied stress on the slip systems with a z-component in response to the BC constraints on displacement of the crystal in the z-direction.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md'
[]

[volumetric_eigenstrain_parabolic]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_parabolic.i'
  csvdiff = 'volumetric_eigenstrain_parabolic_out.csv'
  issues = '#25932'
  requirement = 'The system shall produce an isotropic eigenstrain in response to parabolic evolution of both the void number density and average radius, and shall induce plastic deformation in the crystal plasticity reponse through the state dependance of the deformation gradient that final strain state of the FCC crystal is not zero.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[update_method_hcp_basal_active_restart]
  type = 'CSVDiff'
  input = 'update_method_hcp_basal_active.i'
  csvdiff = 'update_method_hcp_basal_active_restart_out.csv'
  allow_warnings = true
  cli_args = 'Problem/restart_file_base=update_method_hcp_basal_active_out_cp/LATEST Outputs/file_base=update_method_hcp_basal_active_restart_out Executioner/end_time=2.75 Executioner/dt=0.125'
  detail = 'continue to evolve the forest dislocation densities on basal <a> slip planes.'
  prereq = 'constitutive_model/update_method_hcp_basal_active'
[]

[update_method_hcp_aprismatic_capyramidal_restart]
  type = 'CSVDiff'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  csvdiff = 'update_method_hcp_aprismatic_capyramidal_restart_out.csv'
  cli_args = 'Problem/restart_file_base=update_method_hcp_aprismatic_capyramidal_out_cp/LATEST Outputs/file_base=update_method_hcp_aprismatic_capyramidal_restart_out Executioner/end_time=6'
  allow_warnings = true
  detail = 'continue to compute the slip system strength and resolved applied shear stress for the prismatic<a> and pyramidal<c+a> slip systems.'
  prereq = 'constitutive_model/update_method_hcp_aprismatic_capyramidal'
[]

[update_method_hcp_representative_slip_systems]
  type = 'CSVDiff'
  input = 'update_method_hcp_representative_slip_systems.i'
  csvdiff = 'update_method_hcp_representative_slip_systems_out.csv'
  allow_warnings = true
  detail = ' compute the Schmid tensors and resulting resolved applied shear stress for a non-physical representative set of basal, prismatic, and pyramidal slip systems;'
[]

[update_method_hcp_representative_equal_lattice_parameters]
  type = 'RunException'
  input = 'update_method_hcp_representative_slip_systems.i'
  cli_args = 'Materials/trial_xtalpl/unit_cell_dimension="3e-7 3e-7 3e-7"'
  expect_err = 'The specified unit cell dimensions are not consistent with expectations for HCP crystal hexagonal lattices'
  detail = 'ensure that the provided lattice parameters match the expectation a = b != c for HCP crystals;'
[]

[update_method_hcp_representative_incorrect_index_numbers]
  type = 'RunException'
  input = 'update_method_hcp_representative_slip_systems.i'
  cli_args = 'Materials/trial_xtalpl/slip_sys_file_name=input_slip_sys.txt Materials/trial_xtalpl/number_slip_systems=12'
  expect_err = 'CrystalPlasticityStressUpdateBase Error: The number of entries in the first row of the slip system file is not consistent with the expectations for the 4-index Miller-Bravais assumption for HCP crystals. This file should represent both the slip plane normal and the slip direction with 4-indices each.'
  detail = 'ensure that eight indices are given for the Miller-Bravais notation for HCP slip systems;'
[]

[update_method_hcp_representative_incorrect_basal_plane]
  type = 'RunException'
  input = 'update_method_hcp_representative_slip_systems.i'
  cli_args = 'Materials/trial_xtalpl/slip_sys_file_name=error_slip_sys_hcp.txt'
  expect_err = 'CrystalPlasticityStressUpdateBase Error: The specified HCP basal plane Miller-Bravais indices do not sum to zero. Check the values supplied in the associated text file.'
  detail = ' ensure that the Miller-Bravais basal plane indices sum to zero.'
[]

[update_method_hcp_representative_incorrect_basal_slip_direction]
  type = 'RunException'
  input = 'update_method_hcp_representative_slip_systems.i'
  cli_args = 'Materials/trial_xtalpl/slip_sys_file_name=error_slip_dir_sys_hcp.txt Materials/trial_xtalpl/number_slip_systems=1'
  expect_err = 'CrystalPlasticityStressUpdateBase Error: The specified HCP slip direction Miller-Bravais indices in the basal plane '
  detail = ' ensure that the Miller-Bravais indices for the slip direction  in the basal plane sum to zero.'
[]

[update_method_hcp_convergence_issue_flag]
  type = 'RunException'
  input = 'update_method_hcp_convergence_issue_flag.i'
  expect_err = 'Maximum allowable slip increment exceeded'
  detail = ' provide warning messages about constitutive model and slip increment convergence issues when the corresponding input file parameter is set to true.'
[]

[update_method_hcp_stress_convergence_issue_flag]
  type = 'RunException'
  input = 'update_method_hcp_convergence_issue_flag.i'
  cli_args = 'Materials/trial_xtalpl/slip_increment_tolerance=2.0 Materials/stress/maxiter=1'
  expect_err = 'ComputeMultipleCrystalPlasticityStress: Stress Integration error rmax ='
  detail = 'provide warning messages about constitutive model stress convergence issues with the appropriate input file parameter setting.'
[]

[modified_kalidindi_for_hcp]
  type = CSVDiff
  input = 'modified_kalidindi_for_hcp.i'
  csvdiff = 'modified_kalidindi_for_hcp_out.csv'
  detail = 'calculate the Schmid tensor for a set of HCP twin systems given in Miller-Bravais indices and shall calculate a twin volume fraction when using the FCC Kalidindi twinning model with a modified input file.'
[]

[demonstration_combined_hcp_slip_twins]
  type = CSVDiff
  input = 'demonstration_combined_hcp_slip_twins.i'
  csvdiff = 'demonstration_combined_hcp_slip_twins_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  detail = 'compute a plastic velocity gradient that accounts for deformation contributions from both slip and twinning in an HCP crystal.'
[]

[demonstration_combined_hcp_slip_twins_restart]
  type = CSVDiff
  input = 'demonstration_combined_hcp_slip_twins.i'
  csvdiff = 'demonstration_combined_hcp_slip_twins_restart_out.csv'
  cli_args = 'Problem/restart_file_base=demonstration_combined_hcp_slip_twins_out_cp/LATEST Outputs/file_base=demonstration_combined_hcp_slip_twins_restart_out Executioner/end_time=2.5 Executioner/dt=0.125'
  requirement = 'The crystal plasticity system shall compute the plastic velocity gradient  from both slip and twinning in anHCP crystal upon simulation restart.'
  issues = '#26458'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md /CrystalPlasticityTwinningKalidindiUpdate.md'
  prereq = 'coupling_demonstration/demonstration_combined_hcp_slip_twins'
[]

[update_model_test]
  type = 'Exodiff'
  input = 'update_method_test.i'
  exodiff = 'update_method_test_out.e'
  issues = '#16064'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall provide a StressUpdate material-based extensible crystal plasticity system'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[update_model_test_restart]
  type = 'CSVDiff'
  input = 'update_method_test.i'
  csvdiff = 'update_method_test_restart_out.csv'
  cli_args = 'Problem/restart_file_base=update_method_test_out_cp/LATEST Outputs/file_base=update_method_test_restart_out Outputs/exodus=false Outputs/csv=true'
  issues = '#26458'
  requirement = 'The system shall provide a StressUpdate material-based extensible crystal plasticity framework that shall continue the state-dependent calculation upon restart'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
  prereq = 'update_model_test'
[]

[update_model_011orientation]
  type = 'CSVDiff'
  input = 'update_method_011orientation.i'
  csvdiff = 'update_method_011orientation_out.csv'
  issues = '#16064'
  requirement = 'The material-based crystal plasticity model shall compute the lagrangian stress, PK2 stress, and slip for an orientation not aligned with the Cartesian coordinate system.'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[exception]
  type = 'Exodiff'
  input = 'exception.i'
  exodiff = 'exception_out.e'
  allow_warnings = true
  issues = '#16064'
  requirement = 'A constitutive failure shall trigger an exception leading to a cut time step rather than a failed solve using the stress-update based crystal plasticity implementation'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[substep]
  type = 'Exodiff'
  input = 'substep.i'
  exodiff = 'substep_out.e'
  allow_warnings = true
  issues = '#6097'
  requirement = 'The crystal plasticity system shall provide a substepping capability for improved convergence using the stress-update based crystal plasticity implementation'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[use_substep_dt]
  type = 'CSVDiff'
  input = 'use_substep_dt.i'
  csvdiff = 'use_substep_dt_out.csv'
  allow_warnings = true
  valgrind = HEAVY
  issues = '#17340'
  requirement = 'The system shall apply correct boundary condition after timestep being cut during substepping using the stress-update based crystal plasticity implementation'
  design = '/ComputeMultipleCrystalPlasticityStress.md'
[]

[update_euler_angle_111_orientation]
  type = 'CSVDiff'
  input = 'update_euler_angle.i'
  csvdiff = 'update_euler_angle_111_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=0 Materials/elasticity_tensor/euler_angle_2=54.7 Materials/elasticity_tensor/euler_angle_3=45 Outputs/file_base=update_euler_angle_111_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (111).'
  issues = '#19473'
  design = '/ComputeUpdatedEulerAngle.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[update_euler_angle_112_orientation]
  type = 'CSVDiff'
  input = 'update_euler_angle.i'
  csvdiff = 'update_euler_angle_112_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=90 Materials/elasticity_tensor/euler_angle_2=30 Materials/elasticity_tensor/euler_angle_3=45 Outputs/file_base=update_euler_angle_112_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (112).'
  issues = '#19473'
  design = '/ComputeUpdatedEulerAngle.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[update_euler_angle_123_orientation]
  type = 'CSVDiff'
  input = 'update_euler_angle.i'
  csvdiff = 'update_euler_angle_123_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=50 Materials/elasticity_tensor/euler_angle_2=34 Materials/elasticity_tensor/euler_angle_3=65 Outputs/file_base=update_euler_angle_123_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (123). '
  issues = '#19473'
  design = '/ComputeUpdatedEulerAngle.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[bicrystal_test]
  type = 'CSVDiff'
  input = 'bicrystal_test.i'
  csvdiff = 'bicrystal_test_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall allow multiple crystal plasticity models to be used in a polycrystalline simulation through the use of the base_name input parameter.'
  issues = '#21036'
  design = '/ComputeMultipleCrystalPlasticityStress.md'
[]

[bicrystal_test_restart]
  type = 'CSVDiff'
  input = 'bicrystal_test.i'
  csvdiff = 'bicrystal_test_restart_out.csv'
  requirement = 'The system shall allow multiple crystal plasticity models to be used in a polycrystalline simulation with the restart capability.'
  cli_args = 'Problem/restart_file_base=bicrystal_test_out_cp/LATEST Outputs/file_base=bicrystal_test_restart_out'
  issues = '#26458'
  design = '/ComputeMultipleCrystalPlasticityStress.md'
  prereq = 'bicrystal_test'
[]

[only_twinning_fcc_restart]
  type = 'CSVDiff'
  input = 'only_twinning_fcc.i'
  csvdiff = 'only_twinning_fcc_restart_out.csv'
  allow_warnings = true
  cli_args = 'Problem/restart_file_base=only_twinning_fcc_out_cp/LATEST Outputs/file_base=only_twinning_fcc_restart_out'
  detail = 'continue to compute the plastic shear due to twinning after a simulation restart.'
  prereq = 'constiutive_model/only_twinning_fcc'
  method = "!dbg"
[]

[combined_twinning_slip_111tension_restart]
  type = CSVDiff
  input = 'combined_twinning_slip_111tension.i'
  csvdiff = 'combined_twinning_slip_111tension_restart_out.csv'
  cli_args = 'Problem/restart_file_base=combined_twinning_slip_111tension_out_cp/LATEST Outputs/file_base=combined_twinning_slip_111tension_restart_out Executioner/dtmin=0.001'
  detail = 'continue to calculate plastic shear due to both dislocation slip and twinning when loaded under tension in a 111 orientation in a simulation restart.'
  prereq = 'combined_twinning_slip_models/combined_twinning_slip_111tension'
[]

[hcp_thermal_eigenstrain]
  type = 'CSVDiff'
  input = 'hcp_thermal_eigenstrain.i'
  csvdiff = 'hcp_thermal_eigenstrain_out.csv'
  cli_args = 'Outputs/execute_on=FINAL'
  allow_warnings = true
  issues = '#17734'
  requirement = 'The system shall produce correct thermal deformation gradient values with changing temperature for an anisotropic HCP crystal lattice'
  design = '/ComputeCrystalPlasticityThermalEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md'
[]

[hcp_volumetric_eigenstrain_decrease]
  type = 'CSVDiff'
  input = 'hcp_volumetric_eigenstrain_decrease.i'
  csvdiff = 'hcp_volumetric_eigenstrain_decrease_out.csv'
  issues = '#25932'
  requirement = 'The system shall produce a negative isotropic eigenstrain in response to an decreasing average radius and shall demonstrate an applied stress on the slip systems with a z-component in response to the BC constraints on displacement of the crystal in the z-direction.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md'
[]

[update_method_hcp_aprismatic_capyramidal]
  type = 'CSVDiff'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  csvdiff = 'update_method_hcp_aprismatic_capyramidal_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  allow_warnings = true
  detail = 'compute the slip system strength and resolved applied shear stress for the prismatic<a> and pyramidal<c+a> slip systems when loaded along the c-axis;'
[]

[update_method_hcp_aprismatic_active]
  type = 'CSVDiff'
  input = 'update_method_hcp_aprismatic_active.i'
  csvdiff = 'update_method_hcp_aprismatic_active_out.csv'
  allow_warnings = true
  detail = 'evolve the forest dislocation and substructure densities on prismatic<a> slip planes when loaded in an appropriate orientation;'
[]

[update_method_hcp_capyramidal_active]
  type = 'CSVDiff'
  input = 'update_method_hcp_capyramidal_active.i'
  csvdiff = 'update_method_hcp_capyramidal_active_out.csv'
  allow_warnings = true
  detail = 'evolve the forest dislocation densities on pyramidal <c+a> slip planes and the substructure density when the crystal is loaded in an appropriate orientation.'
[]

[update_method_hcp_basal_active]
  type = 'CSVDiff'
  input = 'update_method_hcp_basal_active.i'
  csvdiff = 'update_method_hcp_basal_active_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  allow_warnings = true
  detail = 'evolve the forest dislocation densities on basal <a> slip planes when the crystal is loaded in an appropriate orientation.'
[]

[update_method_hcp_no_substructure]
  type = 'CSVDiff'
  input = 'update_method_hcp_no_substructure.i'
  csvdiff = 'update_method_hcp_no_substructure_out.csv'
  allow_warnings = true
  detail = 'prevent the calculation of a negative substructure density increment.'
[]

[update_method_hcp_no_negative_aprismatic]
  type = 'CSVDiff'
  input = 'update_method_hcp_no_negative_aprismatic.i'
  csvdiff = 'update_method_hcp_no_negative_aprismatic_out.csv'
  allow_warnings = true
  detail = 'prevent the calculation of a negative total forest density.'
[]

[update_method_hcp_size_slip_modes]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/number_slip_systems_per_mode="3 3 9"'
  expect_err = 'The size the number of slip systems per mode is not equal to the number of slip system types'
  detail = 'ensure the user specifies a number of the slip systems per mode which is equal to the number of modes;'
[]

[update_method_hcp_sum_slip_modes_vs_systems]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/number_slip_systems_per_mode="3 15"'
  expect_err = 'The number of slip systems and the sum of the slip systems in each of the slip system modes are not equal'
  detail = 'ensure the user specifies an equal total number of slip systems  and the sum of the different slip mode systems;'
[]

[update_method_hcp_size_burgers_vectors]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/burgers_vector_per_mode="2"'
  expect_err = 'Please ensure that the size of burgers_vector_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a number of burgers vectors per mode that is equal to the number of modes;'
[]

[update_method_hcp_size_slip_generation]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/slip_generation_coefficient_per_mode="1 2 3"'
  expect_err = 'Please ensure that the size of slip_generation_coefficient_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a number of slip generation coefficient per mode that is equal to the number of modes;'
[]

[update_method_hcp_size_activation_energy]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/normalized_slip_activiation_energy_per_mode="1 2 3 4"'
  expect_err = 'Please ensure that the size of normalized_slip_activiation_energy_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a size of slip activation energy per mode that is equal to the specified number of modes;'
[]

[update_method_hcp_size_proportionality_factor]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/slip_energy_proportionality_factor_per_mode="1"'
  expect_err = 'Please ensure that the size of slip_energy_proportionality_factor_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a size of slip energy proportionality factor per mode that is equal to the specified number of modes;'
[]

[update_method_hcp_size_shear_modulus]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/effective_shear_modulus_per_mode="1"'
  expect_err = 'Please ensure that the size of effective_shear_modulus_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a size of effective shear modulus per mode that is equal to the specified number of modes;'
[]

[update_method_hcp_size_substructure_rate]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/substructure_rate_coefficient_per_mode="3 2 1"'
  expect_err = 'Please ensure that the size of substructure_rate_coefficient_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a size of substructure generation rate coefficient per mode that is equal to the specified number of modes;'
[]

[update_method_hcp_size_hall_petch]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/Hall_Petch_like_constant_per_mode="1"'
  expect_err = 'Please ensure that the size of Hall_Petch_like_constant_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a size of Hall-Petch like coefficient per mode that is equal to the specified number of modes;'
[]

[update_method_hcp_size_lattice_friction]
  type = 'RunException'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  cli_args = 'Materials/trial_xtalpl/lattice_friction_per_mode="3"'
  expect_err = 'Please ensure that the size of lattice_friction_per_mode equals the value supplied for slip_system_modes'
  detail = 'ensure the user specifies a size of lattice friction values per mode that is equal to the specified number of modes;'
[]

[update_method_hcp_basal_active_restart]
  type = 'CSVDiff'
  input = 'update_method_hcp_basal_active.i'
  csvdiff = 'update_method_hcp_basal_active_restart_out.csv'
  allow_warnings = true
  cli_args = 'Problem/restart_file_base=update_method_hcp_basal_active_out_cp/LATEST Outputs/file_base=update_method_hcp_basal_active_restart_out Executioner/end_time=2.75 Executioner/dt=0.125'
  detail = 'continue to evolve the forest dislocation densities on basal <a> slip planes.'
  prereq = 'constitutive_model/update_method_hcp_basal_active'
[]

[update_method_hcp_aprismatic_capyramidal_restart]
  type = 'CSVDiff'
  input = 'update_method_hcp_aprismatic_capyramidal.i'
  csvdiff = 'update_method_hcp_aprismatic_capyramidal_restart_out.csv'
  cli_args = 'Problem/restart_file_base=update_method_hcp_aprismatic_capyramidal_out_cp/LATEST Outputs/file_base=update_method_hcp_aprismatic_capyramidal_restart_out Executioner/end_time=6'
  allow_warnings = true
  detail = 'continue to compute the slip system strength and resolved applied shear stress for the prismatic<a> and pyramidal<c+a> slip systems.'
  prereq = 'constitutive_model/update_method_hcp_aprismatic_capyramidal'
[]

[modified_kalidindi_for_hcp]
  type = CSVDiff
  input = 'modified_kalidindi_for_hcp.i'
  csvdiff = 'modified_kalidindi_for_hcp_out.csv'
  detail = 'calculate the Schmid tensor for a set of HCP twin systems given in Miller-Bravais indices and shall calculate a twin volume fraction when using the FCC Kalidindi twinning model with a modified input file.'
[]

[demonstration_combined_hcp_slip_twins]
  type = CSVDiff
  input = 'demonstration_combined_hcp_slip_twins.i'
  csvdiff = 'demonstration_combined_hcp_slip_twins_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  detail = 'compute a plastic velocity gradient that accounts for deformation contributions from both slip and twinning in an HCP crystal.'
[]

[demonstration_combined_hcp_slip_twins_restart]
  type = CSVDiff
  input = 'demonstration_combined_hcp_slip_twins.i'
  csvdiff = 'demonstration_combined_hcp_slip_twins_restart_out.csv'
  cli_args = 'Problem/restart_file_base=demonstration_combined_hcp_slip_twins_out_cp/LATEST Outputs/file_base=demonstration_combined_hcp_slip_twins_restart_out Executioner/end_time=2.5 Executioner/dt=0.125'
  requirement = 'The crystal plasticity system shall compute the plastic velocity gradient  from both slip and twinning in anHCP crystal upon simulation restart.'
  issues = '#26458'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md /CrystalPlasticityTwinningKalidindiUpdate.md'
  prereq = 'coupling_demonstration/demonstration_combined_hcp_slip_twins'
[]

[volumetric_eigenstrain_increase]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_increase.i'
  csvdiff = 'volumetric_eigenstrain_increase_out.csv'
  issues = '#25932'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall produce a positive isotropic eigenstrain in response to an increasing number density and shall demonstrate an applied shear stress on the slip systems with a z-component in response to the BCs on displacement in the z-direction.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[volumetric_eigenstrain_increase_restart]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_increase.i'
  csvdiff = 'volumetric_eigenstrain_increase_restart_out.csv'
  cli_args = 'Problem/restart_file_base=volumetric_eigenstrain_increase_out_cp/LATEST Outputs/file_base=volumetric_eigenstrain_increase_restart_out Executioner/end_time=7.5'
  issues = '#26458'
  requirement = 'The system shall continue the isotropic eigenstrain response calculation upon simulation restart.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[hcp_volumetric_eigenstrain_decrease]
  type = 'CSVDiff'
  input = 'hcp_volumetric_eigenstrain_decrease.i'
  csvdiff = 'hcp_volumetric_eigenstrain_decrease_out.csv'
  issues = '#25932'
  requirement = 'The system shall produce a negative isotropic eigenstrain in response to an decreasing average radius and shall demonstrate an applied stress on the slip systems with a z-component in response to the BC constraints on displacement of the crystal in the z-direction.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md'
[]

[volumetric_eigenstrain_parabolic]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_parabolic.i'
  csvdiff = 'volumetric_eigenstrain_parabolic_out.csv'
  issues = '#25932'
  requirement = 'The system shall produce an isotropic eigenstrain in response to parabolic evolution of both the void number density and average radius, and shall induce plastic deformation in the crystal plasticity reponse through the state dependance of the deformation gradient that final strain state of the FCC crystal is not zero.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[volumetric_eigenstrain_density_check]
  type = 'RunException'
  input = 'volumetric_eigenstrain_increase.i'
  cli_args = 'Materials/void_density/expression="-0.01"'
  expect_err = 'A negative, non-physical spherical void number density has been provided: -0.01. This value is non-physical and violates the assumptions of this eigenstrain class'
  requirement = 'The system shall not attempt to calculate the volumetric eigenstrain from a negative number density of voids.'
  issues = '#25932'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md'
[]

[volumetric_eigenstrain_radius_check]
  type = 'RunException'
  input = 'volumetric_eigenstrain_increase.i'
  cli_args = 'Materials/void_radius/prop_values="-1.0e-6"'
  expect_err = 'A negative mean spherical void radius value, -1e-06, has been provided; this value is non-physical and violates the assumptions of this eigenstrain class'
  requirement = 'The system shall not attempt to calculate the volumetric eigenstrain from a negative average radius value.'
  issues = '#25932'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md'
[]

[volumetric_eigenstrain_increase]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_increase.i'
  csvdiff = 'volumetric_eigenstrain_increase_out.csv'
  issues = '#25932'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall produce a positive isotropic eigenstrain in response to an increasing number density and shall demonstrate an applied shear stress on the slip systems with a z-component in response to the BCs on displacement in the z-direction.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[volumetric_eigenstrain_parabolic]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain_parabolic.i'
  csvdiff = 'volumetric_eigenstrain_parabolic_out.csv'
  issues = '#25932'
  requirement = 'The system shall produce an isotropic eigenstrain in response to parabolic evolution of both the void number density and average radius, and shall induce plastic deformation in the crystal plasticity reponse through the state dependance of the deformation gradient that final strain state of the FCC crystal is not zero.'
  design = '/ComputeCrystalPlasticityVolumetricEigenstrain.md /ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[update_model_test]
  type = 'Exodiff'
  input = 'update_method_test.i'
  exodiff = 'update_method_test_out.e'
  issues = '#16064'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  requirement = 'The system shall provide a StressUpdate material-based extensible crystal plasticity system'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[update_model_test_restart]
  type = 'CSVDiff'
  input = 'update_method_test.i'
  csvdiff = 'update_method_test_restart_out.csv'
  cli_args = 'Problem/restart_file_base=update_method_test_out_cp/LATEST Outputs/file_base=update_method_test_restart_out Outputs/exodus=false Outputs/csv=true'
  issues = '#26458'
  requirement = 'The system shall provide a StressUpdate material-based extensible crystal plasticity framework that shall continue the state-dependent calculation upon restart'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
  prereq = 'update_model_test'
[]

[update_model_011orientation]
  type = 'CSVDiff'
  input = 'update_method_011orientation.i'
  csvdiff = 'update_method_011orientation_out.csv'
  issues = '#16064'
  requirement = 'The material-based crystal plasticity model shall compute the lagrangian stress, PK2 stress, and slip for an orientation not aligned with the Cartesian coordinate system.'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[exception]
  type = 'Exodiff'
  input = 'exception.i'
  exodiff = 'exception_out.e'
  allow_warnings = true
  issues = '#16064'
  requirement = 'A constitutive failure shall trigger an exception leading to a cut time step rather than a failed solve using the stress-update based crystal plasticity implementation'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[substep]
  type = 'Exodiff'
  input = 'substep.i'
  exodiff = 'substep_out.e'
  allow_warnings = true
  issues = '#6097'
  requirement = 'The crystal plasticity system shall provide a substepping capability for improved convergence using the stress-update based crystal plasticity implementation'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityKalidindiUpdate.md'
[]

[linesearch]
  type = 'Exodiff'
  input = 'linesearch.i'
  exodiff = 'linesearch_out.e'
  issues = '#16064'
  requirement = 'The crystal plasticity system shall implement a line search capability for accelerated internal Newton solves using the stress-update based crystal plasticity implementation'
  design = '/CrystalPlasticityKalidindiUpdate.md'
[]

[combined_twinning_slip_111tension]
  type = CSVDiff
  input = 'combined_twinning_slip_111tension.i'
  csvdiff = 'combined_twinning_slip_111tension_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  detail = 'compute plastic shear due to both slip and twin propagation when loaded under tension in a 111 orientation.'
[]

[combined_twinning_slip_111compression]
  type = CSVDiff
  input = 'combined_twinning_slip_111tension.i'
  csvdiff = 'combined_twinning_slip_111compression_out.csv'
  cli_args = 'BCs/tdisp/function=-0.02*t Outputs/file_base=combined_twinning_slip_111compression_out '
  detail = 'compute a near-zero twin volume fraction when loaded under compression in a 111 orientation.'
[]

[combined_twinning_slip_100tension]
  type = CSVDiff
  input = 'combined_twinning_slip_100compression.i'
  csvdiff = 'combined_twinning_slip_100tension_out.csv'
  cli_args = 'BCs/tdisp/function=0.025*t Outputs/file_base=combined_twinning_slip_100tension_out'
  detail = 'compute a near-zero volume fraction of twins for all twin system when a 100 oriented crystal is loaded under tension.'
[]

[combined_twinning_slip_100compression]
  type = CSVDiff
  input = 'combined_twinning_slip_100compression.i'
  csvdiff = 'combined_twinning_slip_100compression_out.csv'
  detail = 'compute both dislocation glide and twin propagation in a 100 oriented crystal loaded under compression.'
[]

[only_twinning_fcc_restart]
  type = 'CSVDiff'
  input = 'only_twinning_fcc.i'
  csvdiff = 'only_twinning_fcc_restart_out.csv'
  allow_warnings = true
  cli_args = 'Problem/restart_file_base=only_twinning_fcc_out_cp/LATEST Outputs/file_base=only_twinning_fcc_restart_out'
  detail = 'continue to compute the plastic shear due to twinning after a simulation restart.'
  prereq = 'constiutive_model/only_twinning_fcc'
  method = "!dbg"
[]

[combined_twinning_slip_111tension_restart]
  type = CSVDiff
  input = 'combined_twinning_slip_111tension.i'
  csvdiff = 'combined_twinning_slip_111tension_restart_out.csv'
  cli_args = 'Problem/restart_file_base=combined_twinning_slip_111tension_out_cp/LATEST Outputs/file_base=combined_twinning_slip_111tension_restart_out Executioner/dtmin=0.001'
  detail = 'continue to calculate plastic shear due to both dislocation slip and twinning when loaded under tension in a 111 orientation in a simulation restart.'
  prereq = 'combined_twinning_slip_models/combined_twinning_slip_111tension'
[]

[euler_angle_auxvar]
  type = 'CSVDiff'
  input = 'euler_angle_auxvar.i'
  csvdiff = 'euler_angle_auxvar_out.csv'
  requirement = 'The crystal plasticity models should be able to utilize Euler angle values supplied through AuxVariables.'
[]

[euler_angle_auxvar_conflict]
  type = 'RunException'
  input = 'euler_angle_conflict.i'
  expect_err = 'Euler angles cannot be supplied from both coupled variables and auxiliary input file in the option `read_prop_user_object`.'
  requirement = 'An error will be thrown when trying to set Euler angles information from a text file and AuxVariables at the same time.'
[]

[euler_angle_components]
  type = 'RunException'
  input = 'euler_angle_auxvar.i'
  expect_err = 'The Euler angles should have three components.'
  cli_args = 'Materials/elasticity_tensor/euler_angle_variables="euler_angle_1"'
  requirement = 'An error will be thrown when trying to set Euler angles information with less than three components.'
[]

[orthotropic_rotation_Cijkl]
  type = 'CSVDiff'
  input = 'orthotropic_rotation_Cijkl.i'
  csvdiff = 'orthotropic_rotation_Cijkl_out.csv'
  issues = '#10629'
  requirement = 'The crystal plasticity rotations shall correctly rotate the elasticity tensors at each material point using the stress-update based crystal plasticity implementation'
  design = '/ComputeElasticityTensorCP.md'
[]

[rotation_matrix_update_euler_angle_111_orientation]
  type = 'CSVDiff'
  input = 'rotation_matrix_update_euler_angle_111_orientation.i'
  csvdiff = 'rotation_matrix_update_euler_angle_111_orientation_out.csv'
  requirement = 'The system shall produce the initial Euler angles phi1=0, psi=54.7356103, and phi2=45 when supplied with the associated rotation matrix and shall calculate a relatively higher 2nd Piola Kirchoff stress in agreement with the low Schmid factor for this loading orientation.'
  issues = '#23451'
  design = '/ComputeElasticityTensorCP.md /ComputeUpdatedEulerAngle.md '
[]

[rotation_matrix_update_euler_angle_011_orientation]
  type = 'CSVDiff'
  input = 'rotation_matrix_update_euler_angle_111_orientation.i'
  csvdiff = 'rotation_matrix_update_euler_angle_011_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/rotation_matrix="0.5 0.5   0.707106781 -0.5 -0.5 0.707106781 0.707106781 0.0 0.0" Outputs/file_base=rotation_matrix_update_euler_angle_011_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce the initial Euler angles of phi1=45, psi=90, and phi2=45, which shall quickly update as the crystal rotates, when supplied with the associated rotation matrix. The system shall calculate a relatively low 2nd Piola Kirchoff stress in the z-direction in agreement with the high Schmid factor for this loading orientation'
  issues = '#23451'
  design = '/ComputeElasticityTensorCP.md /ComputeUpdatedEulerAngle.md '
[]

[rotation_matrix_update_euler_angle_112_orientation]
  type = 'CSVDiff'
  input = 'rotation_matrix_update_euler_angle_111_orientation.i'
  csvdiff = 'rotation_matrix_update_euler_angle_112_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/rotation_matrix="-0.612372436 0.707106781 0.353553391 -0.612372436 -0.707106781 0.353553391 0.5 0.0 0.866025404" Outputs/file_base=rotation_matrix_update_euler_angle_112_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce the initial Euler angles of phi1=90, psi=30, and phi2=35, when supplied with the associated rotation matrix, and the updated Euler angles values as the crystal under goes rotation during deformation.'
  issues = '#23451'
  design = '/ComputeElasticityTensorCP.md /ComputeUpdatedEulerAngle.md '
[]

[rotation_matrix_and_euler_angles_error]
  type = RunException
  input = 'rotation_matrix_update_euler_angle_111_orientation.i'
  cli_args = 'Materials/elasticity_tensor/euler_angle_2=50'
  expect_err = 'Bunge Euler angle information and the rotation_matrix cannot both be specified. Provide only one type of orientation information in the input file.'
  requirement = 'The system shall not allow specification of both the rotation matrix and the Bunge Euler angles within the same input file.'
  issues = '#23451'
  design = '/ComputeElasticityTensorCP.md'
[]

[./orthotropic_rotation_Cijkl]
  type = 'CSVDiff'
  input = 'orthotropic_rotation_Cijkl.i'
  csvdiff = 'orthotropic_rotation_Cijkl_out.csv'
  issues = '#10629'
  requirement = 'The crystal plasticity rotations shall correctly rotate the elasticity tensors at each material point'
  design = '/ComputeElasticityTensorCP.md'
[../]

[modified_kalidindi_for_hcp]
  type = CSVDiff
  input = 'modified_kalidindi_for_hcp.i'
  csvdiff = 'modified_kalidindi_for_hcp_out.csv'
  detail = 'calculate the Schmid tensor for a set of HCP twin systems given in Miller-Bravais indices and shall calculate a twin volume fraction when using the FCC Kalidindi twinning model with a modified input file.'
[]

[demonstration_combined_hcp_slip_twins]
  type = CSVDiff
  input = 'demonstration_combined_hcp_slip_twins.i'
  csvdiff = 'demonstration_combined_hcp_slip_twins_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  detail = 'compute a plastic velocity gradient that accounts for deformation contributions from both slip and twinning in an HCP crystal.'
[]

[demonstration_combined_hcp_slip_twins_restart]
  type = CSVDiff
  input = 'demonstration_combined_hcp_slip_twins.i'
  csvdiff = 'demonstration_combined_hcp_slip_twins_restart_out.csv'
  cli_args = 'Problem/restart_file_base=demonstration_combined_hcp_slip_twins_out_cp/LATEST Outputs/file_base=demonstration_combined_hcp_slip_twins_restart_out Executioner/end_time=2.5 Executioner/dt=0.125'
  requirement = 'The crystal plasticity system shall compute the plastic velocity gradient  from both slip and twinning in anHCP crystal upon simulation restart.'
  issues = '#26458'
  design = '/ComputeMultipleCrystalPlasticityStress.md /CrystalPlasticityHCPDislocationSlipBeyerleinUpdate.md /CrystalPlasticityTwinningKalidindiUpdate.md'
  prereq = 'coupling_demonstration/demonstration_combined_hcp_slip_twins'
[]

[only_twinning_fcc]
  type = 'CSVDiff'
  input = 'only_twinning_fcc.i'
  csvdiff = 'only_twinning_fcc_out.csv'
  allow_warnings = true
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  detail = 'compute the plastic shear due to twinning as a function of the applied shear stress and resistance to twin propagation, the corresponding twin volume fraction per twin system, and the total value of the twin volume fraction across all twin systems.'
[]

[check_direction_twin_propagation]
  type = 'CSVDiff'
  input = 'check_direction_twin_propagation.i'
  csvdiff = 'check_direction_twin_propagation_out.csv'
  allow_warnings = true
  detail = 'compute a non-zero twin volume fraction, and associate plastic shear increment, for only postive applied shear stress values.'
[]

[coplanar_twin_hardening]
  type = 'CSVDiff'
  input = 'coplanar_twin_hardening.i'
  csvdiff = 'coplanar_twin_hardening_out.csv'
  detail = 'calculate the coplanar twin propogation resistance contribution as a function of the twin volume fractions on coplanar systems alone.'
[]

[non_coplanar_twin_hardening]
  type = 'CSVDiff'
  input = 'non_coplanar_twin_hardening.i'
  csvdiff = 'non_coplanar_twin_hardening_out.csv'
  detail = 'calculate the contribution to twin propagation resistance from non-coplanar systems as a function of only the twin volume fraction on non-coplanar twin systems.'
[]

[upper_twin_fraction_limit]
  type = CSVDiff
  input = 'upper_twin_fraction_limit.i'
  csvdiff = 'upper_twin_fraction_limit_out.csv'
  allow_warnings = true
  detail = 'set the plastic shear increments due to twinning to zero once the total twin volume fraction limit is reached.'
[]

[upper_twin_fraction_limit_error]
  type = RunException
  input = 'upper_twin_fraction_limit.i'
  cli_args = 'Materials/twin_only_xtalpl/print_state_variable_convergence_error_messages=true Materials/twin_only_xtalpl/initial_twin_lattice_friction=3.0 Executioner/dtmin=0.025 Outputs/csv=false'
  expect_err = 'Maximum allowable twin volume fraction limit exceeded with a value of'
  detail = 'prevent the accumulation of a total twin volume fraction above the user-defined limit.'
[]

[strain_increment_upper_limit]
  type = RunException
  input = 'upper_twin_fraction_limit.i'
  cli_args = 'BCs/tdisp/function=5.0e-3*t'
  expect_err = 'Maximum allowable plastic slip increment due to twinning exceeded'
  detail = 'prevent the calculation of a plastic shear increment in excess of the user-defined tolerance value.'
[]

[combined_twinning_slip_111tension]
  type = CSVDiff
  input = 'combined_twinning_slip_111tension.i'
  csvdiff = 'combined_twinning_slip_111tension_out.csv'
  cli_args = 'Outputs/out/type=Checkpoint Outputs/out/execute_on=Final'
  detail = 'compute plastic shear due to both slip and twin propagation when loaded under tension in a 111 orientation.'
[]

[combined_twinning_slip_111compression]
  type = CSVDiff
  input = 'combined_twinning_slip_111tension.i'
  csvdiff = 'combined_twinning_slip_111compression_out.csv'
  cli_args = 'BCs/tdisp/function=-0.02*t Outputs/file_base=combined_twinning_slip_111compression_out '
  detail = 'compute a near-zero twin volume fraction when loaded under compression in a 111 orientation.'
[]

[combined_twinning_slip_100tension]
  type = CSVDiff
  input = 'combined_twinning_slip_100compression.i'
  csvdiff = 'combined_twinning_slip_100tension_out.csv'
  cli_args = 'BCs/tdisp/function=0.025*t Outputs/file_base=combined_twinning_slip_100tension_out'
  detail = 'compute a near-zero volume fraction of twins for all twin system when a 100 oriented crystal is loaded under tension.'
[]

[combined_twinning_slip_100compression]
  type = CSVDiff
  input = 'combined_twinning_slip_100compression.i'
  csvdiff = 'combined_twinning_slip_100compression_out.csv'
  detail = 'compute both dislocation glide and twin propagation in a 100 oriented crystal loaded under compression.'
[]

[only_twinning_fcc_restart]
  type = 'CSVDiff'
  input = 'only_twinning_fcc.i'
  csvdiff = 'only_twinning_fcc_restart_out.csv'
  allow_warnings = true
  cli_args = 'Problem/restart_file_base=only_twinning_fcc_out_cp/LATEST Outputs/file_base=only_twinning_fcc_restart_out'
  detail = 'continue to compute the plastic shear due to twinning after a simulation restart.'
  prereq = 'constiutive_model/only_twinning_fcc'
  method = "!dbg"
[]

[combined_twinning_slip_111tension_restart]
  type = CSVDiff
  input = 'combined_twinning_slip_111tension.i'
  csvdiff = 'combined_twinning_slip_111tension_restart_out.csv'
  cli_args = 'Problem/restart_file_base=combined_twinning_slip_111tension_out_cp/LATEST Outputs/file_base=combined_twinning_slip_111tension_restart_out Executioner/dtmin=0.001'
  detail = 'continue to calculate plastic shear due to both dislocation slip and twinning when loaded under tension in a 111 orientation in a simulation restart.'
  prereq = 'combined_twinning_slip_models/combined_twinning_slip_111tension'
[]

[./test_one_elem]
  type = 'Exodiff'
  input = 'crysp.i'
  exodiff = 'out.e'
  requirement = 'The system shall compute the stress and strain response of a single crystal using the Kalidindi constitutive equation for hardening as a function of slip rate on each slip system.'
[../]

[./test_substep]
  type = 'Exodiff'
  input = 'crysp_substep.i'
  exodiff = 'crysp_substep_out.e'
  allow_warnings = true
  max_time = 350
  valgrind = HEAVY
  issues = '#5082 #5683'
  requirement = 'The system shall compute the stress and strain response of a single crystal using the Kalidindi constitutive equation for hardening as a function of slip rate on each slip system with the substepping capability that reduces the intermediate time step size to aid with convergence within the crystal plasticity hardening model.'
[../]

[./test_with_linesearch]
  type = 'Exodiff'
  input = 'crysp_linesearch.i'
  exodiff = 'crysp_linesearch_out.e'
  allow_warnings = true
  max_time = 350
  valgrind = HEAVY
  requirement = 'The system shall compute the stress and strain response of a single crystal using the Kalidindi constitutive equation for hardening as a function of slip rate on each slip system with the bisection line search method within the crystal plasticity hardening model to aid with convergence.'
[../]

[./test]
  type = 'Exodiff'
  input = 'crysp.i'
  exodiff = 'out.e'
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./test_fileread]
  type = 'Exodiff'
  input = 'crysp_fileread.i'
  exodiff = 'crysp_fileread_out.e'
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./test_user_object]
  type = 'Exodiff'
  input = 'crysp_user_object.i'
  exodiff = 'crysp_user_object_out.e'
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./test_save_euler]
  type = 'Exodiff'
  input = 'crysp_save_euler.i'
  exodiff = 'crysp_save_euler_out.e'
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./test_read_slip_prop]
  type = 'Exodiff'
  input = 'crysp_read_slip_prop.i'
  exodiff = 'crysp_read_slip_prop_out.e'
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./test_cutback]
  type = 'Exodiff'
  input = 'crysp_cutback.i'
  exodiff = 'crysp_cutback_out.e'
  allow_warnings = true
  max_parallel = 1
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./test_substep]
  type = 'Exodiff'
  input = 'crysp_substep.i'
  exodiff = 'crysp_substep_out.e'
  allow_warnings = true
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./test_linesearch]
  type = 'Exodiff'
  input = 'crysp_linesearch.i'
  exodiff = 'crysp_lsearch_out.e'
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[./orthotropic_rotation]
  type = 'CSVDiff'
  input = 'orthotropic_rotation_Cijkl.i'
  csvdiff = 'orthotropic_rotation_Cijkl_out.csv'
  requirement = 'This is a deprecated system that has been replaced by the stress update material-based crystal plasticity and should be removed.'
[../]

[patch_recovery]
  type = 'Exodiff'
  input = 'patch_recovery.i'
  exodiff = 'patch_recovery_out.e'
  abs_zero = 1e-8
  mesh_mode = replicated
  requirement = "The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in the stress-update based crystal plasticity implementation"
  design = 'nodal_patch_recovery.md'
  issues = '#18721'
[]

[./patch_recovery]
  type = 'Exodiff'
  input = 'patch_recovery.i'
  exodiff = 'patch_recovery_out.e'
  abs_zero = 1e-8
  mesh_mode = replicated
  requirement = "The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in a crystal plasticity finite strain application."
  design = 'nodal_patch_recovery.md'
  issues = '#18721'
[../]

[nodal_patch_recovery]
  type = Exodiff
  input = 'patch_recovery.i'
  exodiff = 'patch_recovery_out.e'
  issues = '#15748 #12036'
  requirement = 'The SolidMechanics module shall be able to construct nodal variables from material properties that are defined at quadrature points.'
  design = 'nodal_patch_recovery.md'
[]

[./patch_small_strain]
  type = 'Exodiff'
  input = 'patch.i'
  exodiff = 'patch_out.e'
  mesh_mode = replicated
  requirement = "The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in a small strain application."
  design = 'nodal_patch_recovery.md'
  issues = '#11880'
[../]

[./patch_finite_strain]
  type = 'Exodiff'
  input = 'patch_finite_stress.i'
  exodiff = 'patch_finite_stress_out.e'
  mesh_mode = replicated
  requirement = "The Zienkiewicz-Zhu patch shall calculate the stress components at the nodes, with equivalent results in both serial and parallel simulations, in a finite strain application."
  design = 'nodal_patch_recovery.md'
  issues = '#18721'
[../]

[./stress_concentration]
  type = 'Exodiff'
  input = 'stress_concentration.i'
  exodiff = 'stress_concentration_out.e'
  custom_cmp = 'stress_concentration_out.cmp'
  mesh_mode = replicated
  requirement = "In areas of high concentration gradients, the Zienkiewicz-Zhu implementation shall recover the specified material property."
  design = 'nodal_patch_recovery.md'
  issues = '#11880'
[../]

[update_euler_angle_111_orientation]
  type = 'CSVDiff'
  input = 'update_euler_angle.i'
  csvdiff = 'update_euler_angle_111_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=0 Materials/elasticity_tensor/euler_angle_2=54.7 Materials/elasticity_tensor/euler_angle_3=45 Outputs/file_base=update_euler_angle_111_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (111).'
  issues = '#19473'
  design = '/ComputeUpdatedEulerAngle.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[update_euler_angle_112_orientation]
  type = 'CSVDiff'
  input = 'update_euler_angle.i'
  csvdiff = 'update_euler_angle_112_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=90 Materials/elasticity_tensor/euler_angle_2=30 Materials/elasticity_tensor/euler_angle_3=45 Outputs/file_base=update_euler_angle_112_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (112).'
  issues = '#19473'
  design = '/ComputeUpdatedEulerAngle.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[update_euler_angle_123_orientation]
  type = 'CSVDiff'
  input = 'update_euler_angle.i'
  csvdiff = 'update_euler_angle_123_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/euler_angle_1=50 Materials/elasticity_tensor/euler_angle_2=34 Materials/elasticity_tensor/euler_angle_3=65 Outputs/file_base=update_euler_angle_123_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce correct Euler angles during the crystal plastic simulation for single crystal oriented along (123). '
  issues = '#19473'
  design = '/ComputeUpdatedEulerAngle.md /ComputeMultipleCrystalPlasticityStress.md'
[]

[rotation_matrix_update_euler_angle_111_orientation]
  type = 'CSVDiff'
  input = 'rotation_matrix_update_euler_angle_111_orientation.i'
  csvdiff = 'rotation_matrix_update_euler_angle_111_orientation_out.csv'
  requirement = 'The system shall produce the initial Euler angles phi1=0, psi=54.7356103, and phi2=45 when supplied with the associated rotation matrix and shall calculate a relatively higher 2nd Piola Kirchoff stress in agreement with the low Schmid factor for this loading orientation.'
  issues = '#23451'
  design = '/ComputeElasticityTensorCP.md /ComputeUpdatedEulerAngle.md '
[]

[rotation_matrix_update_euler_angle_011_orientation]
  type = 'CSVDiff'
  input = 'rotation_matrix_update_euler_angle_111_orientation.i'
  csvdiff = 'rotation_matrix_update_euler_angle_011_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/rotation_matrix="0.5 0.5   0.707106781 -0.5 -0.5 0.707106781 0.707106781 0.0 0.0" Outputs/file_base=rotation_matrix_update_euler_angle_011_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce the initial Euler angles of phi1=45, psi=90, and phi2=45, which shall quickly update as the crystal rotates, when supplied with the associated rotation matrix. The system shall calculate a relatively low 2nd Piola Kirchoff stress in the z-direction in agreement with the high Schmid factor for this loading orientation'
  issues = '#23451'
  design = '/ComputeElasticityTensorCP.md /ComputeUpdatedEulerAngle.md '
[]

[rotation_matrix_update_euler_angle_112_orientation]
  type = 'CSVDiff'
  input = 'rotation_matrix_update_euler_angle_111_orientation.i'
  csvdiff = 'rotation_matrix_update_euler_angle_112_orientation_out.csv'
  cli_args = 'Materials/elasticity_tensor/rotation_matrix="-0.612372436 0.707106781 0.353553391 -0.612372436 -0.707106781 0.353553391 0.5 0.0 0.866025404" Outputs/file_base=rotation_matrix_update_euler_angle_112_orientation_out'
  allow_warnings = true
  requirement = 'The system shall produce the initial Euler angles of phi1=90, psi=30, and phi2=35, when supplied with the associated rotation matrix, and the updated Euler angles values as the crystal under goes rotation during deformation.'
  issues = '#23451'
  design = '/ComputeElasticityTensorCP.md /ComputeUpdatedEulerAngle.md '
[]

[./test]
  type = 'Exodiff'
  input = 'test.i'
  exodiff = 'test_out.e'
  issues = '#6097'
  requirement = 'The system shall provide a plug-in based extensible crystal plasticity system'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./user_object_011orientation]
  type = 'CSVDiff'
  input = 'user_object_011orientation.i'
  csvdiff = 'user_object_011orientation_out.csv'
  issues = '#16064'
  requirement = 'The material-based crystal plasticity model shall compute the lagrangian stress, PK2 stress, and slip for an orientation not aligned with the Cartesian coordinate system.'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./exception]
  type = 'Exodiff'
  input = 'exception.i'
  exodiff = 'exception_out.e'
  allow_warnings = true
  issues = '#10133'
  requirement = 'A constitutive failure shall trigger an exception leading to a cut time step rather than a failed solve'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./fileread]
  type = 'Exodiff'
  input = 'fileread.i'
  exodiff = 'fileread_out.e'
  issues = '#6097'
  requirement = 'The crystal plasticity system shall provide a function to read slip system parameters from files'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./user_object]
  type = 'Exodiff'
  input = 'user_object.i'
  exodiff = 'user_object_out.e'
  issues = '#6097'
  requirement = 'The crystal plasticity system shall use pluggable user objects to dtermine the plasticity state variable evolution'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./save_euler]
  type = 'Exodiff'
  input = 'save_euler.i'
  exodiff = 'save_euler_out.e'
  issues = '#6097'
  requirement = 'The crystal plasticity system shall make local Euler angles at material points available for output'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./substep]
  type = 'Exodiff'
  input = 'substep.i'
  exodiff = 'substep_out.e'
  allow_warnings = true
  issues = '#6097'
  requirement = 'The crystal plasticity system shall provide a substepping capability for improved convergence'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./linesearch]
  type = 'Exodiff'
  input = 'linesearch.i'
  exodiff = 'linesearch_out.e'
  issues = '#6097'
  requirement = 'The crystal plasticity system shall implement a line search capability for accellerated internal Newton solves'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./use_substep_dt]
  type = 'CSVDiff'
  input = 'use_substep_dt.i'
  csvdiff = 'use_substep_dt_out.csv'
  allow_warnings = true
  valgrind = HEAVY
  issues = '#17340'
  requirement = 'The system shall apply correct boundary condition after timestep being cut during substepping'
  design = '/FiniteStrainUObasedCP.md'
[../]

[./user_object_Voce_BCC]
  type = 'Exodiff'
  input = 'user_object_Voce_BCC.i'
  exodiff = 'user_object_Voce_BCC_out.e'
  issues = '#11307'
  requirement = 'The crystal plasticity system shall provide a plugin user object implementing the Voce hardening law'
  design = '/CrystalPlasticityStateVarRateComponentVoce.md'
[../]

[./prop_block_read]
  type = 'Exodiff'
  input = 'prop_block_read.i'
  exodiff = 'prop_block_read_out.e'
  issues = '#4066'
  requirement = 'The system shall provide an object to read values from a file and map them onto a mesh besed on mesh block IDs'
  design = 'PropertyReadFile.md'
  allow_warnings = true # number of blocks is smaller than number of data points in CSV file
[../]

[./test_elem]
  type = 'Exodiff'
  input = 'prop_elem_read.i'
  exodiff = 'prop_elem_read_out.e'
  design = 'PropertyReadFile.md'
  requirement = 'The system shall provide an object to read values from a file and map them onto a mesh based on mesh element IDs'
  allow_warnings = true # CSV file has more rows than number of elements
[../]

[./test_grain]
  type = 'Exodiff'
  input = 'prop_grain_read.i'
  exodiff = 'prop_grain_read_out.e'
  design = 'PropertyReadFile.md'
  requirement = 'The system shall provide an object to read values from a file and map them onto a mesh based on grain IDs determined by a random Voronoi tessellation'
  allow_warnings = true # CSV has more rows than number of grains
[../]

[./test_jthermal]
  type = 'Exodiff'
  input = 'j_integral_2d.i'
  exodiff = 'j_integral_2d_out.e'
  custom_cmp = 'j_integral_2d.cmp'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D.'
  issues = '#3807 #10232'
[../]

[./c_integral_2d]
  type = 'Exodiff'
  input = 'c_integral_2d.i'
  exodiff = 'c_integral_2d_out.e'
  custom_cmp = 'c_integral_2d.cmp'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the C integral for problems in 2D.'
  issues = '#3807 #10232'
[../]

[./test_iithermal]
  type = 'CSVDiff'
  input = 'interaction_integral_2d.i'
  csvdiff = 'interaction_integral_2d_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the interaction integral for problems in 2D.'
  issues = '#7527 #9966'
[../]

[./test_iithermal_generic]
  type = 'CSVDiff'
  input = 'interaction_integral_2d_thermal_generic.i'
  csvdiff = 'interaction_integral_2d_thermal_generic_out.csv'
  requirement = 'The domain integral action shall compute the stress intensity factor using the interaction integral approach for a problem dominated by thermal strains using an approach that integrates eigenstrain gradients in a general manner.'
  issues = '#26452'
[../]

[./test_ii_arb_eig_grad]
  type = 'CSVDiff'
  input = 'interaction_integral_2d_eig_grad.i'
  csvdiff = 'interaction_integral_2d_eig_grad_out.csv'
  requirement = 'The interaction integral shall account for the contributions of the gradients of arbitrary eigenstrains in 2D'
  allow_test_objects = true
  issues = '#18804'
[../]

[./test_ii_arb_eig_grad_err_jint]
  prereq = test_ii_arb_eig_grad
  type = 'RunException'
  input = 'interaction_integral_2d_eig_grad.i'
  cli_args = "DomainIntegral/integrals='JIntegral InteractionIntegralKI'"
  expect_err = "'eigenstrain_gradient' cannot be specified when the computed integrals include JIntegral, CIntegral, or KFromJIntegral"
  requirement = 'The DomainIntegralAction shall generate an error if a user specifies the eigenstrain gradient and also request the J integral'
  allow_test_objects = true
  issues = '#18804'
[../]

[./test_ii_arb_eig_grad_err_temp]
  prereq = test_ii_arb_eig_grad_err_jint
  type = 'RunException'
  input = 'interaction_integral_2d_eig_grad.i'
  cli_args = "DomainIntegral/temperature=temp DomainIntegral/eigenstrain_names=thermal_expansion"
  expect_err = "'eigenstrain_gradient' cannot be specified together with 'temperature' or 'eigenstrain_names'. These are for separate, mutually exclusive systems for including the effect of eigenstrains"
  requirement = 'The DomainIntegralAction shall generate an error if a user specifies the temperature and also provides the eigenstrain_gradient'
  allow_test_objects = true
  issues = '#18804'
[../]

[./test_ii_bf]
  type = 'CSVDiff'
  input = 'interaction_integral_2d_bf.i'
  csvdiff = 'interaction_integral_2d_bf_out.csv'
  requirement = 'The interaction integral shall account for the contributions of body forces in 2D'
  issues = '#18804'
[../]

[./test_ii_bf_err_jint]
  prereq = test_ii_bf
  type = 'RunException'
  input = 'interaction_integral_2d_bf.i'
  cli_args = "DomainIntegral/integrals='JIntegral InteractionIntegralKI'"
  expect_err = "'body_force' cannot be specified when the computed integrals include JIntegral, CIntegral, or KFromJIntegral"
  requirement = 'The DomainIntegralAction shall generate an error if a user specifies the body force and also request the J integral'
  issues = '#18804'
[../]

[./test_iithermal_rot]
  type = 'CSVDiff'
  input = 'interaction_integral_2d_rot.i'
  csvdiff = 'interaction_integral_2d_rot_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane for 2D.'
  issues = '#7527 #9966'
[../]

[./interaction_integral_2d_c]
  type = 'Exodiff'
  input = 'interaction_integral_2d_c.i'
  exodiff = 'interaction_integral_2d_c_out.e'
  custom_cmp = 'interaction_integral_2d_c.cmp'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the C(t) integral for problems in 2D.'
  issues = '#7527 #9966'
[../]

[./test_jthermal_ctefunc]
  type = 'CSVDiff'
  input = 'j_integral_2d_ctefunc.i'
  csvdiff = 'j_integral_2d_ctefunc_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the instantaneous thermal expansion function eigenstrain.'
  issues = '#3807 #10232'
[../]

[./test_jthermal_mean_ctefunc]
  type = 'CSVDiff'
  input = 'j_integral_2d_mean_ctefunc.i'
  csvdiff = 'j_integral_2d_mean_ctefunc_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the mean thermal expansion function eigenstrain.'
  issues = '#3807 #10232'
[../]

[./test_jthermal_inst_ctefunc]
  type = 'CSVDiff'
  input = 'j_integral_2d_inst_ctefunc.i'
  csvdiff = 'j_integral_2d_inst_ctefunc_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the instantaneous thermal expansion function eigenstrain.'
  issues = '#3807 #10232'
[../]

[./ii_2d]
  type = 'CSVDiff'
  input = 'interaction_integral_2d.i'
  csvdiff = 'interaction_integral_2d_out.csv'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 2D.'
[../]

[./ii_2d_rot]
  type = 'CSVDiff'
  input = 'interaction_integral_2d_rot.i'
  csvdiff = 'interaction_integral_2d_rot_out.csv'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems for all planes in 2D.'
[../]

[./ii_3d_as_2d]
  type = 'CSVDiff'
  input = 'interaction_integral_3d_as_2d.i'
  csvdiff = 'interaction_integral_3d_as_2d_out.csv'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3d evaluated as 2D.'
[../]

[./ii_3d]
  type = 'CSVDiff'
  input = 'interaction_integral_3d.i'
  csvdiff = 'interaction_integral_3d_out.csv interaction_integral_3d_out_II_KI_1_0001.csv interaction_integral_3d_out_II_KI_2_0001.csv interaction_integral_3d_out_II_KII_1_0001.csv interaction_integral_3d_out_II_KII_2_0001.csv interaction_integral_3d_out_II_KIII_1_0001.csv interaction_integral_3d_out_II_KIII_2_0001.csv'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  abs_zero = 1e-8
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D.'
[../]

[./ii_3d_noq]
  type = 'CSVDiff'
  input = 'interaction_integral_3d.i'
  cli_args = 'Outputs/file_base=interaction_integral_3d_noq_out'
  csvdiff = 'interaction_integral_3d_noq_out.csv interaction_integral_3d_noq_out_II_KI_1_0001.csv interaction_integral_3d_noq_out_II_KI_2_0001.csv interaction_integral_3d_noq_out_II_KII_1_0001.csv interaction_integral_3d_noq_out_II_KII_2_0001.csv interaction_integral_3d_noq_out_II_KIII_1_0001.csv interaction_integral_3d_noq_out_II_KIII_2_0001.csv'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  abs_zero = 1e-8
  prereq = ii_3d
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D while supressing the output of q function values.'
[../]

[./ii_3d_points]
  type = 'CSVDiff'
  input = 'interaction_integral_3d_points.i'
  csvdiff = 'interaction_integral_3d_points_out.csv interaction_integral_3d_points_out_II_KI_1_0001.csv interaction_integral_3d_points_out_II_KI_2_0001.csv interaction_integral_3d_points_out_II_KII_1_0001.csv interaction_integral_3d_points_out_II_KII_2_0001.csv interaction_integral_3d_points_out_II_KIII_1_0001.csv interaction_integral_3d_points_out_II_KIII_2_0001.csv'
  abs_zero = 1e-8
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D at specified points.'
[../]

[./ii_3d_rot]
  type = 'CSVDiff'
  input = 'interaction_integral_3d_rot.i'
  csvdiff = 'interaction_integral_3d_rot_out.csv interaction_integral_3d_rot_out_II_KI_1_0001.csv interaction_integral_3d_rot_out_II_KI_2_0001.csv interaction_integral_3d_rot_out_II_KII_1_0001.csv interaction_integral_3d_rot_out_II_KII_2_0001.csv interaction_integral_3d_rot_out_II_KIII_1_0001.csv interaction_integral_3d_rot_out_II_KIII_2_0001.csv'
  abs_zero = 2e-8
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane in 3D.'
[../]

[./ii_2d_chk_q]
  type = 'Exodiff'
  input = 'interaction_integral_2d.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'interaction_integral_2d_out.e'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  prereq = 'ii_2d'
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 2D while outputting q vlaues.'
[../]

[./ii_2d_rot_chk_q]
  type = 'Exodiff'
  input = 'interaction_integral_2d_rot.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'interaction_integral_2d_rot_out.e'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  prereq = 'ii_2d_rot'
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane 2D while outputting q values.'
[../]

[./ii_3d_as_2d_chk_q]
  type = 'Exodiff'
  input = 'interaction_integral_3d_as_2d.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'interaction_integral_3d_as_2d_out.e'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  prereq = 'ii_3d_as_2d'
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D evaluated as 2D.'
[../]

[./ii_3d_chk_q]
  type = 'Exodiff'
  input = 'interaction_integral_3d.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'interaction_integral_3d_out.e'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  prereq = 'ii_3d_noq'
  abs_zero = 1e-8
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D while outputting q values.'
[../]

[./ii_3d_points_chk_q]
  type = 'Exodiff'
  input = 'interaction_integral_3d_points.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'interaction_integral_3d_points_out.e'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  prereq = 'ii_3d_points'
  abs_zero = 1e-8
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in 3D for specified points, while outputting q values.'
[../]

[./ii_3d_rot_chk_q]
  type = 'Exodiff'
  input = 'interaction_integral_3d_rot.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'interaction_integral_3d_rot_out.e'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  prereq = 'ii_3d_rot'
  abs_zero = 2e-8
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the interaction integral for problems in any plane in 3D while outputting q values.'
[../]

[./test]
  type = 'CSVDiff'
  input = 'input.i'
  csvdiff = '360degree_model_out.csv'
  max_parallel = 1 # nl_its and lin_its will not be the same in parallel and serial
  heavy = true
  issues = '#3705'
  design = 'syntax/DomainIntegral/index.md'
  requirement = 'The system shall compute mixed-mode fracture integrals that match values of K fields applied at the boundary of a 3D disk cut on one side by a slit'
[../]

[j_2d]
  type = 'CSVDiff'
  input = 'j_integral_2d.i'
  csvdiff = 'j_integral_2d_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D.'
[]

[j_2d_block_restrict]
  type = 'CSVDiff'
  issues = '#24795'
  input = 'j_integral_2d_block_restrict.i'
  csvdiff = 'j_integral_2d_block_restrict_out.csv'
  requirement = 'The domain integral action shall compute the fracture domain integrals including the J integral for problems in which the fracture domains of interest represent a subset of all the domains in the system.'
[]

[j_2d_block_restrict_error]
  type = 'RunException'
  issues = '#24795'
  input = 'j_integral_2d_block_restrict.i'
  cli_args = "DomainIntegral/block='1 2'"
  expect_err = "'EshelbyTensor' is not defined on block lowerd_dummy."
  requirement = 'The domain integral action shall error out if the blocks selected do not have the adequate material objects.'
[]

[j_2d_output_vpp]
  type = 'CheckFiles'
  issues = '#25162'
  input = 'j_integral_2d.i'
  check_files = 'j_integral_2d_output_vpp_out.csv'
  check_not_exists = 'j_integral_2d_output_vpp_out_*VPP*.csv'
  cli_args = "DomainIntegral/output_vpp=false Outputs/file_base=j_integral_2d_output_vpp_out"
  requirement = 'The domain integral action shall suppress the vector postprocessor output and stop generating a csv file for each integration ring at each time step.'
[]

[j_2d_output_pp]
  type = 'CSVDiff'
  issues = '#25162'
  input = 'j_integral_2d.i'
  csvdiff = 'j_integral_2d_output_pp_out.csv'
  cli_args = "DomainIntegral/output_vpp=false Outputs/file_base=j_integral_2d_output_pp_out"
  requirement = 'The domain integral action shall suppress the vector postprocessor output while the postprocessor outputs are not affected.'
[]

[j_2d_small_strain]
  type = 'CSVDiff'
  input = 'j_integral_2d_small_strain.i'
  csvdiff = 'j_integral_2d_small_strain_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using small strain.'
[]

[j_2d_points]
  type = 'CSVDiff'
  input = 'j_integral_2d_points.i'
  csvdiff = 'j_integral_2d_points_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D at specified points.'
[]

[j_2d_mouth_dir]
  type = 'CSVDiff'
  input = 'j_integral_2d_mouth_dir.i'
  csvdiff = 'j_integral_2d_mouth_dir_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D given a mouth direction.'
[]

[j_2d_topo_q]
  type = 'CSVDiff'
  input = 'j_integral_2d_topo_q_func.i'
  csvdiff = 'j_integral_2d_topo_q_func_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D using the topology type q function.'
[]

[j_3d_as_2d]
  type = 'CSVDiff'
  input = 'j_integral_3d_as_2d.i'
  csvdiff = 'j_integral_3d_as_2d_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D evaluated as a 2D problem.'
[]

[j_3d_as_2d_topo_q]
  type = 'CSVDiff'
  input = 'j_integral_3d_as_2d_topo_q_func.i'
  csvdiff = 'j_integral_3d_as_2d_topo_q_func_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D evaluated as a 2D problem using the topology type q function.'
[]

[j_3d]
  type = 'CSVDiff'
  input = 'j_integral_3d.i'
  csvdiff = 'j_integral_3d_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D.'
[]

[j_3d_noq]
  type = 'CSVDiff'
  input = 'j_integral_3d.i'
  csvdiff = 'j_integral_3d_out.csv'
  prereq = j_3d
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with the q function turned off.'
[]

[j_3d_points]
  type = 'CSVDiff'
  input = 'j_integral_3d_points.i'
  csvdiff = 'j_integral_3d_points_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with specified points.'
[]

[j_3d_mouth_dir]
  type = 'CSVDiff'
  input = 'j_integral_3d_mouth_dir.i'
  csvdiff = 'j_integral_3d_mouth_dir_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D given a crack mouth direction.'
[]

[j_3d_mouth_dir_end_dir_vec]
  type = 'CSVDiff'
  input = 'j_integral_3d_mouth_dir_end_dir_vec.i'
  csvdiff = 'j_integral_3d_mouth_dir_end_dir_vec_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D given a crack mouth direction and end direction vector.'
[]

[j_3d_topo_q]
  type = 'CSVDiff'
  input = 'j_integral_3d_topo_q_func.i'
  csvdiff = 'j_integral_3d_topo_q_func_out.csv'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with a topology type q function.'
[]

[j_3d_as_2d_topo_q_outq]
  type = 'CSVDiff'
  input = 'j_integral_3d_as_2d_topo_q_func.i'
  csvdiff = 'j_integral_3d_as_2d_topo_q_func_out.csv'
  prereq = j_3d_as_2d_topo_q
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D evaluated as a 2D problem using the topology type q function.'
[]

[j_3d_mouth_dir_outq]
  type = 'CSVDiff'
  input = 'j_integral_3d_mouth_dir.i'
  csvdiff = 'j_integral_3d_mouth_dir_out.csv'
  prereq = j_3d_mouth_dir
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D given a crack mouth direction.'
[]

[j_2d_noq]
  type = 'CSVDiff'
  input = 'j_integral_2d.i'
  csvdiff = 'j_integral_2d_out.csv'
  prereq = 'j_2d'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D while supressing the output of the q function values.'
[]

[j_2d_chk_q]
  type = 'Exodiff'
  input = 'j_integral_2d.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'j_integral_2d_out.e'
  prereq = 'j_2d_noq'
  rel_err = 1e-5
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D while outputting the q function values.'
[]

[j_2d_topo_chk_q]
  type = 'Exodiff'
  input = 'j_integral_2d_topo_q_func.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'j_integral_2d_topo_q_func_out.e'
  prereq = 'j_2d_topo_q'
  rel_err = 1e-5
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 2D with the topology type q function and outputting the values.'
[]

[j_3d_chk_q]
  type = 'Exodiff'
  input = 'j_integral_3d.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'j_integral_3d_out.e'
  prereq = 'j_3d_noq'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D while supressing the output of the q values.'
[]

[j_3d_topo_chk_q]
  type = 'Exodiff'
  input = 'j_integral_3d_topo_q_func.i'
  cli_args = 'DomainIntegral/output_q=true'
  exodiff = 'j_integral_3d_topo_q_func_out.e'
  prereq = 'j_3d_topo_q'
  requirement = 'The domain integral action shall compute all of the fracture domain integrals including the J integral for problems in 3D with the topology type q function and outputting the values.'
[]

[j_ellip]
  type = 'CSVDiff'
  input = 'j_int_surfbreak_ellip_crack_sym_mm.i'
  csvdiff = 'j_int_surfbreak_ellip_crack_sym_mm_out_J_1_0001.csv j_int_surfbreak_ellip_crack_sym_mm_out_J_2_0001.csv j_int_surfbreak_ellip_crack_sym_mm_out_J_3_0001.csv'
  max_parallel = 1
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks.'
[]

[J_ellip_cm]
  type = 'CSVDiff'
  input = 'j_int_surfbreak_ellip_crack_sym_mm_cm.i'
  csvdiff = 'j_int_surfbreak_ellip_crack_sym_mm_cm_out_J_1_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cm_out_J_2_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cm_out_J_3_0001.csv'
  max_parallel = 1
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks using the crack mouth specification.'
[]

[J_ellip_cm_ad]
  type = 'CSVDiff'
  input = 'j_int_surfbreak_ellip_crack_sym_mm_cm_ad.i'
  csvdiff = 'j_int_surfbreak_ellip_crack_sym_mm_cm_ad_out_J_1_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cm_ad_out_J_2_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cm_ad_out_J_3_0001.csv'
  max_parallel = 1
  valgrind = 'none'
  method = 'opt'
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks using the crack mouth specification computing the system Jacobian via automatic differentiation.'
[]

[j_ellip_cfp]
  type = 'CSVDiff'
  input = 'j_int_surfbreak_ellip_crack_sym_mm_cfp.i'
  csvdiff = 'j_int_surfbreak_ellip_crack_sym_mm_cfp_out_J_1_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cfp_out_J_2_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cfp_out_J_3_0001.csv'
  max_parallel = 1
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks with crack face pressure.'
[]

[J_ellip_cm_cfp]
  type = 'CSVDiff'
  input = 'j_int_surfbreak_ellip_crack_sym_mm_cfp_cm.i'
  csvdiff = 'j_int_surfbreak_ellip_crack_sym_mm_cfp_cm_out_J_1_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cfp_cm_out_J_2_0001.csv j_int_surfbreak_ellip_crack_sym_mm_cfp_cm_out_J_3_0001.csv'
  max_parallel = 1
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the J integral for surface breaking elliptical cracks with crack face pressure and crack mouth boundary specified.'
[]

[c_int_surfbreak_ellip_crack_sym_mm]
  design = 'syntax/DomainIntegral/index.md'
  type = 'CSVDiff'
  input = 'c_int_surfbreak_ellip_crack_sym_mm.i'
  csvdiff = 'c_int_surfbreak_ellip_crack_sym_mm_out_C_1_0002.csv c_int_surfbreak_ellip_crack_sym_mm_out_C_2_0002.csv c_int_surfbreak_ellip_crack_sym_mm_out_C_3_0002.csv'
  max_parallel = 1
  heavy = true
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the C integral for surface breaking elliptical cracks.'
[]

[c_int_surfbreak_ellip_crack_sym_mm_ad]
  design = 'syntax/DomainIntegral/index.md'
  type = 'CSVDiff'
  input = 'c_int_surfbreak_ellip_crack_sym_mm_ad.i'
  csvdiff = 'c_int_surfbreak_ellip_crack_sym_mm_ad_out_C_1_0002.csv c_int_surfbreak_ellip_crack_sym_mm_ad_out_C_2_0002.csv c_int_surfbreak_ellip_crack_sym_mm_ad_out_C_3_0002.csv'
  max_parallel = 1
  heavy = true
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the C integral for surface breaking elliptical cracks using automatic differentiation.'
  rel_err = 1.0e-4
[]

[j_int_fgm_sif]
  type = 'CSVDiff'
  issues = '#23313'
  input = 'j_int_fgm_sif.i'
  csvdiff = 'j_int_fgm_sif_out.csv'
  cli_args = 'DomainIntegral/functionally_graded_youngs_modulus_crack_dir_gradient=elastic_mod_material_der_mat'
  requirement = 'The Domain Integral Action shall compute stress intensity factors from the interaction integral for a crack perpendicular to a bi-material interface, treating the interface as a functionally-graded material.'
[]

[j_int_fgm_sif_error]
  type = 'RunException'
  input = 'j_int_fgm_sif.i'
  expect_err = 'You have selected to compute the interaction integral for a crack in FGM'
  requirement = "The Domain Integral shall error out if the user input does not consistently define the required material properties to consider extra interaction integral terms for functionally graded materials."
[]

[fgm_5]
  issues = '#23313'
  type = 'CSVDiff'
  input = 'fgm_5.i'
  csvdiff = 'fgm_5_out.csv'
  requirement = 'The Domain Integral Action shall compute stress intensity factors from the interaction integral, with an added term stemming for spatially varying properties, that accounts for the crack perpendicularity to the property grading and yield verified results.'
[]

[axisymmetric_solution_tran]
  issues = '#23631'
  type = 'CSVDiff'
  input = 'axisymmetric_solution_tran.i'
  csvdiff = 'axisymmetric_solution_tran_out.csv'
  requirement = 'The Domain Integral Action shall compute verified stress intensity factors from the interaction integral for axisymmetric geometries and circumferential cracks.'
[]

[t_stress_crack_infinite_plate_2d]
  type = 'CSVDiff'
  input = 't_stress_crack_infinite_plate_2d.i'
  csvdiff = 't_stress_crack_infinite_plate_out.csv'
  rel_err = 2e-5
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the T stress for cracks in an infinite plate.'
[]

[t_stress_ellip_crack_3d]
  type = 'CSVDiff'
  input = 't_stress_ellip_crack_3d.i'
  csvdiff = 't_stress_ellip_crack_out.csv t_stress_ellip_crack_out_II_KI_1_0001.csv t_stress_ellip_crack_out_II_KI_2_0001.csv t_stress_ellip_crack_out_II_KI_3_0001.csv t_stress_ellip_crack_out_II_T_1_0001.csv t_stress_ellip_crack_out_II_T_2_0001.csv t_stress_ellip_crack_out_II_T_3_0001.csv t_stress_ellip_crack_out_J_1_0001.csv t_stress_ellip_crack_out_J_2_0001.csv t_stress_ellip_crack_out_J_3_0001.csv'
  rel_err = 2e-5
  valgrind = 'heavy'
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the T stress for an elliptical crack in 3D.'
[]

[ad_t_stress_ellip_crack_3d]
  type = 'CSVDiff'
  input = 'ad_t_stress_ellip_crack_3d.i'
  csvdiff = 'ad_t_stress_ellip_crack_out.csv ad_t_stress_ellip_crack_out_II_KI_1_0001.csv ad_t_stress_ellip_crack_out_II_KI_2_0001.csv ad_t_stress_ellip_crack_out_II_KI_3_0001.csv ad_t_stress_ellip_crack_out_II_T_1_0001.csv ad_t_stress_ellip_crack_out_II_T_2_0001.csv ad_t_stress_ellip_crack_out_II_T_3_0001.csv ad_t_stress_ellip_crack_out_J_1_0001.csv ad_t_stress_ellip_crack_out_J_2_0001.csv ad_t_stress_ellip_crack_out_J_3_0001.csv'
  rel_err = 2e-5
  valgrind = 'heavy'
  requirement = 'The Domain Integral Action shall compute all of the fracture domain integrals including the T stress for an elliptical crack in 3D using automatic differentiation objects.'
  method = '!dbg'
[]

[./acceleration_bc]
  type = 'Exodiff'
  input = 'AccelerationBC_test.i'
  exodiff = 'AccelerationBC_test_out.e'
  abs_zero = 1e-08
  compiler = 'GCC CLANG'

  requirement = "The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary."
  design = "Dynamics.md PresetAcceleration.md"
  issues = "#7642"
[../]

[./acceleration_bc_ti]
  type = 'Exodiff'
  input = 'AccelerationBC_test.i'
  exodiff = 'AccelerationBC_test_out.e'
  abs_zero = 1e-08
  compiler = 'GCC CLANG'

  requirement = "The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary when the Newmark-Beta time integrator is used to calculate the velocity and acceleration."
  design = "Dynamics.md PresetAcceleration.md"
  issues = "#12185"
  prereq = "acceleration_bc"
[../]

[./displacement_bc]
  type = 'Exodiff'
  input = '3D_QStatic_1_Ramped_Displacement.i'
  exodiff = '3D_QStatic_1_Ramped_Displacement_out.e'
  custom_cmp = 'displacement.cmp'
  use_old_floor = true
  compiler = 'GCC CLANG'

  requirement = "The PresetDisplacement class shall accurately prescribe the displacement at the given boundary."
  design = "Dynamics.md PresetDisplacement.md"
  issues = "#7642"
[../]

[./displacement_bc_ti]
  type = 'Exodiff'
  input = '3D_QStatic_1_Ramped_Displacement_ti.i'
  exodiff = '3D_QStatic_1_Ramped_Displacement_out.e'
  custom_cmp = 'displacement.cmp'
  use_old_floor = true
  compiler = 'GCC CLANG'

  requirement = "The PresetDisplacement class shall accurately prescribe the displacement at the given boundary using the velocity and and acceleration computed using the Newmark-Beta time integrator."
  design = "Dynamics.md PresetDisplacement.md"
  issues = "#12185"
  prereq = "displacement_bc"
[../]

[./displacement_bc_gravity]
  type = 'Exodiff'
  input = '3D_QStatic_1_Ramped_Displacement_with_gravity.i'
  exodiff = '3D_QStatic_1_Ramped_Displacement_with_gravity_out.e'
  custom_cmp = 'displacement.cmp'
  use_old_floor = true
  compiler = 'GCC CLANG'

  requirement = "The mechanics system shall accurately conduct a static analysis in a small number of time steps to equilibrate the system under gravity before starting the dynamic analysis."
  design = "Dynamics.md"
  issues = "#7642"
[../]

[./hht]
  type = 'Exodiff'
  input = 'rayleigh_hht.i'
  exodiff = 'rayleigh_hht_out.e'
  abs_zero = 1e-09
  compiler = 'GCC CLANG'

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration."
  design = "Dynamics.md"
  issues = "#5559"
[../]

[./hht_ti]
  type = 'Exodiff'
  input = 'rayleigh_hht_ti.i'
  exodiff = 'rayleigh_hht_out.e'
  abs_zero = 1e-09
  compiler = 'GCC CLANG'

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when using the velocity and acceleration computed using the Newmark-Beta time integrator."
  design = "Dynamics.md"
  issues = "#12185"
  prereq = "hht"
[../]

[./newmark]
  type = 'Exodiff'
  input = 'rayleigh_newmark.i'
  exodiff = 'rayleigh_newmark_out.e'
  abs_zero = 1e-09
  compiler = 'GCC CLANG'

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system with a constant Rayleigh damping."
  design = "Dynamics.md"
  issues = "#5559"
[../]

[./newmark_material]
  type = 'Exodiff'
  input = 'rayleigh_newmark_material_dependent.i'
  exodiff = 'rayleigh_newmark_out.e'
  abs_zero = 1e-09
  compiler = 'GCC CLANG'
  prereq = 'newmark'

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system with Rayleigh damping provided as a material property."
  design = "Dynamics.md"
  issues = "#5559"
[../]

[hht]
  type = 'Exodiff'
  input = 'hht_test.i'
  exodiff = 'hht_test_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system using Hilber-Hughes-Taylor (HHT) time integration."
  design = "Dynamics.md"
  issues = "#5559"
[]

[hht_action]
  type = 'Exodiff'
  input = 'hht_test_action.i'
  exodiff = 'hht_test_action_out.e'
  abs_zero = 1e-09
  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system using Hilber-Hughes-Taylor (HHT) time integration when using the dynamic tensor mechanics action."
  design = "Dynamics.md"
  issues = "#18388"
[]

[newmark]
  type = 'Exodiff'
  input = 'newmark.i'
  exodiff = 'newmark_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system using Newmark time integration."
  design = "Dynamics.md"
  issues = "#5559"
[]

[newmark_action]
  type = 'Exodiff'
  input = 'newmark_action.i'
  exodiff = 'newmark_action_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system using Newmark time integration and the dynamic tensor mechanics action."
  design = "Dynamics.md"
  issues = "#18388"
[]

[hht_ti]
  type = 'Exodiff'
  input = 'hht_test_ti.i'
  exodiff = 'hht_test_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall accurately predict the dynamic response of a linear elastic system using Hilber-Hughes-Taylor (HHT) time integration when velocity and acceleration of the system are calculated using the Newmark-Beta time integrator."
  design = "Dynamics.md"
  issues = "#12185"
[]

[ad_newmark_action]
  type = 'Exodiff'
  input = 'newmark_action.i'
  exodiff = 'newmark_action_out.e'
  abs_zero = 1e-09

  cli_args = 'Physics/SolidMechanics/Dynamic/all/use_automatic_differentiation=true Materials/Elasticity_tensor/type=ADComputeElasticityTensor Materials/stress/type=ADComputeLinearElasticStress Executioner/solve_type=NEWTON'
  requirement = "The dynamic tensor mechanics action shall support automatic differentiation using the Newmark-Beta time integrator."
  design = "Dynamics.md"
  issues = "#18687"
[]

[hht]
  type = 'Exodiff'
  input = 'wave_hht.i'
  exodiff = 'wave_hht_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration."
[]

[newmark]
  type = 'Exodiff'
  input = 'wave_newmark.i'
  exodiff = 'wave_newmark_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with no numerical or structural damping."
[]

[rayleigh_hht]
  type = 'Exodiff'
  input = 'wave_rayleigh_hht.i'
  exodiff = 'wave_rayleigh_hht_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration."
[]

[rayleigh_hht_ad]
  type = 'Exodiff'
  input = 'wave_rayleigh_hht_AD.i'
  exodiff = 'wave_rayleigh_hht_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when automatic differentiation is used."
  prereq = "rayleigh_hht"
[]

[rayleigh_hht_ad_jac]
  type = 'PetscJacobianTester'
  input = 'wave_rayleigh_hht_AD.i'

  requirement = "The mechanics system shall correctly compute the Jacobian for 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when automatic differentiation is used."
[]

[rayleigh_hht_ti]
  type = 'Exodiff'
  input = 'wave_rayleigh_hht_ti.i'
  exodiff = 'wave_rayleigh_hht_out.e'
  abs_zero = 1e-09

  allow_warnings = True
  requirement = "The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with both Rayleigh damping and numerical damping resulting from Hilber-Hughes-Taylor (HHT) time integration when using the velocity and acceleration computed using the Newmark-Beta time integrator."
  issues = "#12185"
  prereq = "rayleigh_hht_ad"
[]

[rayleigh_newmark]
  type = 'Exodiff'
  input = 'wave_rayleigh_newmark.i'
  exodiff = 'wave_rayleigh_newmark_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with Rayleigh damping."
[]

[rayleigh_newmark_action]
  type = 'Exodiff'
  input = 'wave_rayleigh_newmark_action.i'
  exodiff = 'wave_rayleigh_newmark_action_out.e'
  abs_zero = 1e-09

  requirement = "The mechanics system shall correctly predict 1D wave propagation in a linear elastic material with Rayleigh damping when using the dynamic tensor mechanics parent action."
[]

[./acceleration_bc]
  type = 'Exodiff'
  input = 'AccelerationBC_test.i'
  exodiff = 'AccelerationBC_test_out.e'
  abs_zero = 1e-08
  compiler = 'GCC CLANG'

  requirement = "The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary."
  design = "Dynamics.md PresetAcceleration.md"
  issues = "#7642"
[../]

[./acceleration_bc_ti]
  type = 'Exodiff'
  input = 'AccelerationBC_test.i'
  exodiff = 'AccelerationBC_test_out.e'
  abs_zero = 1e-08
  compiler = 'GCC CLANG'

  requirement = "The PresetAcceleration class shall accurately prescribe the acceleration at the given boundary when the Newmark-Beta time integrator is used to calculate the velocity and acceleration."
  design = "Dynamics.md PresetAcceleration.md"
  issues = "#12185"
  prereq = "acceleration_bc"
[../]

[./linear_nodal_constraint]
  type = 'Exodiff'
  input = 'disp_mid.i'
  exodiff = 'disp_mid_out.e'
  abs_zero = 1e-09
  compiler = 'GCC CLANG'

  requirement = "The LinearNodalConstraint class shall constrain the secondary nodes to move as a linear combination of the primary nodes."
  design = "LinearNodalConstraint.md"
  issues = "#5783"
[../]

[./displacement_bc]
  type = 'Exodiff'
  input = '3D_QStatic_1_Ramped_Displacement.i'
  exodiff = '3D_QStatic_1_Ramped_Displacement_out.e'
  custom_cmp = 'displacement.cmp'
  use_old_floor = true
  compiler = 'GCC CLANG'

  requirement = "The PresetDisplacement class shall accurately prescribe the displacement at the given boundary."
  design = "Dynamics.md PresetDisplacement.md"
  issues = "#7642"
[../]

[./displacement_bc_ti]
  type = 'Exodiff'
  input = '3D_QStatic_1_Ramped_Displacement_ti.i'
  exodiff = '3D_QStatic_1_Ramped_Displacement_out.e'
  custom_cmp = 'displacement.cmp'
  use_old_floor = true
  compiler = 'GCC CLANG'

  requirement = "The PresetDisplacement class shall accurately prescribe the displacement at the given boundary using the velocity and and acceleration computed using the Newmark-Beta time integrator."
  design = "Dynamics.md PresetDisplacement.md"
  issues = "#12185"
  prereq = "displacement_bc"
[../]

[direct_central_difference]
  type = 'Exodiff'
  input = 'direct_central_difference.i'
  exodiff = 'direct_central_difference_out.e'
  abs_zero = 1e-09
  requirement = "The solid mechanics app shall support a form of central difference time integration
                   that uses a direct calculation of the acceleration from the residual forces to
                   perform a solution update."
  design = "DirectCentralDifference.md"
  issues = "#27833"
[]

[direct_central_difference_varied_dt]
  type = 'Exodiff'
  input = 'direct_central_difference_varied_dt.i'
  exodiff = 'direct_central_difference_varied_dt_out.e'
  abs_zero = 1e-09
  requirement = "The solid mechanics app shall support a form of central difference time integration
                   that uses a direct calculation of the acceleration from the residual forces to
                   perform a solution update. The direct central difference method should properly use
                   a time step averaging method to handle non-constant time steps."
  design = "DirectCentralDifference.md"
  issues = "#27833"
[]

[direct_central_difference_multiVarBC]
  type = 'Exodiff'
  input = 'direct_central_difference_multiVarBC.i'
  exodiff = 'direct_central_difference_multiVarBC_out.e'
  abs_zero = 1e-09
  requirement = "The solid mechanics app shall support dirichlet boundary conditions for direct central
                   difference time integration that correctly enforce constant and function boundary
                   conditions"
  design = "DirectCentralDifference.md"
  issues = "#27833"
[]

[./composite]
  type = 'Exodiff'
  input = 'composite.i'
  exodiff = 'composite_out.e'
  issues = '#5850'
  design = 'CompositeElasticityTensor.md'
  requirement = 'The system shall provide a method for assembling an elasticity tensor from multiple tensor contributions weighted by material properties.'
[../]

[./rotation_matrix_one_rotation]
  type = 'Exodiff'
  input = 'rotation_matrix_1_rotation.i'
  exodiff = 'rotation_matrix_1_rotation_out.e'
  issues = '#16340'
  design = 'ComputeElasticityTensor.md'
  requirement = 'The system shall provide a method for rotating a tensor using a rotation matrix.'
[../]

[./rotation_matrix_two_rotations]
  type = 'Exodiff'
  input = 'rotation_matrix_2_rotations.i'
  exodiff = 'rotation_matrix_2_rotations_out.e'
  issues = '#16340'
  design = 'ComputeElasticityTensor.md'
  requirement = 'The system shall provide a method for rotating a tensor using a rotation matrix requiring more than one rotation.'
[../]

[./axisymmetric_rz]
  type = Exodiff
  input = '2D-axisymmetric_rz_test.i'
  exodiff = '2D-axisymmetric_rz_test_out.e'
  requirement = 'The ComputeElasticityTensor class shall correctly compute the elasticity tensor for an isotropic axisymmetric problem.'
  design = 'ComputeElasticityTensor.md'
[../]

[fake_plastic]
  type = 'Exodiff'
  input = 'finite_strain_fake_plastic.i'
  exodiff = 'finite_strain_fake_plastic_out.e'
  issues = '#9212 #7555'
  design = 'source/materials/ComputeMultiPlasticityStress.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the QuasiStatic SolidMechanics Physics.'
[]

[fake_plastic_Bbar]
  type = 'Exodiff'
  input = 'finite_strain_fake_plastic.i'
  exodiff = 'finite_strain_fake_plastic_out.e'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'fake_plastic'
  issues = '#9212 #8235'
  design = 'source/materials/ComputeMultiPlasticityStress.md solid_mechanics/VolumetricLocking.md'
  requirement = 'The ComputeMultiPlasticityStress class shall, when supplied with no plastic models, reduce to and produce the solely elastic stress solution for a finite strain fomulation, using the volumetric locking correction b-bar formulation.'
[]

[./rotation_test]
  type = 'Exodiff'
  input = 'elastic_rotation.i'
  exodiff = 'elastic_rotation_out.e'
  exodiff_opts = '-F 1e-8'
  requirement = 'The system shall track a changing global stress state when a model undergoes rigid body rotation'
  issues = '#8422'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./patch_test]
  type = 'Exodiff'
  input = 'finite_strain_patch.i'
  exodiff = 'finite_strain_patch_out.e'
  scale_refine = 1
  max_parallel = 1
  requirement = 'The system shall compute a uniform stress state given a uniform strain state with finite strains'
  issues = '#12584'
[../]

[free_expansion_abs_ref]
  type = 'Exodiff'
  input = 'free_expansion_abs_ref.i'
  exodiff = 'free_expansion_abs_ref_out.e'
  requirement = 'The tensor mechanics action shall set up the mechanics kernels with the appropriate options to accumulate absolute values of the residual to a tag vector usable for relative convergence checks.'
  design = 'Physics/SolidMechanics/QuasiStatic/index.md ReferenceResidualProblem.md'
[]

[./test]
  type = 'Exodiff'
  input = 'global_strain.i'
  exodiff = 'global_strain_out.e'
  requirement = "The globalstrain system shall correctly compute the volume change
                   due to applied stress while still maintaining periodicity in 2D."
[../]

[./uniaxial]
  type = 'Exodiff'
  input = 'global_strain_uniaxial.i'
  exodiff = 'global_strain_uniaxial_out.e'
  custom_cmp = 'global_strain_uniaxial_out.cmp'
  requirement = "The globalstrain system shall correctly compute the volume change
                   under uniaxial stress while still maintaining periodicity
                   in all the directions in 3D."
[../]

[./hydrostat]
  type = 'Exodiff'
  input = 'global_strain_hydrostat.i'
  exodiff = 'global_strain_hydrostat_out.e'
  requirement = "The globalstrain system shall correctly compute the volume change
                   under hydrostratic stress while still maintaining periodicity
                   in all the directions in 3D."
[../]

[./shear]
  type = 'Exodiff'
  input = 'global_strain_shear.i'
  exodiff = 'global_strain_shear_out.e'
  requirement = "The globalstrain system shall correctly compute the shear
                   deformation due to applied stress while still maintaining
                   periodicity in all the directions in 3D."
[../]

[./direction]
  type = 'Exodiff'
  input = 'global_strain_direction.i'
  exodiff = 'global_strain_direction_out.e'
  requirement = "The globalstrain system shall correctly compute the deformation
                   behavior in 2D with applied displacement boundary condition in
                   one direction while still maintaining periodicity in the other."
[../]

[./disp]
  type = 'Exodiff'
  input = 'global_strain_disp.i'
  exodiff = 'global_strain_disp_out.e'
  abs_zero = 1e-9
  requirement = "The globalstrain system shall correctly compute the deformation
                   behavior in 3D with applied displacement boundary condition in
                   one direction while still maintaining periodicity in the others."
[../]

[./pressure_3D]
  type = 'Exodiff'
  input = 'global_strain_pressure_3D.i'
  exodiff = 'global_strain_pressure_3D_out.e'
  requirement = "The globalstrain system shall correctly compute the deformation behavior
                   in 3D with pressure boundary condition in one direction while
                   still maintaining periodicity in the others."
[../]

[./action_check]
  type = 'Exodiff'
  input = 'global_strain_action.i'
  exodiff = 'global_strain_action_out.e'
  abs_zero = 1e-9
  requirement = "The 'GlobalStrainAction' should set all the objects reqiured
                   for the globalstrain system to correctly compute the deformation
                   behavior maintaining strain periodicity."
[../]

[gravity_test]
  type = Exodiff
  input = 'gravity_test.i'
  exodiff = 'gravity_test_out.e'
  requirement = 'The tensor mechanics module shall have the capability of applying a body force term in the stress divergence equilibrium equation that accounts for the force of gravity on a solid object due to its own weight.'
  design = 'Gravity.md'
  issues = '#4781'
[]

[ad_gravity_test]
  type = Exodiff
  input = 'ad_gravity_test.i'
  exodiff = 'ad_gravity_test_out.e'
  requirement = 'The tensor mechanics module shall be able to reproduce gravity test results of the hand-coded jacobian using automatic differentiation.'
  design = 'ADGravity.md'
  issues = '#13100'
[]

[ad_gravity_test-jac]
  type = PetscJacobianTester
  input = 'ad_gravity_test.i'
  run_sim = 'True'
  ratio_tol = 1e-7
  difference_tol = 1e-4
  requirement = 'The Jacobian for the AD gravity problem shall be perfect'
  issues = '#13100'
  design = 'ADGravity.md'
  cli_args = "Outputs/active=''"
[]

[material_vector_body_force]
  type = Exodiff
  input = 'material_vector_body_force.i'
  exodiff = 'material_vector_body_force_out.e'
  requirement = 'The system shall provide a way to apply a vector valued body force density to a volume'
  issues = '#13100'
  design = 'MaterialVectorBodyForce.md'
[]

[block-gravity-kinetic-energy]
  issues = '#19671'
  design = 'KineticEnergyAux.md'
  type = CSVDiff
  csvdiff = 'block-gravity-kinetic-energy_out.csv'
  input = 'block-gravity-kinetic-energy.i'
  requirement = 'The system shall provide a way to compute the system total kinetic energy through the use of auxiliary kernels and postprocessors. This test verifies that a body falls at the right acceleration under the action of gravity and that the computed kinetic energy matches the analytical expression.'
[]

[./longFiber]
  type = 'Exodiff'
  input = 'anisoLongFiber.i'
  exodiff = 'anisoLongFiber_out.e'
  requirement = 'The system shall compute homogenized elastic constants using the asymptotic expansion homogenization approach and match values for the so-called long fiber problem'
[../]

[./shortFiber]
  type = 'Exodiff'
  input = 'anisoShortFiber.i'
  exodiff = 'anisoShortFiber_out.e'
  custom_cmp = 'anisoShortFiber.exodiff'
  compiler = 'GCC CLANG'
  requirement = 'The system shall compute homogenized elastic constants using the asymptotic expansion homogenization approach and match values for the so-called short fiber problem'
[../]

[./test]
  type = 'CSVDiff'
  input = 'volume_weighted_weibull.i'
  csvdiff = 'volume_weighted_weibull_initial_histo_0000.csv'
  requirement = 'VolumeWeightedWeibull shall generate a randomly distributed field that approximates the analytic expression for the Weibull distribution when the mesh is uniform and the reference volume is set equal to the element size'
[../]

[./test_finer]
  prereq = test
  type = 'CSVDiff'
  input = 'volume_weighted_weibull.i'
  cli_args = 'Mesh/nx=200 Mesh/ny=200 Outputs/initial/file_base=volume_weighted_weibull_finer_initial ICs/u_vww/reference_volume=0.000025'
  csvdiff = 'volume_weighted_weibull_finer_initial_histo_0000.csv'
  requirement = 'VolumeWeightedWeibull shall generate a randomly distributed field that approaches the analytic expression for the Weibull distribution when the mesh is uniform and the reference volume is set equal to the element size as the mesh density is increased'
[../]

[./test_ref_vol]
  prereq = test_finer
  type = 'CSVDiff'
  input = 'volume_weighted_weibull.i'
  # Setting the median to 1/(V_ref/V_el)^(1/weibull_modulus) should give the same result as the baseline case
  #The ratio V_ref/V_el is 2 in this case, so the median should be 1/(2^(1/15)), or 0.9548416039
  cli_args = 'ICs/u_vww/median=0.9548416039 ICs/u_vww/reference_volume=0.0002'
  csvdiff = 'volume_weighted_weibull_initial_histo_0000.csv'
  requirement = 'VolumeWeightedWeibull shall generate a randomly distributed field that approximates the analytic expression for the Weibull distribution when the mesh is uniform, the reference volume is set to a value different from the element size, and the median is adjusted to account for the different reference volume'
[../]

[./2D]
  type = Exodiff
  input = 'inclined_bc_2d.i'
  exodiff = 'inclined_bc_2d_out.e'
  superlu = true
  issues = '#13128'
  design = 'PenaltyInclinedNoDisplacementBC.md InclinedNoDisplacementBCAction.md'
  requirement = 'The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 2D model using a penalty method.'
[../]

[./3D]
  type = Exodiff
  input = 'inclined_bc_3d.i'
  exodiff = 'inclined_bc_3d_out.e'
  superlu = true
  issues = '#13128'
  design = 'PenaltyInclinedNoDisplacementBC.md InclinedNoDisplacementBCAction.md'
  requirement = 'The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 3D model using a penalty method.'
[../]

[ad]
  type = Exodiff
  input = 'ad_inclined_bc_3d.i'
  exodiff = 'ad_inclined_bc_3d_out.e'
  superlu = true
  issues = '#24910'
  design = 'PenaltyInclinedNoDisplacementBC.md InclinedNoDisplacementBCAction.md'
  requirement = 'The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions while using automatic differentiation.'
[]

[./2D]
  type = Exodiff
  input = 'inclined_bc_2d.i'
  exodiff = 'inclined_bc_2d_out.e'
  superlu = true
  issues = '#13128'
  design = 'PenaltyInclinedNoDisplacementBC.md InclinedNoDisplacementBCAction.md'
  requirement = 'The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 2D model using a penalty method.'
[../]

[./3D]
  type = Exodiff
  input = 'inclined_bc_3d.i'
  exodiff = 'inclined_bc_3d_out.e'
  superlu = true
  issues = '#13128'
  design = 'PenaltyInclinedNoDisplacementBC.md InclinedNoDisplacementBCAction.md'
  requirement = 'The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions on a 3D model using a penalty method.'
[../]

[ad]
  type = Exodiff
  input = 'ad_inclined_bc_3d.i'
  exodiff = 'ad_inclined_bc_3d_out.e'
  superlu = true
  issues = '#24910'
  design = 'PenaltyInclinedNoDisplacementBC.md InclinedNoDisplacementBCAction.md'
  requirement = 'The SolidMechanics module shall have the capabilty to enforce inclined boundary conditions while using automatic differentiation.'
[]

[./residual]
  type = 'CSVDiff'
  input = 'residual.i'
  csvdiff = 'residual_out.csv'
  design = 'InertialTorque.md'
  requirement = 'The tensor mechanics module computes residual for a simplesituation correctly'

  issues = '#13634'
[../]

[./simple]
  type = 'CSVDiff'
  input = 'simple.i'
  csvdiff = 'simple_out.csv'
  design = 'InertialTorque.md'
  requirement = 'The tensor mechanics module computes the ith component ofinertial torque where the only degree of freedom in y'

  issues = '#13634'
[../]

[./except01]
  type = 'RunException'
  input = 'except01.i'
  expect_err = 'ComputeEigenstrainFromInitialStress: 9 initial stress functions must be provided.  You supplied 3'
  design = 'ComputeEigenstrainFromInitialStress.md'
  issues = "#9749"
  requirement = "SolidMechanics shall allow users to specify initial stresses, but shall error-out with appropriate message if the user does not supply the correct number of functions to define the initial stress tensor"
[../]

[./except02]
  type = 'RunException'
  input = 'except02.i'
  expect_err = 'ComputeEigenstrainFromInitialStress: If you supply initial_stress_aux, 9 values must be given.  You supplied 3'
  design = 'ComputeEigenstrainFromInitialStress.md'
  issues = "#13087"
  requirement = "SolidMechanics shall allow users to specify initial stresses, but shall error-out with appropriate message if the user does not supply the correct number of AuxVariables to define the initial stress tensor"
[../]

[./gravity]
  type = 'Exodiff'
  input = 'gravity.i'
  exodiff = 'gravity.e'
  design = 'ComputeEigenstrainFromInitialStress.md'
  issues = "#9749"
  requirement = "SolidMechanics shall allow users to specify initial stresses using Functions"
[../]

[./gravity_with_aux]
  type = 'Exodiff'
  input = 'gravity_with_aux.i'
  exodiff = 'gravity_with_aux.e'
  design = 'ComputeEigenstrainFromInitialStress.md'
  issues = "#13087"
  requirement = "SolidMechanics shall allow users to specify initial stresses using AuxVariables"
[../]

[./gravity_cosserat]
  type = 'Exodiff'
  input = 'gravity_cosserat.i'
  exodiff = 'gravity_cosserat.e'
  design = 'ComputeEigenstrainFromInitialStress.md'
  issues = "#9749"
  requirement = "SolidMechanics shall allow users to specify initial stresses for problems with Cosserat mechanics"
[../]

[./mc_tensile]
  type = 'CSVDiff'
  input = 'mc_tensile.i'
  csvdiff = 'mc_tensile.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-5
  cli_args = '--no-trap-fpe'
  design = 'ComputeEigenstrainFromInitialStress.md'
  issues = "#9749"
  requirement = "SolidMechanics shall allow users to specify initial stresses for problems with plasticity, and if the initial stresses are inadmissible, the return-map algorithm will be applied, perhaps incrementally, to bring the initial stresses back to the admissible region"
[../]

[damper_exodus]
  type = 'Exodiff'
  input = 'cube_load.i'
  exodiff = 'cube_load_out.e'
  requirement = "The module shall be able to apply a damper on the displaced mesh to limit the element Jacobian change over nonlinear iterations."
[]

[damper_verify]
  type = 'RunApp'
  input = 'cube_load.i'
  expect_out = '9 Nonlinear'
  prereq = 'damper_exodus'
  requirement = "The element Jacobian damper shall be able to apply a partial nonlinear update."
[]

[ref_damper]
  type = 'Exodiff'
  input = 'cube_load_undisplaced.i'
  exodiff = 'cube_load_undisplaced_out.e'
  requirement = "The module shall be able to apply a damper on the undisplaced mesh to limit the element Jacobian change over nonlinear iterations."
[]

[ref_damper_block_restricted]
  type = 'Exodiff'
  input = 'block_restriction.i'
  exodiff = 'block_restriction_out.e'
  requirement = "The module shall be able to apply a damper on certain blocks of the undisplaced mesh to limit the element Jacobian change over nonlinear iterations."
[]

[damper_exodus]
  type = 'Exodiff'
  input = 'cube_load.i'
  exodiff = 'cube_load_out.e'
  requirement = "The module shall be able to apply a damper on the displaced mesh to limit the element Jacobian change over nonlinear iterations."
[]

[damper_verify]
  type = 'RunApp'
  input = 'cube_load.i'
  expect_out = '9 Nonlinear'
  prereq = 'damper_exodus'
  requirement = "The element Jacobian damper shall be able to apply a partial nonlinear update."
[]

[ref_damper]
  type = 'Exodiff'
  input = 'cube_load_undisplaced.i'
  exodiff = 'cube_load_undisplaced_out.e'
  requirement = "The module shall be able to apply a damper on the undisplaced mesh to limit the element Jacobian change over nonlinear iterations."
[]

[ref_damper_block_restricted]
  type = 'Exodiff'
  input = 'block_restriction.i'
  exodiff = 'block_restriction_out.e'
  requirement = "The module shall be able to apply a damper on certain blocks of the undisplaced mesh to limit the element Jacobian change over nonlinear iterations."
[]

[./without_correction]
  issues = '#20281'
  type = RunApp
  input = 'simple_test.i'
  design = 'source/actions/TensorMechanicsAction.md'
  requirement = "Can run second order problem without stabilization"
  cli_args = "Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false"
[../]

[./with_correction]
  issues = '#20281'
  type = RunException
  input = 'simple_test.i'
  design = 'source/actions/TensorMechanicsAction.md'
  requirement = "Cannot run second order problem with stabilization"
  cli_args = "Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true"
  expect_err = "Volumetric locking correction should not be used for higher-order elements."
[../]

[./homogenization_block_restriction]
  issues = '#21716'
  type = RunApp
  input = 'homogenization_block.i'
  design = 'source/actions/TensorMechanicsAction.md'
  requirement = "Homogenization system can be block restricted"
[../]

[action_small_unstabilized]
  type = Exodiff
  input = 'action.i'
  exodiff = 'small_unstabilized.e'
  abs_zero = 1e-6
  requirement = "Action produces identical results for small deformations/without stabilization in axisymmetric RZ coordinates"
  cli_args = "Outputs/file_base=small_unstabilized Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false Materials/compute_stress/large_kinematics=false"
[]

[action_small_stabilized]
  type = Exodiff
  input = 'action.i'
  exodiff = 'small_stabilized.e'
  abs_zero = 1e-6
  requirement = "Action produces identical results for small deformations/with stabilization in axisymmetric RZ coordinates"
  cli_args = "Outputs/file_base=small_stabilized Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true Materials/compute_stress/large_kinematics=false"
[]

[action_large_unstabilized]
  type = Exodiff
  input = 'action.i'
  exodiff = 'large_unstabilized.e'
  abs_zero = 1e-6
  requirement = "Action produces identical results for large deformations/without stabilization in axisymmetric RZ coordinates"
  cli_args = "Outputs/file_base=large_unstabilized Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false Materials/compute_stress/large_kinematics=true"
[]

[action_large_stabilized]
  type = Exodiff
  input = 'action.i'
  exodiff = 'large_stabilized.e'
  abs_zero = 1e-6
  requirement = "Action produces identical results for large deformations/with stabilization in axisymmetric RZ coordinates"
  cli_args = "Outputs/file_base=large_stabilized Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true Materials/compute_stress/large_kinematics=true"
[]

[./action_large_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_large_stab.e'
  requirement = "Action produces identical results for large deformations/with stabilization"
  abs_zero = 1e-6
  cli_args = "Outputs/out/file_base=L_large_stab Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Physics/SolidMechanics/QuasiStatic/all/formulation=TOTAL Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true Materials/compute_stress/large_kinematics=true"
  design = 'source/actions/TensorMechanicsAction.md'
  heavy = true
[../]

[./action_large_no_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_large_nostab.e'
  requirement = "Action produces identical results for large deformations/no stabilization"
  abs_zero = 1e-6
  cli_args = "Outputs/out/file_base=L_large_nostab Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Physics/SolidMechanics/QuasiStatic/all/formulation=TOTAL Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false Materials/compute_stress/large_kinematics=true"
  design = 'source/actions/TensorMechanicsAction.md'
  heavy = true
[../]

[./action_small_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_small_stab.e'
  requirement = "Action produces identical results for small deformations/with stabilization"
  abs_zero = 1e-6
  cli_args = "Outputs/out/file_base=L_small_stab Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/formulation=TOTAL Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true"
  design = 'source/actions/TensorMechanicsAction.md'
[../]

[./action_small_no_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_small_nostab.e'
  requirement = "Action produces identical results for small deformations/no stabilization"
  abs_zero = 1e-4
  cli_args = "Outputs/out/file_base=L_small_nostab Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/formulation=TOTAL Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false"
  design = 'source/actions/TensorMechanicsAction.md'
[../]

[./action_1D]
  type = Exodiff
  input = 'action_1D.i'
  exodiff = 'action_1D_out.e'
  requirement = "Action produces identical results for 1D Cartesian problem"
  abs_zero = 1e-6
  design = 'source/actions/TensorMechanicsAction.md'
[../]

[compare_3d]
  type = Exodiff
  input = 'action_3d.i'
  exodiff = '3d.e'
  requirement = "Action produces identical results for a 3D, large deformation problem with mixed constraints compared to a case where the components are specified manually."
  abs_zero = 1e-6
[]

[compare_2d]
  type = Exodiff
  input = 'action_2d.i'
  exodiff = '2d.e'
  requirement = "Action produces identical results for a 2D, small deformation problem with mixed constraints compared to a case where the components are specific manually."
  abs_zero = 1e-6
[]

[./action_large_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_large_stab.e'
  requirement = "Action produces identical results for large deformations/with stabilization"
  abs_zero = 1e-6
  heavy = true
  cli_args = "Outputs/out/file_base=L_large_stab Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Physics/SolidMechanics/QuasiStatic/all/formulation=UPDATED Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true Materials/compute_stress/large_kinematics=true"
[../]

[./action_large_no_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_large_nostab.e'
  requirement = "Action produces identical results for large deformations/no stabilization"
  abs_zero = 1e-6
  heavy = true
  cli_args = "Outputs/out/file_base=L_large_nostab Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Physics/SolidMechanics/QuasiStatic/all/formulation=UPDATED Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false Materials/compute_stress/large_kinematics=true"
[../]

[./action_small_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_small_stab.e'
  requirement = "Action produces identical results for small deformations/with stabilization"
  abs_zero = 1e-6
  cli_args = "Outputs/out/file_base=L_small_stab Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/formulation=UPDATED Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=true"
[../]

[./action_small_no_stab]
  type = Exodiff
  input = 'action_L.i'
  exodiff = 'L_small_nostab.e'
  requirement = "Action produces identical results for small deformations/no stabilization"
  abs_zero = 1e-4
  cli_args = "Outputs/out/file_base=L_small_nostab Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/formulation=UPDATED Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false"
[../]

[action_small_unstabilized]
  type = Exodiff
  input = 'action.i'
  exodiff = 'small_unstabilized.e'
  abs_zero = 1e-6
  requirement = "Action produces identical results for small deformations/without stabilization in axisymmetric RZ coordinates"
  cli_args = "Outputs/file_base=small_unstabilized Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false Materials/compute_stress/large_kinematics=false"
[]

[action_large_unstabilized]
  type = Exodiff
  input = 'action.i'
  exodiff = 'large_unstabilized.e'
  abs_zero = 1e-6
  requirement = "Action produces identical results for large deformations/without stabilization in axisymmetric RZ coordinates"
  cli_args = "Outputs/file_base=large_unstabilized Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Physics/SolidMechanics/QuasiStatic/all/volumetric_locking_correction=false Materials/compute_stress/large_kinematics=true"
[]

[dirichlet_small_unstabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates'
[]

[dirichlet_small_stabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates'
[]

[dirichlet_large_unstabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates'
[]

[dirichlet_large_stabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs in 2D axisymmetric RZ coordinates'
[]

[neumann_small_unstabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates'
[]

[neumann_small_stabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates'
[]

[neumann_large_unstabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates'
[]

[neumann_large_stabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neumann BCs in 2D axisymmetric RZ coordinates'
[]

[jacobian_small_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms'
[]

[jacobian_large_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms'
[]

[jacobian_small_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms'
[]

[jacobian_large_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms'
[]

[jacobian_small_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms'
[]

[jacobian_large_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms'
[]

[jacobian_small_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms'
[]

[jacobian_large_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms'
[]

[jacobian_small_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms'
[]

[jacobian_large_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, no stabilization, including cross-terms'
[]

[jacobian_small_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms'
[]

[jacobian_large_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 2D axisymmetric cylindrical coordinates, with stabilization, including cross-terms'
[]

[small]
  type = Exodiff
  input = 'small.i'
  exodiff = 'small_out.e'
  requirement = "Small strain solution in 1D centrosymmetric spherical coordinates matches analytical solution"
  abs_zero = 1e-6
[]

[dirichlet_small_unstabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates'
[]

[dirichlet_small_stabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates'
[]

[dirichlet_large_unstabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates'
[]

[dirichlet_large_stabilized]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs in 1D centrosymmetric spherical coordinates'
[]

[neumann_small_unstabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates'
[]

[neumann_small_stabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates'
[]

[neumann_large_unstabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates'
[]

[neumann_large_stabilized]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neumann BCs in 1D centrosymmetric spherical coordinates'
[]

[jacobian_small_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms'
[]

[jacobian_large_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, no stabilization, including cross-terms'
[]

[jacobian_small_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for small displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms'
[]

[jacobian_large_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 5e-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 5e-6 for large displacements in 1D centrosymmetric spherical coordinates, with stabilization, including cross-terms'
[]

[./dirichlet_small_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_small_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_large_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_large_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_small_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_small_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs'
[../]

[./dirichlet_large_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_large_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs'
[../]

[./dirichlet_small_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_small_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_large_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_large_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_small_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_small_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs'
[../]

[./dirichlet_large_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_large_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs'
[../]

[./dirichlet_small_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_small_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_large_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_large_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_small_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_small_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs'
[../]

[./dirichlet_large_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_large_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs'
[../]

[./dirichlet]
  type = CSVDiff
  input = 'dirichlet.i'
  csvdiff = 'dirichlet_out.csv'
  requirement = "Quadratic convergence in 1D for DirichletBCs, SMP does better than FDP for this problem."
[../]

[./L-large]
  type = CSVDiff
  input = 'large.i'
  csvdiff = 'large_out.csv'
  requirement = "Quadratic convergence in 3D for PresetBCs on a complicated geometry, SMP matches FDP."
  valgrind = HEAVY
[../]

[./L-small]
  type = CSVDiff
  input = 'small.i'
  csvdiff = 'small_out.csv'
  requirement = "Quadratic convergence in 3D for PresetBCs on a complicated geometry, SMP matches FDP."
  valgrind = HEAVY
[../]

[residual_jacobian_together]
  type = Exodiff
  prereq = large
  input = 'large_patch.i'
  exodiff = 'large_patch_out.e'
  cli_args = 'Executioner/residual_and_jacobian_together=true'
  requirement = "The new system shall produce the correct results if residual and jacobian are computed together."
  abs_zero = 1e-6
[]

[./base_name]
  type = Exodiff
  input = 'patch.i'
  exodiff = 'patch_out.e'
  requirement = "System still functions if you supply a base_name"
  abs_zero = 1e-6
  issues = '#17472'
  design = 'source/kernels/lagrangian/TotalLagrangianStressDivergence.md'
[../]

[./elastic_small_neither]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an elastic material'
[../]

[./elastic_large_neither]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an elastic material'
[../]

[./elastic_small_right]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an elastic material'
[../]

[./elastic_large_right]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an elastic material'
[../]

[./plastic_j2_small_neither]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an plastic_j2 material'
[../]

[./plastic_j2_large_neither]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an plastic_j2 material'
[../]

[./plastic_j2_small_right]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an plastic_j2 material'
[../]

[./plastic_j2_large_right]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an plastic_j2 material'
[../]

[./elastic_small_neither]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an elastic material'
[../]

[./elastic_large_neither]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=true Kernels/sdy/use_displaced_mesh=true Kernels/sdz/use_displaced_mesh=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an elastic material'
[../]

[./elastic_small_right]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an elastic material'
[../]

[./elastic_large_right]
  type = PetscJacobianTester
  input = 'elastic.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=true Kernels/sdy/use_displaced_mesh=true Kernels/sdz/use_displaced_mesh=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an elastic material'
[../]

[./plastic_j2_small_neither]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and an plastic_j2 material'
[../]

[./plastic_j2_large_neither]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=true Kernels/sdy/use_displaced_mesh=true Kernels/sdz/use_displaced_mesh=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and an plastic_j2 material'
[../]

[./plastic_j2_small_right]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and an plastic_j2 material'
[../]

[./plastic_j2_large_right]
  type = PetscJacobianTester
  input = 'plastic_j2.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=true Kernels/sdy/use_displaced_mesh=true Kernels/sdz/use_displaced_mesh=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and an plastic_j2 material'
[../]

[./runs_with_small_strain_model]
  type = RunApp
  input = 'strain_check.i'
  requirement = "The Lagrangian kernels can use a small strain elastic update with a large kinematics formulation"
[../]

[sd-strain_no_stab]
  type = PetscJacobianTester
  input = 'sd-strain.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=false'
  requirement = 'Jacobian is exact with rtol 1e-7 for small deformations, imposed strains, and no stabilization'
[]

[sd-stress_no_stab]
  type = PetscJacobianTester
  input = 'sd-stress.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=false'
  requirement = 'Jacobian is exact with rtol 1e-7 for small deformations, imposed stresses, and no stabilization'
[]

[ld-strain_no_stab]
  type = PetscJacobianTester
  input = 'ld-strain.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=false'
  requirement = 'Jacobian is exact with rtol 1e-7 for large deformations, imposed strains, and no stabilization'
[]

[ld-stress_no_stab]
  type = PetscJacobianTester
  input = 'ld-stress.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=false'
  requirement = 'Jacobian is exact with rtol 1e-7 for large deformations, imposed stresses, and no stabilization'
[]

[sd-strain_right_stab]
  type = PetscJacobianTester
  input = 'sd-strain.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=true'
  requirement = 'Jacobian is exact with rtol 1e-7 for small deformations, imposed strains, and stabilization on'
[]

[sd-stress_right_stab]
  type = PetscJacobianTester
  input = 'sd-stress.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=true'
  requirement = 'Jacobian is exact with rtol 1e-7 for small deformations, imposed stresses, and stabilization on'
[]

[ld-strain_right_stab]
  type = PetscJacobianTester
  input = 'ld-strain.i'
  ratio_tol = 1E-6 # For some reason this one is 1.01e-7...
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=true'
  requirement = 'Jacobian is exact with rtol 1e-6 for large deformations, imposed strains, and stabilization on'
[]

[ld-stress_right_stab]
  type = PetscJacobianTester
  input = 'ld-stress.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = 'GlobalParams/stabilize_strain=true'
  requirement = 'Jacobian is exact with rtol 1e-7 for large deformations, imposed stresses, and stabilization on'
[]

[1d-strain]
  type = CSVDiff
  input = '1d.i'
  csvdiff = '1d-strain_out.csv'
  cli_args = "Outputs/file_base=1d-strain_out constraint_types='strain none none none none none none none none' targets=func_strain"
  requirement = "Homogenized strain field hits the targets in 1D using large kinematics"
[]

[1d-stress]
  type = CSVDiff
  input = '1d.i'
  csvdiff = '1d-stress_out.csv'
  cli_args = "Outputs/file_base=1d-stress_out constraint_types='stress none none none none none none none none' targets=func_stress"
  requirement = "Homogenized stress field hits the targets in 1D using large kinematics"
[]

[2d-strain]
  type = CSVDiff
  input = '2d.i'
  csvdiff = '2d-strain_out.csv'
  cli_args = "Outputs/file_base=2d-strain_out constraint_types='strain strain none strain strain none none none none' targets='strain11 strain21 strain12 strain22'"
  requirement = "Homogenization with strain constraints hits the targets in 2D using large kinematics"
[]

[2d-stress]
  type = CSVDiff
  input = '2d.i'
  csvdiff = '2d-stress_out.csv'
  cli_args = "Outputs/file_base=2d-stress_out constraint_types='stress stress none strain stress none none none none' targets='stress11 stress21 0 stress22'"
  requirement = "Homogenization with stress constraints hits the targets in 2D using large kinematics"
[]

[3d-strain]
  type = CSVDiff
  input = '3d.i'
  csvdiff = '3d-strain_out.csv'
  cli_args = "Outputs/file_base=3d-strain_out constraint_types='strain strain strain strain strain strain strain strain strain' targets='strain11 strain21 strain31 strain12 strain22 strain32 strain13 strain23 strain33'"
  requirement = "Homogenization with strain constraints hits the targets in 3D using large kinematics"
[]

[3d-stress]
  type = CSVDiff
  input = '3d.i'
  csvdiff = '3d-stress_out.csv'
  cli_args = "Outputs/file_base=3d-stress_out constraint_types='stress strain strain stress stress strain stress stress stress' targets='stress11 0 0 stress12 stress22 0 stress13 stress23 stress33'"
  requirement = "Homogenization with stress constraints hits the targets in 3D using large kinematics"
[]

[1d-strain]
  type = CSVDiff
  input = '1d.i'
  csvdiff = '1d-strain_out.csv'
  cli_args = "Outputs/file_base=1d-strain_out constraint_types='strain none none none none none none none none' targets=func_strain"
  requirement = "Homogenized strain field hits the targets in 1D"
[]

[1d-stress]
  type = CSVDiff
  input = '1d.i'
  csvdiff = '1d-stress_out.csv'
  cli_args = "Outputs/file_base=1d-stress_out constraint_types='stress none none none none none none none none' targets=func_stress"
  requirement = "Homogenized stress field hits the targets in 1D"
[]

[2d-strain]
  type = CSVDiff
  input = '2d.i'
  csvdiff = '2d-strain_out.csv'
  cli_args = "Outputs/file_base=2d-strain_out constraint_types='strain none none strain strain none none none none' targets='strain11 strain12 strain22'"
  requirement = "Homogenization with strain constraints hits the targets in 2D"
[]

[2d-stress]
  type = CSVDiff
  input = '2d.i'
  csvdiff = '2d-stress_out.csv'
  cli_args = "Outputs/file_base=2d-stress_out constraint_types='stress none none stress stress none none none none' targets='stress11 stress12 stress22'"
  requirement = "Homogenization with stress constraints hits the targets in 2D"
[]

[2d-mixed]
  type = CSVDiff
  input = '2d.i'
  csvdiff = '2d-mixed_out.csv'
  cli_args = "Outputs/file_base=2d-mixed_out constraint_types='stress none none stress strain none none none none' targets='stress11 stress12 strain22'"
  requirement = "Homogenization with mixed stress and strain constraints hits the targets in 2D"
[]

[3d-strain]
  type = CSVDiff
  input = '3d.i'
  csvdiff = '3d-strain_out.csv'
  cli_args = "Outputs/file_base=3d-strain_out constraint_types='strain none none strain strain none strain strain strain' targets='strain11 strain12 strain22 strain13 strain23 strain33'"
  requirement = "Homogenization with strain constraints hits the targets in 3D"
[]

[3d-stress]
  type = CSVDiff
  input = '3d.i'
  csvdiff = '3d-stress_out.csv'
  cli_args = "Outputs/file_base=3d-stress_out constraint_types='stress none none stress stress none stress stress stress' targets='stress11 stress12 stress22 stress13 stress23 stress33'"
  requirement = "Homogenization with stress constraints hits the targets in 3D"
[]

[3d-mixed]
  type = CSVDiff
  input = '3d.i'
  csvdiff = '3d-mixed_out.csv'
  cli_args = "Outputs/file_base=3d-mixed_out constraint_types='stress none none strain strain none stress stress stress' targets='stress11 strain12 strain22 stress13 stress23 stress33'"
  requirement = "Homogenization with mixed stress and strain constraints hits the targets in 3D"
[]

[2d-strainS]
  type = CSVDiff
  input = '2dscalar.i'
  csvdiff = '2d-strain_out.csv'
  cli_args = "Outputs/file_base=2d-strain_out constraint_types='strain none none strain strain none none none none' targets='strain11 strain12 strain22'"
  requirement = "Homogenization from scalar wrapper class with strain constraints hits the targets in 2D"
  allow_test_objects = true
[]

[2d-stressS]
  type = CSVDiff
  input = '2dscalar.i'
  csvdiff = '2d-stress_out.csv'
  cli_args = "Outputs/file_base=2d-stress_out constraint_types='stress none none stress stress none none none none' targets='stress11 stress12 stress22'"
  requirement = "Homogenization from scalar wrapper class with stress constraints hits the targets in 2D"
  allow_test_objects = true
[]

[2d-mixedS]
  type = CSVDiff
  input = '2dscalar.i'
  csvdiff = '2d-mixed_out.csv'
  cli_args = "Outputs/file_base=2d-mixed_out constraint_types='stress none none stress strain none none none none' targets='stress11 stress12 strain22'"
  requirement = "Homogenization from scalar wrapper class with mixed stress and strain constraints hits the targets in 2D"
  allow_test_objects = true
[]

[2d-stressA]
  type = CSVDiff
  input = '2dsole.i'
  csvdiff = '2dsole_out.csv'
  cli_args = "constraint_types='stress none none stress stress none none none none' targets='stress11 stress12 stress22'"
  requirement = "Framework scalar kernel wrapper correctly assembles scalar-to-scalar coupling Jacobian"
  allow_test_objects = true
[]

[2d-stressR]
  type = CSVDiff
  input = '2drow.i'
  csvdiff = '2drow_out.csv'
  cli_args = "constraint_types='stress none none stress stress none none none none' targets='stress11 stress12 stress22'"
  requirement = "Framework scalar kernel wrapper correctly assembles Jacobian by rows"
  allow_test_objects = true
[]

[2D]
  type = CSVDiff
  input = 'pull_2D.i'
  csvdiff = 'pull_2D_out.csv'
  abs_zero = 1E-6
  rel_err = 1e-6
  issues = '#21757'
  design = 'source/kernels/lagrangian/TotalLagrangianWeakPlaneStress.md'
  requirement = '2D generalized plane strain solution shall match the 3D results in the limit of infinite thickness.'
[]

[jacobian_small_unstabilized]
  type = PetscJacobianTester
  input = 'convergence.i'
  ratio_tol = 1E-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for small displacements without stabilization.'
[]

[jacobian_small_stabilized]
  type = PetscJacobianTester
  input = 'convergence.i'
  ratio_tol = 1E-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for small displacements with stabilization.'
[]

[jacobian_large_unstabilized]
  type = PetscJacobianTester
  input = 'convergence.i'
  ratio_tol = 1E-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for large displacements without stabilization.'
[]

[jacobian_large_stabilized]
  type = PetscJacobianTester
  input = 'convergence.i'
  ratio_tol = 1E-6
  difference_tol = 1E10
  run_sim = true
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Weak plane stress Jacobian is exact with relative tolerance of 1e-6 for large displacements with stabilization.'
[]

[2D]
  type = CSVDiff
  input = 'pull_2D.i'
  csvdiff = 'pull_3D_out.csv'
  abs_zero = 1E-6
  rel_err = 1e-6
  cli_args = "Outputs/file_base=pull_3D_out"
  detail = "the 2D weak plane stress result should match"
[]

[truesdell_shear]
  type = CSVDiff
  input = 'shear.i'
  cli_args = 'Materials/compute_stress/objective_rate=truesdell Outputs/file_base=truesdell_shear_out'
  csvdiff = 'truesdell_shear_out.csv'
  requirement = "Classical Truesdell response to pure shear matches known solution"
  abs_zero = 1e-6
[]

[jaumann_shear]
  type = CSVDiff
  input = 'shear.i'
  cli_args = 'Materials/compute_stress/objective_rate=jaumann Outputs/file_base=jaumann_shear_out'
  csvdiff = 'jaumann_shear_out.csv'
  requirement = "Classical Jaumann response to pure shear matches known solution"
  abs_zero = 1e-6
[]

[green_naghdi_shear]
  type = CSVDiff
  input = 'shear.i'
  cli_args = 'Materials/compute_stress/objective_rate=green_naghdi Outputs/file_base=green_naghdi_shear_out'
  csvdiff = 'green_naghdi_shear_out.csv'
  requirement = "Classical Green-Naghdi response to pure shear matches known solution"
  abs_zero = 1e-6
[]

[truesdell_rotation]
  type = CSVDiff
  input = 'rotation.i'
  cli_args = 'Materials/stress/objective_rate=truesdell Outputs/file_base=truesdell_rotation_out'
  csvdiff = 'truesdell_rotation_out.csv'
  requirement = "Classical Truesdell response to pure rotation matches known solution"
  abs_zero = 1e-6
[]

[jaumann_rotation]
  type = CSVDiff
  input = 'rotation.i'
  cli_args = 'Materials/stress/objective_rate=jaumann Outputs/file_base=jaumann_rotation_out'
  csvdiff = 'jaumann_rotation_out.csv'
  requirement = "Classical Jaumann response to pure rotation matches known solution"
  abs_zero = 1e-6
[]

[green_naghdi_rotation]
  type = CSVDiff
  input = 'rotation.i'
  cli_args = 'Materials/stress/objective_rate=green_naghdi Outputs/file_base=green_naghdi_rotation_out'
  csvdiff = 'green_naghdi_rotation_out.csv'
  requirement = "Classical Green-Naghdi response to pure rotation matches known solution"
  abs_zero = 1e-6
[]

[truesdell_jacobian]
  type = PetscJacobianTester
  input = 'jacobian.i'
  cli_args = 'Materials/compute_stress/objective_rate=truesdell'
  ratio_tol = 1E-7
  difference_tol = 1E10
  requirement = "Treusdell tangent is exact within rtol of 1e-7"
[]

[jaumann_jacobian]
  type = PetscJacobianTester
  input = 'jacobian.i'
  cli_args = 'Materials/compute_stress/objective_rate=jaumann'
  ratio_tol = 1E-7
  difference_tol = 1E10
  requirement = "Jaumann tangent is exact within rtol of 1e-7"
[]

[green_naghdi_jacobian]
  type = PetscJacobianTester
  input = 'jacobian.i'
  cli_args = 'Materials/compute_stress/objective_rate=green_naghdi'
  ratio_tol = 1E-7
  difference_tol = 1E10
  requirement = "Green-Naghdi tangent is exact within rtol of 1e-7"
[]

[./area_change]
  type = CSVDiff
  input = 'area.i'
  csvdiff = 'area_out.csv'
  requirement = "Stresses are being computed on the deformed volume"
  issues = '#17472'
  design = 'source/materials/lagrangian/ComputeLagrangianObjectiveStress.md'
[../]

[./rotate_stresses]
  type = CSVDiff
  input = 'rotate.i'
  csvdiff = 'rotate_out.csv'
  requirement = "Stress state correctly rotates from step 10 to the final step"
  issues = '#17472'
  design = 'source/materials/lagrangian/ComputeLagrangianObjectiveStress.md'
[../]

[./truesdell]
  type = Exodiff
  input = 'objective_shear.i'
  exodiff = 'objective_shear_out.e'
  requirement = "Classical demonstration that the shear stress/strain response remains linear for a Truesdell rate."
  issues = '#17472'
  design = 'source/materials/lagrangian/ComputeLagrangianObjectiveStress.md'
[../]

[./truesdell]
  type = Exodiff
  input = 'objective_shear.i'
  exodiff = 'objective_shear_out.e'
  requirement = "Classical demonstration that the shear stress/strain response remains linear for a Truesdell rate."
[../]

[./constrained]
  type = Exodiff
  input = 'constrained.i'
  exodiff = 'constrained_out.e'
  requirement = "Stresses and strain as expected for thermal expansion constrained in one direction"
  abs_zero = 1e-6
[../]

[./jacobian_small_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-5
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, no stabilization, including cross-terms'
[../]

[./jacobian_large_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-5
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, no stabilization, including cross-terms'
[../]

[./jacobian_small_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-5
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, including cross-terms'
[../]

[./jacobian_large_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-5
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, including cross-terms'
[../]

[./dirichlet_small_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_small_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_large_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_large_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_small_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_small_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs'
[../]

[./dirichlet_large_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_large_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs'
[../]

[./dirichlet_small_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_small_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_large_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_large_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_small_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_small_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs'
[../]

[./dirichlet_large_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_large_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs'
[../]

[./dirichlet_small_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_small_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_large_neither]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Dirichlet BCs'
[../]

[./neumann_large_neither]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, without stabilization, and Neumann BCs'
[../]

[./dirichlet_small_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_small_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, and Neumann BCs'
[../]

[./dirichlet_large_right]
  type = PetscJacobianTester
  input = 'dirichlet.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Dirichlet BCs'
[../]

[./neumann_large_right]
  type = PetscJacobianTester
  input = 'neumann.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, and Neurmann BCs'
[../]

[./dirichlet]
  type = CSVDiff
  input = 'dirichlet.i'
  csvdiff = 'dirichlet_out.csv'
  requirement = "Quadratic convergence in 1D for DirichletBCs, SMP does better than FDP for this problem."
[../]

[L-large]
  type = CSVDiff
  input = 'large.i'
  csvdiff = 'large_out.csv'
  requirement = "The system shall achieve quadratic convergence in 3D with preset Dirichlet displacement boundary conditions on a complicated geometry for small deformation, and the preconditioning for a single matrix shall match finite-difference preconditioning results."
  valgrind = HEAVY
  # For CI timing requirements
  method = '!dbg'
[]

[L-small]
  type = CSVDiff
  input = 'small.i'
  csvdiff = 'small_out.csv'
  requirement = "The system shall achieve quadratic convergence in 3D with preset Dirichlet displacement boundary conditions for large deformation, and the preconditioning for a single matrix shall match finite-difference preconditioning results."
  valgrind = HEAVY
[]

[./constrained]
  type = Exodiff
  input = 'constrained.i'
  exodiff = 'constrained_out.e'
  requirement = "Stresses and strain as expected for thermal expansion constrained in one direction"
  abs_zero = 1e-6
[../]

[./jacobian_small_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, no stabilization, including cross-terms'
[../]

[./jacobian_large_no_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=false Kernels/sdx/use_displaced_mesh=true Kernels/sdy/use_displaced_mesh=true Kernels/sdz/use_displaced_mesh=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, no stabilization, including cross-terms'
[../]

[./jacobian_small_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=false GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=false Kernels/sdy/use_displaced_mesh=false Kernels/sdz/use_displaced_mesh=false"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for small displacements, with stabilization, including cross-terms'
[../]

[./jacobian_large_with_stab]
  type = PetscJacobianTester
  input = 'jactest.i'
  ratio_tol = 1E-7
  difference_tol = 1E10
  cli_args = "GlobalParams/large_kinematics=true GlobalParams/stabilize_strain=true Kernels/sdx/use_displaced_mesh=true Kernels/sdy/use_displaced_mesh=true Kernels/sdz/use_displaced_mesh=true"
  requirement = 'Jacobian is exact with relative tolerance of 1e-7 for large displacements, with stabilization, including cross-terms'
[../]

[./cook_small_total]
  type = CSVDiff
  input = 'cook_small.i'
  csvdiff = 'cook_small_out.csv'
  requirement = "Stabilized solution matches Cook's solution for stabilized Q4 elements for small deformations."
[../]

[./cook_large_total]
  type = CSVDiff
  input = 'cook_large.i'
  csvdiff = 'cook_large_out.csv'
  requirement = "Stabilized solution matches Cook's solution for stabilized Q4 elements for large deformations."
[../]

[./stvenantkirchhoff]
  type = RunException
  input = stvenantkirchhoff.i
  expect_err = 'ComputeStVenantKirchhoffStress requires an isotropic elasticity'
  requirement = 'Throw an error if you do not provide an isotropic tensor to ComputeStVenantKirchhoffStress'
  issues = '#17472'
  design = 'source/materials/lagrangian/ComputeStVenantKirchhoffStress.md'
[../]

[pk_stvenant]
  type = PetscJacobianTester
  input = 'stvenantkirchhoff.i'
  cli_args = 'GlobalParams/large_kinematics=true'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeStVenantKirchhoffStress.md'
  requirement = 'Correct Jacobian coming from the material model for nonlinear kinematics  with relative error less than 1e-6'
[]

[pk_stvenant_small]
  type = PetscJacobianTester
  input = 'stvenantkirchhoff.i'
  cli_args = 'GlobalParams/large_kinematics=false'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeStVenantKirchhoffStress.md'
  requirement = 'Correct Jacobian coming from the material model for linear kinematics  with relative error less than 1e-6'
[]

[hypoelastic_stvenant]
  type = PetscJacobianTester
  input = 'stvenantkirchhoff.i'
  cli_args = 'GlobalParams/large_kinematics=true Materials/compute_stress/type=ComputeHypoelasticStVenantKirchhoffStress'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeStVenantKirchhoffStress.md'
  requirement = 'Correct Jacobian coming from the material model for nonlinear kinematics with relative error less than 1e-6'
[]

[hypoelastic_stvenant_small]
  type = PetscJacobianTester
  input = 'stvenantkirchhoff.i'
  cli_args = 'GlobalParams/large_kinematics=false Materials/compute_stress/type=ComputeHypoelasticStVenantKirchhoffStress'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeStVenantKirchhoffStress.md'
  requirement = 'Correct Jacobian coming from the material model for linear kinematics with relative error less than 1e-6'
[]

[stvenantkirchhoff]
  type = CSVDiff
  input = stvenantkirchhoff.i
  csvdiff = 'stvenantkirchhoff_out.csv'
  requirement = 'Stress matches exact solution (xx=1.6144e3, rest zero)'
  design = 'source/materials/lagrangian/ComputeStVenantKirchhoffStress.md'
[]

[stvenantkirchhoff_small_deformation]
  type = CSVDiff
  issues = '#22588'
  input = stvenantkirchhoff.i
  csvdiff = 'stvenantkirchhoff_small_deformation_out.csv'
  requirement = 'Stress matches exact solution'
  design = 'source/materials/lagrangian/ComputeStVenantKirchhoffStress.md'
  cli_args = 'GlobalParams/large_kinematics=false Outputs/file_base=stvenantkirchhoff_small_deformation_out'
[]

[cauchy_linear]
  type = PetscJacobianTester
  input = 'cauchy-elastic.i'
  cli_args = 'GlobalParams/large_kinematics=true'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeLagrangianLinearElasticStress.md'
  requirement = 'Correct Jacobian coming from the material model for nonlinear kinematics  with relative error less than 1e-6'
[]

[cauchy_linear_small]
  type = PetscJacobianTester
  input = 'cauchy-elastic.i'
  cli_args = 'GlobalParams/large_kinematics=false'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeLagrangianLinearElasticStress.md'
  requirement = 'Correct Jacobian coming from the material model for linear kinematics  with relative error less than 1e-6'
[]

[cauchy-elastic]
  type = CSVDiff
  input = cauchy-elastic.i
  csvdiff = 'cauchy-elastic_out.csv'
  requirement = 'Stress matches elastic solution (xx=1e4, rest zero)'
  design = 'source/materials/lagrangian/ComputeLagrangianLinearElasticStress.md'
[]

[neohookean]
  type = PetscJacobianTester
  input = 'neohookean.i'
  cli_args = 'GlobalParams/large_kinematics=true'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeNeoHookeanStress.md'
  requirement = 'Correct Jacobian coming from the material model for nonlinear kinematics with relative error less than 1e-6'
[]

[neohookean_small]
  type = PetscJacobianTester
  input = 'neohookean.i'
  cli_args = 'GlobalParams/large_kinematics=false'
  ratio_tol = 1E-6
  difference_tol = 1E10
  design = 'source/materials/lagrangian/ComputeNeoHookeanStress.md'
  requirement = 'Correct Jacobian coming from the material model for linear kinematics with relative error less than 1e-6'
[]

[neohookean]
  type = CSVDiff
  input = neohookean.i
  csvdiff = 'neohookean_out.csv'
  abs_zero = 1e-9
  requirement = 'Stress matches exact analytic solution, rest zero'
  design = 'source/materials/lagrangian/ComputeNeoHookeanStress.md'
[]

[neohookean_small_deformation]
  type = CSVDiff
  issues = '#22588'
  input = neohookean.i
  csvdiff = 'neohookean_small_deformation_out.csv'
  abs_zero = 1e-9
  requirement = 'Stress matches exact analytic solution, rest zero'
  design = 'source/materials/lagrangian/ComputeNeoHookeanStress.md'
  cli_args = 'GlobalParams/large_kinematics=false Outputs/file_base=neohookean_small_deformation_out'
[]

[elastoplastic_linear_hardening]
  type = PetscJacobianTester
  input = hyperelastic_J2_plastic.i
  cli_args = "Materials/flow_stress/function='320+688*effective_plastic_strain'"
  ratio_tol = 1E-6
  difference_tol = 1E10
  run_sim = true
  design = 'source/materials/lagrangian/ComputeSimoHughesJ2PlasticityStress.md'
  requirement = 'Correct Jacobian for elastoplasticity with linear hardening with relative error less than 1e-6'
[]

[elastoplastic_powerlaw_hardening]
  type = PetscJacobianTester
  input = hyperelastic_J2_plastic.i
  cli_args = "Materials/flow_stress/function='320*(1+effective_plastic_strain/1e-3)^(1/5)'"
  ratio_tol = 1E-6
  difference_tol = 1E10
  run_sim = true
  design = 'source/materials/lagrangian/ComputeSimoHughesJ2PlasticityStress.md'
  requirement = 'Correct Jacobian for elastoplasticity with power-law hardening with relative error less than 1e-6'
[]

[elastoplastic_linear_hardening]
  type = CSVDiff
  input = hyperelastic_J2_plastic.i
  cli_args = 'Materials/flow_stress/function=320+688*effective_plastic_strain Outputs/file_base=hyperelastic_J2_plastic_linear_hardening_out'
  csvdiff = 'hyperelastic_J2_plastic_linear_hardening_out.csv'
  abs_zero = 1e-9
  requirement = 'Stress matches exact analytic solution for elastoplasticity with linear hardening'
  design = 'source/materials/lagrangian/ComputeSimoHughesJ2PlasticityStress.md'
[]

[elastoplastic_powerlaw_hardening]
  type = CSVDiff
  input = hyperelastic_J2_plastic.i
  cli_args = "Materials/flow_stress/function='320*(1+effective_plastic_strain/1e-3)^(1/5)' Outputs/file_base=hyperelastic_J2_plastic_powerlaw_hardening_out"
  csvdiff = 'hyperelastic_J2_plastic_powerlaw_hardening_out.csv'
  abs_zero = 1e-9
  requirement = 'Stress matches exact analytic solution for elastoplasticity with power-law hardening'
  design = 'source/materials/lagrangian/ComputeSimoHughesJ2PlasticityStress.md'
[]

[stvenantkirchhoff_hypoelastic]
  type = CSVDiff
  input = stvenantkirchhoff.i
  cli_args = 'Materials/compute_stress/type=ComputeHypoelasticStVenantKirchhoffStress Outputs/file_base=stvenantkirchhoff_hypoelastic_out'
  csvdiff = 'stvenantkirchhoff_hypoelastic_out.csv'
  requirement = 'The hypoelastic equivalent of the St. Venant-Kirchhoff model gives the same result as its hyperelastic counterpart.'
  design = 'source/materials/lagrangian/ComputeHypoelasticStVenantKirchhoffStress.md'
[]

[./rank_two_sampler]
  type = 'CSVDiff'
  input = 'rank_two_sampler.i'
  csvdiff = 'rank_two_sampler_out_stress_xx_0010.csv'
  compiler = '!INTEL'
  design = 'source/vectorpostprocessors/LineMaterialRankTwoSampler.md'
  requirement = "The system shall allow sampling of material properties derived
                   from rank two tensors along a line and output those
                   quantities via a vectorpostprocessor."
[../]

[./rank_two_scalar_sampler]
  type = 'CSVDiff'
  input = 'rank_two_scalar_sampler.i'
  csvdiff = 'rank_two_scalar_sampler_out_vonmises_0010.csv'
  compiler = '!INTEL'
  design = 'source/vectorpostprocessors/LineMaterialRankTwoScalarSampler.md'
  requirement = "The system shall allow sampling of scalar material properties along a
                   line and output those quantities via a vectorpostprocessor."
[../]

[./test5a_lim]
  type = 'Exodiff'
  input = 'nafems_test5a_lim.i'
  exodiff = 'nafems_test5a_lim_out.e'
  rel_err = 4e-5
  abs_zero = 1e-8
  superlu = true
  issues = '#8553'
  requirement = 'The system shall compute a timestep size that is limited by a power law creep model and a specified maximum inelastic strain increment.'
[../]

[./test5a_lim_on_initial]
  type = 'CSVDiff'
  input = 'nafems_test5a_lim.i'
  cli_args = 'Postprocessors/matl_ts_min/execute_on="initial timestep_end"
    Outputs/file_base=nafems_test5a_lim_on_initial_out'
  csvdiff = 'nafems_test5a_lim_on_initial_out.csv'
  superlu = true
  override_columns = '_dt elas_str_yy matl_ts_min'
  override_rel_err = '4e-5 4e-5 4e-5'
  override_abs_zero = '1e-8 1e-10 1e-10'
  issues = '#10382'
  requirement = 'The system shall not impose a limit on the time step during the initial evaluation when the creep limiting time step option is used.'
[../]

[./elements_damage_limit]
  type = 'Exodiff'
  input = 'elements_changed_timestep_limit.i'
  exodiff = 'elements_changed_timestep_limit_out.e'
  abs_zero = 1.e-6
  requirement = 'The ScalarMaterialDamage model shall be capable of informing the material-based time step calculation based on the number of elements changing damage state in a step'
  issues = '#11662'
  design = 'ScalarMaterialDamage.md MaterialTimeStepPostprocessor.md'
[../]

[./mixed_timestep_limit]
  type = 'Exodiff'
  input = 'elements_changed_timestep_limit.i'
  exodiff = 'mixed_timestep_limit_out.e'
  abs_zero = 1.e-6
  cli_args = 'Postprocessors/time_step_limit/use_material_timestep_limit=true
                Outputs/file_base=mixed_timestep_limit_out'
  requirement = 'The MaterialTimeStepPostprocessor model shall be capable of computing a time step based on both the material time step limited by damage evoluation and the number of elements changing damage state in a step'
  issues = '#11662'
  design = 'ScalarMaterialDamage.md MaterialTimeStepPostprocessor.md'
[../]

[./elements_damage_limit_unknown_prop]
  type = 'RunException'
  prereq = elements_damage_limit
  input = 'elements_changed_timestep_limit.i'
  cli_args = 'Postprocessors/time_step_limit/elements_changed_property=unknown_property' #Point it to an unknown property
  expect_err = "Material property 'unknown_property', requested by 'time_step_limit' is not defined on block 0"
  requirement = "The MaterialTimeStepPostprocessor shall generate an error if an unknown property is requested with the 'time_step_limit' parameter"
  issues = '#11662'
  design = 'MaterialTimeStepPostprocessor.md'
[../]

[./e]
  type = 'RunException'
  prereq = scalar_damage_material_limit
  input = 'scalar_material_damage_timestep_limit.i'
  cli_args = 'Postprocessors/time_step_limit/use_material_timestep_limit=false' #disable botg matl_timestep and elements count
  expect_err = "either use_material_timestep_limit needs to be true or elements_changed_property defined"
  requirement = "The MaterialTimeStepPostprocessor shall generate an error if neither the material time step limit nor the elements changed limit is specified."
  issues = '#11662'
  design = 'MaterialTimeStepPostprocessor.md'
[../]

[./nl1_lim]
  type = 'Exodiff'
  input = 'nafems_nl1_lim.i'
  exodiff = 'nafems_nl1_lim_out.e'
  abs_zero = 1e-9
  requirement = 'The system to limit the analysis time step based on material behavior shall correctly function when used with an isotropic plasticity model.'
[../]

[./nl1_lim_on_initial]
  type = 'CSVDiff'
  input = 'nafems_nl1_lim.i'
  cli_args = 'Postprocessors/matl_ts_min/execute_on="initial timestep_end"
    Outputs/file_base=nafems_nl1_lim_on_initial_out'
  csvdiff = 'nafems_nl1_lim_on_initial_out.csv'
  requirement = 'The system to limit the analysis time step based on material behavior shall correctly function when used with an isotropic plasticity model when the MaterialTimeStepPostprocessor is run at initialization.'
[../]

[./no_inelastic_model_limit]
  type = 'CSVDiff'
  input = 'no_inelastic_model_timestep_limit.i'
  csvdiff = 'no_inelastic_model_timestep_limit_out.csv'
  requirement = 'The ComputeMultipleInelasticStress model shall compute a time step equal to the maximum real number if no inelastic model is provided'
  issues = '#13250'
  design = 'ScalarMaterialDamage.md MaterialTimeStepPostprocessor.md'
[../]

[./no_inelastic_model_limit_defined]
  type = 'CSVDiff'
  input = 'no_inelastic_model_timestep_limit.i'
  csvdiff = 'no_inelastic_model_timestep_limit_defined_out.csv'
  requirement = 'The system shall compute a time step equal to a user input maximum real number if no inelastic model is provided'
  cli_args = 'Postprocessors/time_step_limit/maximum_value=0.2 Outputs/file_base=no_inelastic_model_timestep_limit_defined_out'
  issues = '#22604'
  design = 'MaterialTimeStepPostprocessor.md'
[../]

[./scalar_damage_material_limit]
  type = 'CSVDiff'
  input = 'scalar_material_damage_timestep_limit.i'
  csvdiff = 'scalar_material_damage_timestep_limit_out.csv'
  abs_zero = 1.e-6
  requirement = 'The ScalarMaterialDamage model shall be capable of informing the material-based time step calculation based on the damage evolution'
  issues = '#11662'
  design = 'ScalarMaterialDamage.md'
[../]

[./elements_damage_limit]
  type = 'Exodiff'
  input = 'elements_changed_timestep_limit.i'
  exodiff = 'elements_changed_timestep_limit_out.e'
  abs_zero = 1.e-6
  requirement = 'The ScalarMaterialDamage model shall be capable of informing the material-based time step calculation based on the number of elements changing damage state in a step'
  issues = '#11662'
  design = 'ScalarMaterialDamage.md MaterialTimeStepPostprocessor.md'
[../]

[./mixed_timestep_limit]
  type = 'Exodiff'
  input = 'elements_changed_timestep_limit.i'
  exodiff = 'mixed_timestep_limit_out.e'
  abs_zero = 1.e-6
  cli_args = 'Postprocessors/time_step_limit/use_material_timestep_limit=true
                Outputs/file_base=mixed_timestep_limit_out'
  requirement = 'The MaterialTimeStepPostprocessor model shall be capable of computing a time step based on both the material time step limited by damage evoluation and the number of elements changing damage state in a step'
  issues = '#11662'
  design = 'ScalarMaterialDamage.md MaterialTimeStepPostprocessor.md'
[../]

[./no_inelastic_model_limit]
  type = 'CSVDiff'
  input = 'no_inelastic_model_timestep_limit.i'
  csvdiff = 'no_inelastic_model_timestep_limit_out.csv'
  requirement = 'The ComputeMultipleInelasticStress model shall compute a time step equal to the maximum real number if no inelastic model is provided'
  issues = '#13250'
  design = 'ScalarMaterialDamage.md MaterialTimeStepPostprocessor.md'
[../]

[scalar_damage_material]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  csvdiff = 'scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material."
[]

[ad_scalar_damage_material]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  csvdiff = 'ad_scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation."
[]

[scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=scalar_material_damage_old_out'
  csvdiff = 'scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index."
[]

[ad_scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=ad_scalar_material_damage_old_out'
  csvdiff = 'ad_scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index when using automatic differentiation."
[]

[scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1."
[]

[ad_scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1 also when using automatic differentiation."
[]

[scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress"
[]

[ad_scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation"
[]

[combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  csvdiff = 'combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models."
[]

[combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=combined_scalar_damage_mult_out'
  csvdiff = 'combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models."
[]

[combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_sub_out'
  csvdiff = 'combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model"
[]

[combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_combined_out'
  csvdiff = 'combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models."
[]

[ad_combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  csvdiff = 'ad_combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=ad_combined_scalar_damage_mult_out'
  csvdiff = 'ad_combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_sub_out'
  csvdiff = 'ad_combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_combined_out'
  csvdiff = 'ad_combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation."
[]

[scalar_damage_material_inelastic]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep.i'
  csvdiff = 'scalar_material_damage_creep_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation."
[]

[scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep_power.i'
  csvdiff = 'scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation."
[]

[ad_scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage_creep_power.i'
  csvdiff = 'ad_scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation."
[]

[multiple_inelastic_bad_damage_model]
  type = RunException
  input = ad_scalar_material_damage_creep_power.i
  expect_err = "Damage Model.*damage_index.*is not compatible with ADComputeMultipleInelasticStress"
  requirement = "The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object."
  issues = '#20722'
  cli_args = 'Materials/stress/damage_model=damage_index'
  allow_warnings = True
[]

[nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'nonlocal_scalar_damage.i'
  csvdiff = 'nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model."
  issues = '#21786'
[]

[ad_nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'ad_nonlocal_scalar_damage.i'
  csvdiff = 'ad_nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation."
  issues = '#21786'
[]

[modal]
  type = Exodiff
  input = 'modal.i'
  exodiff = 'modal_out.e'
  exodiff_opts = '-eigen_relative'
  abs_zero = 1e-10
  requirement = "The module shall be able to perform modal analysis with the Eigenvalue Executioner."
[]

[powerlaw]
  type = 'Exodiff'
  input = 'power_law_creep.i'
  exodiff = 'power_law_creep_out.e'
  valgrind = HEAVY
  requirement = "The AD multiple power law creep must reproduce the results of the AD single power law creep: Reference results."
[]

[multipowerlaw]
  type = 'Exodiff'
  input = 'power_law_creep.i'
  exodiff = 'multi_power_law_creep_out.e'
  cli_args = "Materials/creep_one/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_one/stress_thresholds='0 999999999999'
              Materials/creep_nine/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_nine/stress_thresholds='0 999999999999'
               Outputs/file_base=multi_power_law_creep_out"
  valgrind = HEAVY
  requirement = "The AD multiple power law creep must reproduce the results of the AD single power law creep when a single stress increment is provided by the user."
[]

[multipowerlaw_two_intervals]
  type = 'Exodiff'
  input = 'power_law_creep.i'
  exodiff = 'multipowerlaw_two_intervals_out.e'
  cli_args = "Materials/creep_one/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_one/stress_thresholds='0 42000 300000' Materials/creep_one/coefficient='1e-24 1e-24' Materials/creep_one/n_exponent='4 4' Materials/creep_one/m_exponent='0 0' Materials/creep_one/activation_energy='0 0'
              Materials/creep_nine/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_nine/stress_thresholds='0 42000 300000' Materials/creep_nine/coefficient='9e-24 9e-24' Materials/creep_nine/n_exponent='4 4' Materials/creep_nine/m_exponent='0 0' Materials/creep_nine/activation_energy='0 0'
              Outputs/file_base=multipowerlaw_two_intervals_out"
  valgrind = HEAVY
  requirement = "The AD multiple power law creep must reproduce the results of the AD single power law creep with multiple stress intervals with same power law material parameters."
[]

[multipowerlaw_two_intervals_no_continuity]
  type = 'Exodiff'
  input = 'power_law_creep.i'
  exodiff = 'multi_power_law_creep_two_intervals_different_no_continuity_out.e'
  cli_args = "Materials/creep_one/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_one/stress_thresholds='0 53000 300000' Materials/creep_one/coefficient='1e-24 1.92307692e-29' Materials/creep_one/n_exponent='4 9.0' Materials/creep_one/m_exponent='0 0' Materials/creep_one/activation_energy='0 0'
              Materials/creep_nine/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_nine/stress_thresholds='0 53000 300000' Materials/creep_nine/coefficient='9e-24 3.32840237e-33' Materials/creep_nine/n_exponent='4 9.0' Materials/creep_nine/m_exponent='0 0' Materials/creep_nine/activation_energy='0 0'
              Outputs/file_base=multi_power_law_creep_two_intervals_different_no_continuity_out"
  abs_zero = 1.0e-4
  rel_err = 5.0e-4
  requirement = "The AD multiple power law creep must avoid regression for a simple few-element problem whose solution has stress levels encompassing two different sets of power law parameters"
[]

[multipowerlaw_user_input_error]
  type = 'RunException'
  input = 'power_law_creep.i'
  expect_err = 'Stress thresholds input must be provided in increasing ordered'
  cli_args = "Materials/creep_one/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_one/stress_thresholds='0 53000 52000' Materials/creep_one/coefficient='1e-24 1.92307692e-29' Materials/creep_one/n_exponent='4 9.0' Materials/creep_one/m_exponent='0 0' Materials/creep_one/activation_energy='0 0'
              Materials/creep_nine/type=ADMultiplePowerLawCreepStressUpdate Materials/creep_nine/stress_thresholds='0 53000 300000' Materials/creep_nine/coefficient='9e-24 3.32840237e-33' Materials/creep_nine/n_exponent='4 9.0' Materials/creep_nine/m_exponent='0 0' Materials/creep_nine/activation_energy='0 0'
              Outputs/file_base=multi_power_law_creep_two_intervals_different_no_continuity_out"

  requirement = "Stress thresholds must be provided in increasing order, otherwise an error will inform the user of such a requirement. "
[]

[neml2_error]
  type = RunException
  input = 'fem.i'
  cli_args = 'neml2_input=error'
  requirement = 'The system shall be capable of capturing errors occurring during the evaluation of a NEML2 model.'
  expect_err = 'To debug NEML2 related issues'
  collections = 'SYSTEM'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = none
[]

[no_neml2]
  type = RunException
  input = 'fem.i'
  cli_args = 'neml2_input=elasticity'
  requirement = 'The system shall throw an error upon instantiation of NEML2 interface objects if NEML2 is not available.'
  expect_err = 'To use this object, you need to have the `NEML2` library installed'
  collections = 'SYSTEM'
  libtorch = false
[]

[elasticity]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=elasticity
                  UserObjects/active='model input_strain'
                  UserObjects/model/gather_uos='input_strain'
                  Materials/active='output_stress_jacobian'"
  exodiff = 'elasticity.e'
  detail = 'to solve an elasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_perfect]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_perfect
                  UserObjects/active='model input_strain input_old_strain input_old_stress'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress'
                  Materials/active='output_stress_jacobian'"
  exodiff = 'viscoplasticity_perfect.e'
  detail = 'to solve a perfect viscoplasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_isoharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_isoharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep'
                  Materials/active='output_stress_jacobian output_ep'"
  exodiff = 'viscoplasticity_isoharden.e'
  detail = 'to solve a viscoplasticity problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_kinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_kinharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_Kp'
                  Materials/active='output_stress_jacobian output_Kp'"
  exodiff = 'viscoplasticity_kinharden.e'
  detail = 'to solve a viscoplasticity problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_isokinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_isokinharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_ep output_Kp'"
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'to solve a viscoplasticity problem with both isotropic and kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_chaboche]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_chaboche
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep input_old_X1 input_old_X2'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep input_old_X1 input_old_X2'
                  Materials/active='output_stress_jacobian output_ep output_X1 output_X2'"
  exodiff = 'viscoplasticity_chaboche.e'
  detail = 'to solve a viscoplasticity problem with non-associative Chaboche hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_radial_return]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_radial_return
                  UserObjects/active='model input_strain input_old_Ep input_old_gamma'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_gamma'
                  Materials/active='output_stress_jacobian output_Ep output_gamma'"
  exodiff = 'viscoplasticity_radial_return.e'
  detail = 'to solve a viscoplasticity problem using radial return;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_perfect]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_perfect
                  UserObjects/active='model input_strain input_old_Ep'
                  UserObjects/model/gather_uos='input_strain input_old_Ep'
                  Materials/active='output_stress_jacobian output_Ep'"
  exodiff = 'rate_independent_plasticity_perfect.e'
  detail = 'to solve a rate-independent problem with perfect plasticity;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_isoharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_isoharden
                  UserObjects/active='model input_strain input_old_Ep input_old_ep'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_ep'
                  Materials/active='output_stress_jacobian output_Ep output_ep'"
  exodiff = 'rate_independent_plasticity_isoharden.e'
  detail = 'to solve a rate-independent problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_kinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_kinharden
                  UserObjects/active='model input_strain input_old_Ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_Ep output_Kp'"
  exodiff = 'rate_independent_plasticity_kinharden.e'
  detail = 'to solve a rate-independent problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_isokinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_isokinharden
                  UserObjects/active='model input_strain input_old_Ep input_old_ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_Ep output_ep output_Kp'"
  exodiff = 'rate_independent_plasticity_isokinharden.e'
  detail = 'to solve a rate-independent problem with both isotropic and kinematic hardening.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[moose_to_neml2_parameter]
  type = Exodiff
  input = 'moose_to_neml2_parameters.i'
  exodiff = 'moose_to_neml2_parameters_out.e'
  requirement = 'The system shall provide a modular way to transfer variables and/or real material property to NEML2 for use as model parameters.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[moose_to_neml2_parameter_error]
  type = RunException
  input = 'moose_to_neml2_parameters.i'
  cli_args = 'UserObjects/gather_E/neml2_parameter=p'
  requirement = 'The system shall error out while trying to set a parameter that does not exist.'
  expect_err = 'there is not such parameter in the NEML2 material model.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[neml2_parameter_derivative]
  type = Exodiff
  input = 'moose_to_neml2_parameters.i'
  exodiff = 'neml2_parameter_derivative_out.e'
  cli_args = "Materials/active='output_stress_jacobian nu_material dstress_dE' Outputs/file_base='neml2_parameter_derivative_out'"
  requirement = 'The system shall provide for a modular way to compute NEML2 output with respect to specific model parameters and save that it as a MOOSE material property.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[neml2_to_moose_material]
  type = Exodiff
  input = 'neml2_to_moose_material.i'
  exodiff = 'neml2_to_moose_material_out.e'
  requirement = 'The system shall provide for a modular way to transfer NEML2 results to material properties..'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[elasticity]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=elasticity'
  exodiff = 'elasticity.e'
  detail = 'to solve an elasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_perfect]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_perfect'
  exodiff = 'viscoplasticity_perfect.e'
  detail = 'to solve a perfect viscoplasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_isoharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isoharden'
  exodiff = 'viscoplasticity_isoharden.e'
  detail = 'to solve a viscoplasticity problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_kinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_kinharden'
  exodiff = 'viscoplasticity_kinharden.e'
  detail = 'to solve a viscoplasticity problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_isokinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isokinharden'
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'to solve a viscoplasticity problem with both isotropic and kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_chaboche]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_chaboche'
  exodiff = 'viscoplasticity_chaboche.e'
  detail = 'to solve a viscoplasticity problem with non-associative Chaboche hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_radial_return]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_radial_return'
  exodiff = 'viscoplasticity_radial_return.e'
  detail = 'to solve a viscoplasticity problem using radial return;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_perfect]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_perfect'
  exodiff = 'rate_independent_plasticity_perfect.e'
  detail = 'to solve a rate-independent problem with perfect plasticity;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_isoharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_isoharden'
  exodiff = 'rate_independent_plasticity_isoharden.e'
  detail = 'to solve a rate-independent problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_kinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_kinharden'
  exodiff = 'rate_independent_plasticity_kinharden.e'
  detail = 'to solve a rate-independent problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_isokinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_isokinharden'
  exodiff = 'rate_independent_plasticity_isokinharden.e'
  detail = 'to solve a rate-independent problem with both isotropic and kinematic hardening.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[batched]
  type = Exodiff
  prereq = 'neml2_legacy/viscoplasticity_isokinharden'
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isokinharden NEML2/mode=ALL'
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'in a batched fashion.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[neml2_error]
  type = RunException
  input = 'fem.i'
  cli_args = 'neml2_input=error'
  requirement = 'The system shall be capable of capturing errors occurring during the evaluation of a NEML2 model.'
  expect_err = 'To debug NEML2 related issues'
  collections = 'SYSTEM'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = none
[]

[no_neml2]
  type = RunException
  input = 'fem.i'
  cli_args = 'neml2_input=elasticity'
  requirement = 'The system shall throw an error upon instantiation of NEML2 interface objects if NEML2 is not available.'
  expect_err = 'To use this object, you need to have the `NEML2` library installed'
  collections = 'SYSTEM'
  libtorch = false
[]

[elasticity]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=elasticity
                  UserObjects/active='model input_strain'
                  UserObjects/model/gather_uos='input_strain'
                  Materials/active='output_stress_jacobian'"
  exodiff = 'elasticity.e'
  detail = 'to solve an elasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_perfect]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_perfect
                  UserObjects/active='model input_strain input_old_strain input_old_stress'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress'
                  Materials/active='output_stress_jacobian'"
  exodiff = 'viscoplasticity_perfect.e'
  detail = 'to solve a perfect viscoplasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_isoharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_isoharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep'
                  Materials/active='output_stress_jacobian output_ep'"
  exodiff = 'viscoplasticity_isoharden.e'
  detail = 'to solve a viscoplasticity problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_kinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_kinharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_Kp'
                  Materials/active='output_stress_jacobian output_Kp'"
  exodiff = 'viscoplasticity_kinharden.e'
  detail = 'to solve a viscoplasticity problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_isokinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_isokinharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_ep output_Kp'"
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'to solve a viscoplasticity problem with both isotropic and kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_chaboche]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_chaboche
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep input_old_X1 input_old_X2'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep input_old_X1 input_old_X2'
                  Materials/active='output_stress_jacobian output_ep output_X1 output_X2'"
  exodiff = 'viscoplasticity_chaboche.e'
  detail = 'to solve a viscoplasticity problem with non-associative Chaboche hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_radial_return]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_radial_return
                  UserObjects/active='model input_strain input_old_Ep input_old_gamma'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_gamma'
                  Materials/active='output_stress_jacobian output_Ep output_gamma'"
  exodiff = 'viscoplasticity_radial_return.e'
  detail = 'to solve a viscoplasticity problem using radial return;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_perfect]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_perfect
                  UserObjects/active='model input_strain input_old_Ep'
                  UserObjects/model/gather_uos='input_strain input_old_Ep'
                  Materials/active='output_stress_jacobian output_Ep'"
  exodiff = 'rate_independent_plasticity_perfect.e'
  detail = 'to solve a rate-independent problem with perfect plasticity;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_isoharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_isoharden
                  UserObjects/active='model input_strain input_old_Ep input_old_ep'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_ep'
                  Materials/active='output_stress_jacobian output_Ep output_ep'"
  exodiff = 'rate_independent_plasticity_isoharden.e'
  detail = 'to solve a rate-independent problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_kinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_kinharden
                  UserObjects/active='model input_strain input_old_Ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_Ep output_Kp'"
  exodiff = 'rate_independent_plasticity_kinharden.e'
  detail = 'to solve a rate-independent problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_isokinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_isokinharden
                  UserObjects/active='model input_strain input_old_Ep input_old_ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_Ep output_ep output_Kp'"
  exodiff = 'rate_independent_plasticity_isokinharden.e'
  detail = 'to solve a rate-independent problem with both isotropic and kinematic hardening.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[moose_to_neml2_parameter]
  type = Exodiff
  input = 'moose_to_neml2_parameters.i'
  exodiff = 'moose_to_neml2_parameters_out.e'
  requirement = 'The system shall provide a modular way to transfer variables and/or real material property to NEML2 for use as model parameters.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[moose_to_neml2_parameter_error]
  type = RunException
  input = 'moose_to_neml2_parameters.i'
  cli_args = 'UserObjects/gather_E/neml2_parameter=p'
  requirement = 'The system shall error out while trying to set a parameter that does not exist.'
  expect_err = 'there is not such parameter in the NEML2 material model.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[neml2_parameter_derivative]
  type = Exodiff
  input = 'moose_to_neml2_parameters.i'
  exodiff = 'neml2_parameter_derivative_out.e'
  cli_args = "Materials/active='output_stress_jacobian nu_material dstress_dE' Outputs/file_base='neml2_parameter_derivative_out'"
  requirement = 'The system shall provide for a modular way to compute NEML2 output with respect to specific model parameters and save that it as a MOOSE material property.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[neml2_to_moose_material]
  type = Exodiff
  input = 'neml2_to_moose_material.i'
  exodiff = 'neml2_to_moose_material_out.e'
  requirement = 'The system shall provide for a modular way to transfer NEML2 results to material properties..'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[elasticity]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=elasticity'
  exodiff = 'elasticity.e'
  detail = 'to solve an elasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_perfect]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_perfect'
  exodiff = 'viscoplasticity_perfect.e'
  detail = 'to solve a perfect viscoplasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_isoharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isoharden'
  exodiff = 'viscoplasticity_isoharden.e'
  detail = 'to solve a viscoplasticity problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_kinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_kinharden'
  exodiff = 'viscoplasticity_kinharden.e'
  detail = 'to solve a viscoplasticity problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_isokinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isokinharden'
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'to solve a viscoplasticity problem with both isotropic and kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_chaboche]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_chaboche'
  exodiff = 'viscoplasticity_chaboche.e'
  detail = 'to solve a viscoplasticity problem with non-associative Chaboche hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_radial_return]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_radial_return'
  exodiff = 'viscoplasticity_radial_return.e'
  detail = 'to solve a viscoplasticity problem using radial return;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_perfect]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_perfect'
  exodiff = 'rate_independent_plasticity_perfect.e'
  detail = 'to solve a rate-independent problem with perfect plasticity;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_isoharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_isoharden'
  exodiff = 'rate_independent_plasticity_isoharden.e'
  detail = 'to solve a rate-independent problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_kinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_kinharden'
  exodiff = 'rate_independent_plasticity_kinharden.e'
  detail = 'to solve a rate-independent problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_isokinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_isokinharden'
  exodiff = 'rate_independent_plasticity_isokinharden.e'
  detail = 'to solve a rate-independent problem with both isotropic and kinematic hardening.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[batched]
  type = Exodiff
  prereq = 'neml2_legacy/viscoplasticity_isokinharden'
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isokinharden NEML2/mode=ALL'
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'in a batched fashion.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[neml2_error]
  type = RunException
  input = 'fem.i'
  cli_args = 'neml2_input=error'
  requirement = 'The system shall be capable of capturing errors occurring during the evaluation of a NEML2 model.'
  expect_err = 'To debug NEML2 related issues'
  collections = 'SYSTEM'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = none
[]

[no_neml2]
  type = RunException
  input = 'fem.i'
  cli_args = 'neml2_input=elasticity'
  requirement = 'The system shall throw an error upon instantiation of NEML2 interface objects if NEML2 is not available.'
  expect_err = 'To use this object, you need to have the `NEML2` library installed'
  collections = 'SYSTEM'
  libtorch = false
[]

[elasticity]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=elasticity
                  UserObjects/active='model input_strain'
                  UserObjects/model/gather_uos='input_strain'
                  Materials/active='output_stress_jacobian'"
  exodiff = 'elasticity.e'
  detail = 'to solve an elasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_perfect]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_perfect
                  UserObjects/active='model input_strain input_old_strain input_old_stress'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress'
                  Materials/active='output_stress_jacobian'"
  exodiff = 'viscoplasticity_perfect.e'
  detail = 'to solve a perfect viscoplasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_isoharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_isoharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep'
                  Materials/active='output_stress_jacobian output_ep'"
  exodiff = 'viscoplasticity_isoharden.e'
  detail = 'to solve a viscoplasticity problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_kinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_kinharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_Kp'
                  Materials/active='output_stress_jacobian output_Kp'"
  exodiff = 'viscoplasticity_kinharden.e'
  detail = 'to solve a viscoplasticity problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_isokinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_isokinharden
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_ep output_Kp'"
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'to solve a viscoplasticity problem with both isotropic and kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_chaboche]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_chaboche
                  UserObjects/active='model input_strain input_old_strain input_old_stress input_old_ep input_old_X1 input_old_X2'
                  UserObjects/model/gather_uos='input_strain input_old_strain input_old_stress input_old_ep input_old_X1 input_old_X2'
                  Materials/active='output_stress_jacobian output_ep output_X1 output_X2'"
  exodiff = 'viscoplasticity_chaboche.e'
  detail = 'to solve a viscoplasticity problem with non-associative Chaboche hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[viscoplasticity_radial_return]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=viscoplasticity_radial_return
                  UserObjects/active='model input_strain input_old_Ep input_old_gamma'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_gamma'
                  Materials/active='output_stress_jacobian output_Ep output_gamma'"
  exodiff = 'viscoplasticity_radial_return.e'
  detail = 'to solve a viscoplasticity problem using radial return;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_perfect]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_perfect
                  UserObjects/active='model input_strain input_old_Ep'
                  UserObjects/model/gather_uos='input_strain input_old_Ep'
                  Materials/active='output_stress_jacobian output_Ep'"
  exodiff = 'rate_independent_plasticity_perfect.e'
  detail = 'to solve a rate-independent problem with perfect plasticity;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_isoharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_isoharden
                  UserObjects/active='model input_strain input_old_Ep input_old_ep'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_ep'
                  Materials/active='output_stress_jacobian output_Ep output_ep'"
  exodiff = 'rate_independent_plasticity_isoharden.e'
  detail = 'to solve a rate-independent problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_kinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_kinharden
                  UserObjects/active='model input_strain input_old_Ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_Ep output_Kp'"
  exodiff = 'rate_independent_plasticity_kinharden.e'
  detail = 'to solve a rate-independent problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[rate_independent_plasticity_isokinharden]
  type = Exodiff
  input = 'fem_modular.i'
  cli_args = "neml2_input=rate_independent_plasticity_isokinharden
                  UserObjects/active='model input_strain input_old_Ep input_old_ep input_old_Kp'
                  UserObjects/model/gather_uos='input_strain input_old_Ep input_old_ep input_old_Kp'
                  Materials/active='output_stress_jacobian output_Ep output_ep output_Kp'"
  exodiff = 'rate_independent_plasticity_isokinharden.e'
  detail = 'to solve a rate-independent problem with both isotropic and kinematic hardening.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[moose_to_neml2_parameter]
  type = Exodiff
  input = 'moose_to_neml2_parameters.i'
  exodiff = 'moose_to_neml2_parameters_out.e'
  requirement = 'The system shall provide a modular way to transfer variables and/or real material property to NEML2 for use as model parameters.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[moose_to_neml2_parameter_error]
  type = RunException
  input = 'moose_to_neml2_parameters.i'
  cli_args = 'UserObjects/gather_E/neml2_parameter=p'
  requirement = 'The system shall error out while trying to set a parameter that does not exist.'
  expect_err = 'there is not such parameter in the NEML2 material model.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[neml2_parameter_derivative]
  type = Exodiff
  input = 'moose_to_neml2_parameters.i'
  exodiff = 'neml2_parameter_derivative_out.e'
  cli_args = "Materials/active='output_stress_jacobian nu_material dstress_dE' Outputs/file_base='neml2_parameter_derivative_out'"
  requirement = 'The system shall provide for a modular way to compute NEML2 output with respect to specific model parameters and save that it as a MOOSE material property.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[neml2_to_moose_material]
  type = Exodiff
  input = 'neml2_to_moose_material.i'
  exodiff = 'neml2_to_moose_material_out.e'
  requirement = 'The system shall provide for a modular way to transfer NEML2 results to material properties..'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
[]

[elasticity]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=elasticity'
  exodiff = 'elasticity.e'
  detail = 'to solve an elasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_perfect]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_perfect'
  exodiff = 'viscoplasticity_perfect.e'
  detail = 'to solve a perfect viscoplasticity problem;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_isoharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isoharden'
  exodiff = 'viscoplasticity_isoharden.e'
  detail = 'to solve a viscoplasticity problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_kinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_kinharden'
  exodiff = 'viscoplasticity_kinharden.e'
  detail = 'to solve a viscoplasticity problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_isokinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isokinharden'
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'to solve a viscoplasticity problem with both isotropic and kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_chaboche]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_chaboche'
  exodiff = 'viscoplasticity_chaboche.e'
  detail = 'to solve a viscoplasticity problem with non-associative Chaboche hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[viscoplasticity_radial_return]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_radial_return'
  exodiff = 'viscoplasticity_radial_return.e'
  detail = 'to solve a viscoplasticity problem using radial return;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_perfect]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_perfect'
  exodiff = 'rate_independent_plasticity_perfect.e'
  detail = 'to solve a rate-independent problem with perfect plasticity;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_isoharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_isoharden'
  exodiff = 'rate_independent_plasticity_isoharden.e'
  detail = 'to solve a rate-independent problem with isotropic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_kinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_kinharden'
  exodiff = 'rate_independent_plasticity_kinharden.e'
  detail = 'to solve a rate-independent problem with kinematic hardening;'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[rate_independent_plasticity_isokinharden]
  type = Exodiff
  input = 'fem.i'
  cli_args = 'neml2_input=rate_independent_plasticity_isokinharden'
  exodiff = 'rate_independent_plasticity_isokinharden.e'
  detail = 'to solve a rate-independent problem with both isotropic and kinematic hardening.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  valgrind = heavy
[]

[batched]
  type = Exodiff
  prereq = 'neml2_legacy/viscoplasticity_isokinharden'
  input = 'fem.i'
  cli_args = 'neml2_input=viscoplasticity_isokinharden NEML2/mode=ALL'
  exodiff = 'viscoplasticity_isokinharden.e'
  detail = 'in a batched fashion.'
  required_submodule = 'contrib/neml2'
  libtorch = true
  recover = false
  valgrind = heavy
[]

[cmc_planar]
  type = 'CSVDiff'
  input = 'cmc_planar.i'
  csvdiff = 'cmc_planar.csv'
  heavy = true
  cli_args = 'Executioner/end_time=1 Postprocessors/active=s_zz'
  detail = 'unsmoothed capped-Mohr-Coulomb plasticity'
[]

[cmc_smooth]
  type = 'CSVDiff'
  input = 'cmc_smooth.i'
  csvdiff = 'cmc_smooth.csv'
  heavy = true
  cli_args = 'Executioner/end_time=1 Postprocessors/active=s_zz'
  detail = 'smoothed capped-Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al'
[]

[biaxial_planar]
  type = 'CSVDiff'
  input = 'biaxial_planar.i'
  csvdiff = 'biaxial_planar_out.csv'
  heavy = true
  # note, the number of residual calls for this test was documented in a published journal article.  To get no diffs when testing in parallel, various tolerances and settings must be set differently, resulting in a different number of residual calls.  Therefore, to keep the journal article correct, only test in serial.
  max_parallel = 1
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/strain=FINITE Executioner/end_time=1 Postprocessors/active=s_zz'
  detail = 'unsmoothed Mohr-Coulomb plasticity'
[]

[biaxial_abbo]
  type = 'CSVDiff'
  input = 'biaxial_abbo.i'
  csvdiff = 'biaxial_abbo.csv'
  heavy = true
  cli_args = 'Executioner/end_time=1 Postprocessors/active=s_zz'
  detail = 'smoothed Mohr-Coulomb plasticity, with smoothing performed by the Abbo et al method'
[]

[biaxial_smooth_cos]
  type = 'CSVDiff'
  input = 'biaxial_smooth.i'
  csvdiff = 'biaxial_smooth_cos.csv'
  heavy = true
  cli_args = 'Executioner/end_time=1 Materials/mc/smoother_function_type=cos Outputs/file_base=biaxial_smooth_cos Postprocessors/active=s_zz'
  detail = 'smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the cosine smoother'
[]

[biaxial_smooth_poly1]
  type = 'CSVDiff'
  input = 'biaxial_smooth.i'
  csvdiff = 'biaxial_smooth_poly1.csv'
  heavy = true
  cli_args = 'Executioner/end_time=1 Materials/mc/smoother_function_type=poly1 Outputs/file_base=biaxial_smooth_poly1 Postprocessors/active=s_zz'
  prereq = 'confined_uniaxial/biaxial_smooth_cos'
  detail = 'smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the poly1 smoother'
[]

[biaxial_smooth_poly2]
  type = 'CSVDiff'
  input = 'biaxial_smooth.i'
  csvdiff = 'biaxial_smooth_poly2.csv'
  heavy = true
  cli_args = 'Executioner/end_time=1 Materials/mc/smoother_function_type=poly2 Outputs/file_base=biaxial_smooth_poly2 Postprocessors/active=s_zz'
  prereq = 'confined_uniaxial/biaxial_smooth_poly1'
  detail = 'smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the poly2 smoother'
[]

[biaxial_smooth_poly3]
  type = 'CSVDiff'
  input = 'biaxial_smooth.i'
  csvdiff = 'biaxial_smooth_poly3.csv'
  heavy = true
  cli_args = 'Executioner/end_time=1 Materials/mc/smoother_function_type=poly3 Outputs/file_base=biaxial_smooth_poly3 Postprocessors/active=s_zz'
  prereq = 'confined_uniaxial/biaxial_smooth_poly2'
  detail = 'smoothed Mohr-Coulomb plasticity, with smoothing performed by the novel MOOSE smoothing method described in Wilkins et al, using the poly3 smoother'
[]

[./smallstrain_3D]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using small strain."
[../]

[./incrementalstrain_3D]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallstrain_3D'
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using incremental small strain."
[../]

[./finitestrain_3D]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=FINITE
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalstrain_3D'
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using finite strain."
[../]

[./smallstrain_RZ]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using small strain."
[../]

[./incrementalstrain_RZ]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallstrain_RZ'
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using incremental small strain."
[../]

[./finitestrain_RZ]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=FINITE
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalstrain_RZ'
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using finite strain."
[../]

[./smallplanestrain]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneSmallStrain
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using small strain."
[../]

[./incrementalplanestrain]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneIncrementalStrain
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallplanestrain'
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using incremental small strain."
[../]

[./finiteplanestrain]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneFiniteStrain
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalplanestrain'
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using finite strain."
[../]

[./smallstrain_spherical]
  type = 'PetscJacobianTester'
  input = 'jacobian_spherical.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL'
  ratio_tol = 2e-10
  difference_tol = 2e5
  requirement = "The mechanics system shall correctly compute the jacobian for spherical problems using small strain."
[../]

[./incrementalstrain_spherical]
  type = 'PetscJacobianTester'
  input = 'jacobian_spherical.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 2e-10
  difference_tol = 2e5
  requirement = "The mechanics system shall correctly compute the jacobian for spherical problems using small, incremental strain."
[../]

[./weak_plane_stress_elastic_jacobian]
  type = 'PetscJacobianTester'
  input = 'weak_plane_stress_elastic_jacobian.i'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = 'The system shall compute the correct Jacobian for plane stress conditions'
[../]

[./ad_weak_plane_stress_elastic_jacobian]
  type = 'PetscJacobianTester'
  input = 'ad_weak_plane_stress_elastic_jacobian.i'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = 'The system shall compute the correct Jacobian for plane stress conditions'
[../]

[./weak_plane_stress_small]
  type = 'Exodiff'
  input = 'weak_plane_stress_small.i'
  exodiff = 'weak_plane_stress_small_out.e'
  requirement = 'The system shall compute plane stress conditions with small strains with input provided using the Master action'
[../]

[./ad_weak_plane_stress_small]
  prereq = 'weak_plane_stress_small'
  type = 'Exodiff'
  input = 'ad_weak_plane_stress_small.i'
  exodiff = 'weak_plane_stress_small_out.e'
  requirement = 'The system shall compute plane stress conditions with small strains'
[../]

[./weak_plane_stress_incremental]
  type = 'Exodiff'
  input = 'weak_plane_stress_incremental.i'
  exodiff = 'weak_plane_stress_incremental_out.e'
  requirement = 'The system shall compute plane stress conditions with incremental strains with input provided using the Master action'
[../]

[./ad_weak_plane_stress_incremental]
  prereq = 'weak_plane_stress_incremental'
  type = 'Exodiff'
  input = 'ad_weak_plane_stress_incremental.i'
  exodiff = 'weak_plane_stress_incremental_out.e'
  requirement = 'The system shall compute plane stress conditions with incremental strains with input provided using the Master action'
[../]

[./weak_plane_stress_finite]
  type = 'Exodiff'
  input = 'weak_plane_stress_finite.i'
  exodiff = 'weak_plane_stress_finite_out.e'
  abs_zero = 1e-9
  requirement = 'The system shall compute plane stress conditions with finite strains with input provided using the Master action'
[../]

[./ad_weak_plane_stress_finite]
  prereq = 'weak_plane_stress_finite'
  type = 'Exodiff'
  input = 'ad_weak_plane_stress_finite.i'
  exodiff = 'weak_plane_stress_finite_out.e'
  abs_zero = 1e-9
  requirement = 'The system shall compute plane stress conditions with finite strains with input provided using the Master action'
[../]

[./3D_finite_tension_pull]
  type = 'CSVDiff'
  input = '3D_finite_tension_pull.i'
  csvdiff = '3D_finite_tension_pull_out.csv'
  requirement = 'The system shall compute the response of a 3D cube in uniaxial tension with finite strain to provide a benchmark for a 2D plane stress, finite strain model'
  max_parallel = 1 #Single element test
[../]

[./weak_plane_stress_finite_tension_pull]
  type = 'CSVDiff'
  input = 'weak_plane_stress_finite_tension_pull.i'
  csvdiff = 'weak_plane_stress_finite_tension_pull_out.csv'
  rel_err = 1e-4
  requirement = 'The system shall compute the response of a cube in uniaxial tension using a 2D plane stress, finite strain model, and produce the same result as a 3D model'
  max_parallel = 1 #Single element test
[../]

[zero]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_zero_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_zero_out Materials/porosity/negative_behavior=ZERO'
  detail = 'by setting the porosity to zero.'
[]

[initial]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_initial_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_initial_out Materials/porosity/negative_behavior=INITIAL_CONDITION'
  detail = 'by setting the porosity to the initial condition.'
[]

[exception]
  type = RunException
  input = 'negative_porosity.i'
  expect_err = 'porosity is negative'
  cli_args = 'Materials/porosity/negative_behavior=EXCEPTION'
  detail = 'by throwing an exception.'
[]

[zero]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_zero_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_zero_out Materials/porosity/negative_behavior=ZERO'
  detail = 'by setting the porosity to zero.'
[]

[initial]
  type = CSVDiff
  input = 'negative_porosity.i'
  csvdiff = 'negative_porosity_initial_out.csv'
  cli_args = 'Outputs/file_base=negative_porosity_initial_out Materials/porosity/negative_behavior=INITIAL_CONDITION'
  detail = 'by setting the porosity to the initial condition.'
[]

[exception]
  type = RunException
  input = 'negative_porosity.i'
  expect_err = 'porosity is negative'
  cli_args = 'Materials/porosity/negative_behavior=EXCEPTION'
  detail = 'by throwing an exception.'
[]

[./sideset_force]
  type = 'CSVDiff'
  input = 'sideset_reaction.i'
  csvdiff = 'sideset_reaction_out.csv'
  requirement = "The system shall be able to compute the force on a sideset."
  design = "SidesetReaction.md"
  issues = "#15163"
[../]

[material_tensor_avg_test]
  type = 'CSVDiff'
  input = 'material_tensor_average_test.i'
  csvdiff = 'material_tensor_average_test_out.csv'
  requirement = 'The system shall be able to compute the volume average of rank two tensor component.'
  design = 'MaterialTensorAverage.md'
  issues = '#15424'
[]

[material_tensor_avg_AD_test]
  type = 'CSVDiff'
  input = 'material_tensor_average_test.i'
  csvdiff = 'material_tensor_average_AD_test_out.csv'
  requirement = 'The system shall be able to compute the volume average of rank two tensor component, which was computed using automatic differentiation.'
  cli_args = 'Materials/stress/type=ADComputeFiniteStrainElasticStress Materials/elasticity_tensor/type=ADComputeElasticityTensor Physics/SolidMechanics/QuasiStatic/all/use_automatic_differentiation=true Outputs/file_base=material_tensor_average_AD_test_out Postprocessors/szz_avg/type=ADMaterialTensorAverage Postprocessors/szz_int/type=ADMaterialTensorIntegral'
  design = 'MaterialTensorAverage.md'
  issues = '#15424'
[]

[normal_displacement]
  type = 'Exodiff'
  input = 'normal_boundary_displacement.i'
  exodiff = 'normal_boundary_displacement_out.e'
  requirement = 'The system shall compute normal displacements on a surface for checking correct application of penalty boundary conditions.'
  design = 'NormalBoundaryDisplacement.md'
  issues = '#16346'
[]

[non]
  type = RunApp
  input = 'nonad_exception.i'
  detail = 'not using automatic differentiation methods.'
  allow_test_objects = true
  expect_out = 'Exceeded maximum iterations in material return mapping iterations.'
[]

[ad]
  type = RunApp
  input = 'ad_exception.i'
  detail = 'using automatic differentiation methods.'
  allow_test_objects = true
  expect_out = 'Exceeded maximum iterations in material return mapping iterations.'
[]

[with_reuse]
  type = CSVDiff
  input = convergence.i
  cli_args = "Executioner/reuse_preconditioner=true Outputs/csv/file_base=reuse_case"
  csvdiff = reuse_case.csv
  requirement = 'Preconditioner is reused until the linear iterations exceed the value of reuse_preconditioner_max_its upon which the system recalculates the preconditioner'
[]

[jacobian_3D_hex8]
  type = 'PetscJacobianTester'
  input = 'cantilever.i'
  run_sim = true
  difference_tol = 5e-3
  issues = '#19657'
  design = 'Pressure.md'
  requirement = "The Pressure boundary condition shall compute the correct Jacobian for a problem in 3D space using hex8 elements."
[]

[jacobian_3D_hex20]
  type = 'PetscJacobianTester'
  input = 'cantilever.i'
  run_sim = true
  cli_args = 'Mesh/MeshGenerator/elem_type=HEX20 GlobalParams/order=SECOND Outputs/file_base=cantilever_hex20_out'
  difference_tol = 0.5
  issues = '#19657'
  design = 'Pressure.md'
  requirement = "The Pressure boundary condition shall compute the correct Jacobian for a problem in 3D space using hex20 elements."
[]

[jacobian_RZ]
  type = 'PetscJacobianTester'
  input = 'ring.i'
  run_sim = true
  difference_tol = 5e-3
  issues = '#19657'
  design = 'Pressure.md'
  requirement = "The Pressure boundary condition shall compute the correct Jacobian for a problem in RZ coordinates with quad4 elements."
[]

[jacobian_RZ_quad8]
  type = 'PetscJacobianTester'
  input = 'ring.i'
  run_sim = true
  cli_args = 'Mesh/MeshGenerator/elem_type=QUAD8 GlobalParams/order=SECOND Outputs/file_base=ring_quad8_out'
  difference_tol = 0.5
  issues = '#19657'
  design = 'Pressure.md'
  requirement = "The Pressure boundary condition shall compute the correct Jacobian for a problem in RZ coordinates with quad8 elements."
[]

[./incstrn_pressure_spherical]
  type = 'PetscJacobianTester'
  input = 'jacobian_pressure_spherical.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 2e-10
  difference_tol = 2e5
  design = 'Pressure.md'
  requirement = "The mechanics system shall correctly compute the jacobian for spherical problems using small, incremental strain."
[../]

[./cylinder_2d_axisymmetric]
  type = 'Exodiff'
  input = 'cylinder_2d_axisymmetric.i'
  exodiff = 'cylinder_2d_axisymmetric_out.e'
  design = 'RadialDisplacementCylinderAux.md'
  requirement = 'The system shall compute the radial component of displacement for axisymmetric cylindrical models'
[../]

[./cylinder_2d_cartesian]
  type = 'Exodiff'
  input = 'cylinder_2d_cartesian.i'
  exodiff = 'cylinder_2d_cartesian_out.e'
  design = 'RadialDisplacementCylinderAux.md'
  requirement = 'The system shall compute the radial component of displacement for 2D Cartesian cylindrical models'
[../]

[./cylinder_3d_cartesian]
  type = 'Exodiff'
  input = 'cylinder_3d_cartesian.i'
  exodiff = 'cylinder_3d_cartesian_out.e'
  design = 'RadialDisplacementCylinderAux.md'
  requirement = 'The system shall compute the radial component of displacement for 3D Cartesian cylindrical models'
[../]

[./cylinder_2d_axisymmetric_except_1]
  type = 'RunException'
  input = 'cylinder_2d_axisymmetric.i'
  cli_args = "AuxKernels/raddispaux/axis_vector='0 0 1'"
  expect_err = "The 'axis_vector' parameter is only valid for 3D Cartesian models."
  prereq = cylinder_2d_axisymmetric
  design = 'RadialDisplacementCylinderAux.md'
  requirement = 'The system shall report an error if "axis_vector" is supplied to RadialDisplacementCylinderAux and the model is not 3D Cartesian'
[../]

[./cylinder_3d_cartesian_except_1]
  type = 'RunException'
  input = 'cylinder_3d_cartesian.i'
  cli_args = "AuxKernels/raddispaux/axis_vector='0 0 0'"
  expect_err = "axis_vector must have nonzero length"
  prereq = cylinder_3d_cartesian
  design = 'RadialDisplacementCylinderAux.md'
  requirement = 'The system shall report an error if "axis_vector" has length of zero'
[../]

[./sphere_1d_spherical]
  type = 'Exodiff'
  input = 'sphere_1d_spherical.i'
  exodiff = 'sphere_1d_spherical_out.e'
  design = 'RadialDisplacementSphereAux.md'
  requirement = 'The system shall compute the radial component of displacement for 1D spherical models'
[../]

[./sphere_2d_axisymmetric]
  type = 'Exodiff'
  input = 'sphere_2d_axisymmetric.i'
  exodiff = 'sphere_2d_axisymmetric_out.e'
  design = 'RadialDisplacementSphereAux.md'
  requirement = 'The system shall compute the radial component of displacement for axisymmetric spherical models'
[../]

[./sphere_3d_cartesian]
  type = 'Exodiff'
  input = 'sphere_3d_cartesian.i'
  exodiff = 'sphere_3d_cartesian_out.e'
  design = 'RadialDisplacementSphereAux.md'
  requirement = 'The system shall compute the radial component of displacement for 3D Cartesian spherical models'
[../]

[./sphere_1d_spherical_except_1]
  type = 'RunException'
  input = 'sphere_1d_spherical.i'
  cli_args = "AuxKernels/raddispaux/origin='0 0 0'"
  expect_err = "The 'origin' parameter is only valid for models with Cartesian or axisymmetric coordinate systems."
  prereq = sphere_1d_spherical
  design = 'RadialDisplacementSphereAux.md'
  requirement = 'The system shall report an error if "origin" is supplied to RadialDisplacementSphereAux when the coordinate system is not Cartesian or axisymmetric'
[../]

[linear_kinharden_nonsymmetric_strain_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = 'linear_kinharden_nonsymmetric_strain_controlled.i'
  csvdiff = 'linear_kinharden_nonsymmetric_strain_controlled_out.csv'
  requirement = 'The system shall compute the J2 linear kinematic plasticity stress based on the imposed cyclic nonsymmetric strain'
[]

[linear_kinharden_symmetric_strain_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = 'linear_kinharden_symmetric_strain_controlled.i'
  csvdiff = 'linear_kinharden_symmetric_strain_controlled_out.csv'
  requirement = 'The system shall compute the J2 linear kinematic plasticity stress based on the imposedcyclic symmetric strain'
[]

[nonlin_isoharden_symmetric_strain_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = 'nonlin_isoharden_symmetric_strain_controlled.i'
  csvdiff = 'nonlin_isoharden_symmetric_strain_controlled_out.csv'
  requirement = 'The system shall compute the J2 nonlinear isotropic plasticity stress based on the imposedcyclic symmetric strain'
[]

[nonlin_isokinharden_symmetric_strain_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = 'nonlin_isokinharden_symmetric_strain_controlled.i'
  csvdiff = 'nonlin_isokinharden_symmetric_strain_controlled_out.csv'
  requirement = 'The system shall compute the J2 nonlinear combined plasticity stress based on the imposed cyclic symmetric strain'
[]

[nonlin_kinharden_nonsymmetric_strain_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = 'nonlin_kinharden_nonsymmetric_strain_controlled.i'
  csvdiff = 'nonlin_kinharden_nonsymmetric_strain_controlled_out.csv'
  requirement = 'The system shall compute the J2 nonlinear kinematic plasticity stress based on the imposed cyclic nonsymmetric strain'
[]

[nonlin_kinharden_symmetric_strain_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = 'nonlin_kinharden_symmetric_strain_controlled.i'
  csvdiff = 'nonlin_kinharden_symmetric_strain_controlled_out.csv'
  requirement = 'The system shall compute the J2 nonlinear kinematic plasticity stress based on the imposed cyclic nonsymmetric strain'
[]

[1D_ratcheting_nonlin_kinharden_stress_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = '1D_ratcheting_nonlin_kinharden_stress_controlled.i'
  csvdiff = '1D_ratcheting_nonlin_kinharden_stress_controlled_out.csv'
  requirement = 'The system shall compute the J2 nonlinear kinematic plasticity strain based on the imposed cyclic nonsymmetric loading'
[]

[linear_kinharden_nonsymmetric_stress_controlled]
  type = CSVDiff
  rel_err = 1.0e-4
  input = 'linear_kinharden_nonsymmetric_stress_controlled.i'
  csvdiff = 'linear_kinharden_nonsymmetric_stress_controlled_out.csv'
  requirement = 'The system shall compute the J2 linear kinematic plasticity strain based on the imposed cyclic nonsymmetric loading'
[]

[isotropic_plasticity_incremental]
  type = Exodiff
  input = 'isotropic_plasticity_incremental_strain.i'
  exodiff = 'isotropic_plasticity_incremental_strain_out.e'
  compiler = 'CLANG GCC'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation.'
[]

[isotropic_plasticity_incremental_base_name]
  type = Exodiff
  input = 'isotropic_plasticity_incremental_strain.i'
  cli_args = "Materials/isotropic_plasticity/base_name=base
                Physics/SolidMechanics/QuasiStatic/all/generate_output=''"
  exodiff = 'isotropic_plasticity_incremental_strain_out.e'
  exodiff_opts = '-allow_name_mismatch'
  compiler = 'CLANG GCC'
  prereq = isotropic_plasticity_incremental
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation while prescribing a base name for the isotropic plasticity material properties.'
[]

[isotropic_plasticity_incremental_Bbar]
  type = Exodiff
  input = 'isotropic_plasticity_incremental_strain.i'
  exodiff = 'isotropic_plasticity_incremental_strain_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'isotropic_plasticity_incremental_base_name'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the small incremental strain formulation and using the b-bar element volume correction.'
[]

[isotropic_plasticity_finite]
  type = Exodiff
  input = 'isotropic_plasticity_finite_strain.i'
  exodiff = 'isotropic_plasticity_finite_strain_out.e'
  compiler = 'CLANG GCC'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation.'
[]

[isotropic_plasticity_finite_Bbar]
  type = Exodiff
  input = 'isotropic_plasticity_finite_strain.i'
  exodiff = 'isotropic_plasticity_finite_strain_out.e'
  compiler = 'CLANG GCC'
  cli_args = 'GlobalParams/volumetric_locking_correction=true'
  prereq = 'isotropic_plasticity_finite'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall compute the J2 isotropic plasticity stress and plastic strain response under tensile loading within the finite incremental strain formulation and using the b-bar element volume correction.'
[]

[isotropic_plasticity_error1]
  type = 'RunException'
  input = 'isotropic_plasticity_errors.i'
  cli_args = 'Materials/isotropic_plasticity/hardening_function=harden_func
                Materials/isotropic_plasticity/hardening_constant=2
                Materials/isotropic_plasticity/yield_stress=50
                Materials/elasticity_tensor/type=ComputeIsotropicElasticityTensor Materials/elasticity_tensor/youngs_modulus=2.1e5
                Materials/elasticity_tensor/poissons_ratio=0.0'
  expect_err = 'Only the hardening_constant or only the hardening_function can be defined but not both'
  design = 'IsotropicPlasticityStressUpdate.md'
  requirement = 'The system shall only allow the calculation of a J2 isotropic plasticity stress response with only one but not both of a hardening function or hardening constant specified to define the evolving yield surface.'
[]

[isotropic_plasticity_error2]
  type = 'RunException'
  input = 'isotropic_plasticity_errors.i'
  cli_args = 'Materials/isotropic_plasticity/yield_stress=50
                Materials/elasticity_tensor/type=ComputeIsotropicElasticityTensor Materials/elasticity_tensor/youngs_modulus=2.1e5
                Materials/elasticity_tensor/poissons_ratio=0.0'
  expect_err = 'Either hardening_constant or hardening_function must be defined'
  prereq = 'isotropic_plasticity_error1'
  design = 'IsotropicPlasticityStressUpdate.md'
  requirement = 'The system shall only calculate the J2 isotropic plasticity stress response when either a hardening function or a hardening constant is specified to define the evolving yield surface.'
[]

[isotropic_plasticity_error3]
  type = 'RunException'
  input = 'isotropic_plasticity_errors.i'
  cli_args = 'Materials/isotropic_plasticity/hardening_function=harden_func
                Materials/elasticity_tensor/type=ComputeIsotropicElasticityTensor Materials/elasticity_tensor/youngs_modulus=2.1e5
                Materials/elasticity_tensor/poissons_ratio=0.0'
  expect_err = 'Either yield_stress or yield_stress_function must be given'
  prereq = 'isotropic_plasticity_error2'
  design = 'IsotropicPlasticityStressUpdate.md'
  requirement = 'The system shall only calculate the J2 isotropic plasticity stress response when either a constant yield stress or a yield stress function is specified to define the initial yield surface.'
[]

[isotropic_plasticity_error4]
  type = 'RunException'
  input = 'isotropic_plasticity_errors.i'
  cli_args = 'Materials/isotropic_plasticity/hardening_function=harden_func
                Materials/elasticity_tensor/type=ComputeIsotropicElasticityTensor Materials/elasticity_tensor/youngs_modulus=2.1e5
                Materials/elasticity_tensor/poissons_ratio=0.0
                Materials/isotropic_plasticity/yield_stress=-5.0'
  expect_err = 'Yield stress must be greater than zero'
  prereq = 'isotropic_plasticity_error3'
  design = 'IsotropicPlasticityStressUpdate.md'
  requirement = 'The system shall return an error if a negative yield stress is supplied when calculating the J2 isotropic plasticity stress response.'
[]

[isotropic_plasticity_error5]
  type = 'RunException'
  input = 'isotropic_plasticity_errors.i'
  cli_args = 'Materials/isotropic_plasticity/hardening_function=harden_func
                Materials/isotropic_plasticity/yield_stress=50
                Materials/elasticity_tensor/type=ComputeElasticityTensor Materials/elasticity_tensor/fill_method=symmetric21
                Materials/elasticity_tensor/C_ijkl="1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21" '
  expect_err = 'Model isotropic_plasticity requires an isotropic elasticity tensor, but the one supplied is not guaranteed isotropic'
  prereq = 'isotropic_plasticity_error4'
  design = 'IsotropicPlasticityStressUpdate.md'
  requirement = 'The system shall return an error if anisotropic elasticity tensor is supplied when the J2 isotropic plasticity stress response calculation is requested.'
[]

[affine_plasticity]
  type = Exodiff
  input = 'affine_plasticity.i'
  exodiff = 'affine_plasticity_out.e'
  custom_cmp = 'affine_plasticity.exodiff'
  design = 'IsotropicPlasticityStressUpdate.md ComputeMultipleInelasticStress.md'
  requirement = 'The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213.'
[]

[cp_affine_plasticity]
  type = Exodiff
  input = 'cp_affine_plasticity.i'
  exodiff = 'cp_affine_plasticity_out.e'
  custom_cmp = 'affine_plasticity.exodiff'
  design = 'IsotropicPlasticityStressUpdate.md ComputeCreepPlasticityStress.md'
  requirement = 'The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213. This shall be done with a coupled creep and plasticity model where the creep model is inactive.'
[]

[uniaxial_viscoplasticity]
  type = Exodiff
  input = 'uniaxial_viscoplasticity_incrementalstrain.i'
  exodiff = 'uniaxial_viscoplasticity_incrementalstrain_out.e'
  compiler = 'CLANG GCC'
  design = 'HyperbolicViscoplasticityStressUpdate.md'
  requirement = 'The system shall compute the hyperbolic visoplastic stress response for a time-dependent linear strain hardening plasticity model in a small incremental strain formulation in a manner equivalent to the ABAQUS result.'
[]

[cp_affine_plasticity]
  type = Exodiff
  input = 'cp_affine_plasticity.i'
  exodiff = 'cp_affine_plasticity_out.e'
  custom_cmp = 'affine_plasticity.exodiff'
  design = 'IsotropicPlasticityStressUpdate.md ComputeCreepPlasticityStress.md'
  requirement = 'The system shall calculate, with J2 isotropic plasticity, the transient stress eigenvalues with stationary eigenvectors verification test from K. Jamojjala, R. Brannon, A. Sadeghirad, J. Guilkey, Verification tests in solid mechanics, Engineering with Computers, Vol 31., p. 193-213. This shall be done with a coupled creep and plasticity model where the creep model is inactive.'
[]

[3tile_strain]
  type = 'CSVDiff'
  input = '3tile_strain.i'
  csvdiff = '3tile_strain_out.csv'
  cli_args = 'Materials/rom_stress_prediction/finite_difference_width=1e-2'
  detail = 'and evolve over time with an good finite difference width.'
  petsc_version = '>=3.9.0'
  allow_test_objects = true
[]

[3tile_strain_small_fd]
  type = 'CSVDiff'
  input = '3tile_strain.i'
  csvdiff = '3tile_strain_small_fd_out.csv'
  cli_args = 'Outputs/file_base=3tile_strain_small_fd_out Materials/rom_stress_prediction/finite_difference_width=1e-20'
  detail = 'and evolve over time with an poor finite difference width with more nonlinear iterations than with a good finite difference width.'
  petsc_version = '>=3.9.0'
  allow_test_objects = true
[]

[3d_MPA]
  type = 'CSVDiff'
  prereq = 'rom/3d'
  input = '3d.i'
  cli_args = 'stress_unit=MPa E=3.3e5 p=1e-1'
  csvdiff = '3d_out.csv'
  detail = 'with units of stress other than Pascal.'
  allow_test_objects = true
[]

[nonad_verification]
  type = 'CSVDiff'
  input = 'nonad_verification.i'
  csvdiff = 'nonad_verification_out.csv'
  petsc_version = '>=3.9.0'
  max_parallel = 1
  allow_test_objects = true
  detail = 'in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a small set of input parameters not using AD.'
[]

[nonad_verification_heavy]
  type = 'CSVDiff'
  input = 'nonad_verification.i'
  csvdiff = 'nonad_verification_heavy_out.csv'
  heavy = true
  max_time = 500
  petsc_version = '>=3.9.0'
  cli_args = 'Executioner/dt=1e-5 Outputs/file_base=nonad_verification_heavy_out Outputs/interval=100'
  max_parallel = 1
  allow_test_objects = true
  detail = 'in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a large set of input parameters not using AD.'
[]

[lower_limit_extrapolated]
  type = 'CSVDiff'
  input = lower_limit.i
  csvdiff = extrapolated_out.csv
  cli_args = 'temp=500 disp=0.5e6 Outputs/file_base=extrapolated_out'
  allow_test_objects = true
  detail = 'below the lower temperature limit and extrapolate correctly.'
[]

[lower_limit_error]
  type = 'RunException'
  input = lower_limit.i
  expect_err = "In rom_stress_prediction: temperature input parameter with value \(500\) is out of lower global range"
  cli_args = 'temp=500 disp=0.5e6 Materials/rom_stress_prediction/temperature_input_window_low_failure=ERROR'
  allow_test_objects = true
  detail = 'but should error out below the lower temperature limit if requested by the user.'
[]

[upper_limit_error]
  type = 'RunException'
  input = lower_limit.i
  expect_err = "In rom_stress_prediction: temperature input parameter with value \(2500\) is out of upper global range"
  cli_args = 'temp=2500 disp=0.5e6 Materials/rom_stress_prediction/temperature_input_window_low_failure=ERROR'
  allow_test_objects = true
  detail = 'but should error out above the upper temperature limit if requested by the user.'
[]

[creep_ramp_sub_false]
  type = 'CSVDiff'
  input = creep_ramp_sub_false.i
  csvdiff = creep_ramp_sub_false_out.csv
  allow_test_objects = true
  detail = 'when substepping is off and the time step size does not guarantee the most accurate results.'
[]

[creep_ramp_sub_false_more_steps]
  type = 'CSVDiff'
  input = creep_ramp_sub_false_more_steps.i
  csvdiff = creep_ramp_sub_false_more_steps_out.csv
  allow_test_objects = true
  detail = 'when substepping is off and the time step size guarantees accurate results.'
[]

[creep_ramp_sub_true]
  type = 'CSVDiff'
  input = creep_ramp_sub_true.i
  csvdiff = creep_ramp_sub_true_out.csv
  allow_test_objects = true
  allow_warnings = true
  detail = 'when substepping is on and the numerical integration error selected by the user guarantees accurate results.'
[]

[creep_ramp_sub_true_exception]
  type = 'RunApp'
  input = creep_ramp_sub_true.i
  expect_out = "The number of substeps computed exceeds 'maximum_number_substeps'"
  cli_args = 'Materials/rom_stress_prediction/substep_strain_tolerance=5.0e-6'
  allow_test_objects = true
  allow_warnings = true
  detail = 'when substepping is on and the numerical integration error selected by the user guarantees accurate results but substepping settings require a system-wise time step cut because the computed number of substeps exceeds the maximum_number_substeps parameter.'
[]

[3tile]
  type = 'CSVDiff'
  input = '3tile.i'
  csvdiff = '3tile_out.csv'
  detail = 'for a variety of overlapping tiles and two overlapping partitions.'
  petsc_version = '>=3.9.0'
  allow_test_objects = true
[]

[3tile_json]
  type = 'CSVDiff'
  input = '3tile_json.i'
  csvdiff = '3tile_json_out.csv'
  detail = 'for a variety of overlapping tiles and two overlapping partitions with a model loaded from a JSON data file.'
  petsc_version = '>=3.9.0'
[]

[3tile_json_relative]
  type = 'CSVDiff'
  input = '3tile_json.i'
  csvdiff = '3tile_json_out.csv'
  cli_args = 'Materials/rom_stress_prediction/model=gold/3tile_json_export.json'
  detail = 'for a variety of overlapping tiles and two overlapping partitions with a model loaded from a JSON data file relative to the input.'
  petsc_version = '>=3.9.0'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[3tile_json_export]
  type = 'JSONDiff'
  input = '3tile.i'
  jsondiff = '3tile_json_export.json'
  detail = 'for a variety of overlapping tiles and two overlapping partitions, and be able to export the model data to a JSON file.'
  petsc_version = '>=3.9.0'
  cli_args = 'Materials/rom_stress_prediction/export_model=3tile_json_export.json'
  allow_test_objects = true
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[3d_MPA]
  type = 'CSVDiff'
  prereq = 'rom/3d'
  input = 'AD3d.i'
  cli_args = 'stress_unit=MPa E=3.3e5 p=1e-1 Outputs/file_base=3d_out'
  csvdiff = '3d_out.csv'
  detail = 'with units of stress other than Pascal.'
  allow_test_objects = true
[]

[3d-jac]
  type = 'PetscJacobianTester'
  input = 'AD3d.i'
  prereq = 'ADrom/3d'
  ratio_tol = 5e-7
  method = 'opt'
  cli_args = 'Executioner/num_steps=2'
  difference_tol = 1
  run_sim = True
  detail = 'in 3D and compute a perfect Jacobian.'
  allow_test_objects = true
[]

[2drz]
  type = 'CSVDiff'
  input = 'AD2drz.i'
  csvdiff = '2drz_out.csv'
  cli_args = 'Outputs/file_base=2drz_out'
  detail = 'in 2DRz.'
  petsc_version = '>=3.9.0'
  allow_test_objects = true
[]

[2drz-jac]
  type = 'PetscJacobianTester'
  input = 'AD2drz.i'
  method = 'opt'
  prereq = 'ADrom/2drz'
  ratio_tol = 5e-7
  difference_tol = 1
  cli_args = 'Executioner/num_steps=2'
  run_sim = True
  detail = 'in 2DRz and compute a perfect Jacobian.'
  allow_test_objects = true
[]

[ad_verification]
  type = 'CSVDiff'
  input = 'ad_verification.i'
  csvdiff = 'ad_verification_out.csv'
  petsc_version = '>=3.9.0'
  max_parallel = 1
  allow_test_objects = true
  detail = 'in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a small set of input parameters using AD.'
[]

[ad_verification_heavy]
  type = 'CSVDiff'
  input = 'ad_verification.i'
  csvdiff = 'ad_verification_heavy_out.csv'
  heavy = true
  max_time = 500
  petsc_version = '>=3.9.0'
  cli_args = 'Executioner/dt=1e-5 Outputs/file_base=ad_verification_heavy_out Outputs/interval=100'
  max_parallel = 1
  allow_test_objects = true
  detail = 'in isolation (i.e. without a full displacement solve), and match with code-to-code comparison with a large set of input parameters using AD.'
[]

[lower_limit]
  type = 'CSVDiff'
  input = ADlower_limit.i
  csvdiff = lower_limit_out.csv
  cli_args = 'Outputs/file_base=lower_limit_out'
  allow_test_objects = true
  detail = 'at the lower temperature limit.'
[]

[lower_limit_extrapolated]
  type = 'CSVDiff'
  input = ADlower_limit.i
  csvdiff = extrapolated_out.csv
  cli_args = 'temp=500 disp=0.5e6 Outputs/file_base=extrapolated_out'
  allow_test_objects = true
  detail = 'below the lower temperature limit and extrapolate correctly.'
[]

[scalar_damage_material]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  csvdiff = 'scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material."
[]

[ad_scalar_damage_material]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  csvdiff = 'ad_scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation."
[]

[scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=scalar_material_damage_old_out'
  csvdiff = 'scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index."
[]

[ad_scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=ad_scalar_material_damage_old_out'
  csvdiff = 'ad_scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index when using automatic differentiation."
[]

[scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1."
[]

[ad_scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1 also when using automatic differentiation."
[]

[scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress"
[]

[ad_scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation"
[]

[combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  csvdiff = 'combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models."
[]

[combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=combined_scalar_damage_mult_out'
  csvdiff = 'combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models."
[]

[combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_sub_out'
  csvdiff = 'combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model"
[]

[combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_combined_out'
  csvdiff = 'combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models."
[]

[ad_combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  csvdiff = 'ad_combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=ad_combined_scalar_damage_mult_out'
  csvdiff = 'ad_combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_sub_out'
  csvdiff = 'ad_combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_combined_out'
  csvdiff = 'ad_combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation."
[]

[scalar_damage_material_inelastic]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep.i'
  csvdiff = 'scalar_material_damage_creep_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation."
[]

[scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep_power.i'
  csvdiff = 'scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation."
[]

[ad_scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage_creep_power.i'
  csvdiff = 'ad_scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation."
[]

[multiple_inelastic_bad_damage_model]
  type = RunException
  input = ad_scalar_material_damage_creep_power.i
  expect_err = "Damage Model.*damage_index.*is not compatible with ADComputeMultipleInelasticStress"
  requirement = "The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object."
  issues = '#20722'
  cli_args = 'Materials/stress/damage_model=damage_index'
  allow_warnings = True
[]

[nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'nonlocal_scalar_damage.i'
  csvdiff = 'nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model."
  issues = '#21786'
[]

[ad_nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'ad_nonlocal_scalar_damage.i'
  csvdiff = 'ad_nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation."
  issues = '#21786'
[]

[scalar_damage_material]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  csvdiff = 'scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material."
[]

[ad_scalar_damage_material]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  csvdiff = 'ad_scalar_material_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a elastic material when using automatic differentiation."
[]

[scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=scalar_material_damage_old_out'
  csvdiff = 'scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index."
[]

[ad_scalar_damage_material_old]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/damage/use_old_damage=true Outputs/file_base=ad_scalar_material_damage_old_out'
  csvdiff = 'ad_scalar_material_damage_old_out.csv'
  requirement = "The system shall calculate damaged stress based on old damage index when using automatic differentiation."
[]

[scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1."
[]

[ad_scalar_damage_material_out_of_bounds]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Executioner/end_time=1.2'
  expect_err = 'damage_index must be between 0 and 1. Current value is:'
  requirement = "The system shall report an error when damage index is greater than 1 also when using automatic differentiation."
[]

[scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = scalar_damage_material
  input = 'scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress"
[]

[ad_scalar_damage_incompatible_model]
  type = 'RunException'
  prereq = ad_scalar_damage_material
  input = 'ad_scalar_material_damage.i'
  cli_args = 'Materials/stress/damage_model=damage_index' #Point it to an incompatible model
  expect_err = 'Damage Model damage_index is not compatible with ComputeDamageStress'
  allow_warnings = true #Avoid failing on another warning before hitting the error we're testing for
  requirement = "The system shall make sure that the damage model is derived from DamageBase and error out when incompatible damage model is used in conjunction with ComputeDamageStress when using automatic differentiation"
[]

[combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  csvdiff = 'combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models."
[]

[combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=combined_scalar_damage_mult_out'
  csvdiff = 'combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models."
[]

[combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_sub_out'
  csvdiff = 'combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model"
[]

[combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=combined_scalar_damage_limit_combined_out'
  csvdiff = 'combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models."
[]

[ad_combined_scalar_damage_max]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  csvdiff = 'ad_combined_scalar_damage_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the maximum value of the damage index comparing different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_mult]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/combination_type=Product Outputs/file_base=ad_combined_scalar_damage_mult_out'
  csvdiff = 'ad_combined_scalar_damage_mult_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effective damage index from different damage models when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_sub]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage_a/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_sub_out'
  csvdiff = 'ad_combined_scalar_damage_limit_sub_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for an individual damage model that is combined with another damage model when using automatic differentiation."
[]

[ad_combined_scalar_damage_limit_combined]
  type = 'CSVDiff'
  input = 'ad_combined_scalar_damage.i'
  cli_args = 'Materials/damage/maximum_damage=0.8 Outputs/file_base=ad_combined_scalar_damage_limit_combined_out'
  csvdiff = 'ad_combined_scalar_damage_limit_combined_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall allow for damage to be limited to a user-defined value for the combination of multiple damage models when using automatic differentiation."
[]

[scalar_damage_material_inelastic]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep.i'
  csvdiff = 'scalar_material_damage_creep_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the creep or plastic deformation."
[]

[scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'scalar_material_damage_creep_power.i'
  csvdiff = 'scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation."
[]

[ad_scalar_damage_material_creep_power]
  type = 'CSVDiff'
  input = 'ad_scalar_material_damage_creep_power.i'
  csvdiff = 'ad_scalar_material_damage_creep_power_out.csv'
  abs_zero = 1.e-6
  requirement = "The system shall calculate the effect of damage on the stress of a inelastic material in conjunction with the power law creep deformation with automatic differentiation."
[]

[multiple_inelastic_bad_damage_model]
  type = RunException
  input = ad_scalar_material_damage_creep_power.i
  expect_err = "Damage Model.*damage_index.*is not compatible with ADComputeMultipleInelasticStress"
  requirement = "The system shall provide a meaningful error if the user selects a material model that is not recognized by the automatic differentiation multiple stress object."
  issues = '#20722'
  cli_args = 'Materials/stress/damage_model=damage_index'
  allow_warnings = True
[]

[nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'nonlocal_scalar_damage.i'
  csvdiff = 'nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model."
  issues = '#21786'
[]

[ad_nonlocal_damage_model]
  type = 'CSVDiff'
  input = 'ad_nonlocal_scalar_damage.i'
  csvdiff = 'ad_nonlocal_scalar_damage_out.csv'
  abs_zero = 1.e-6
  recover = false
  requirement = "The system shall calculate the effect of damage on the stress of a nonlocal damage model. When using automatic differentiation."
  issues = '#21786'
[]

[shell_dynamics_bending_moment_free]
  type = 'CSVDiff'
  input = 'shell_dynamics_bending_moment_free.i'
  csvdiff = 'shell_dynamics_bending_moment_free_out.csv'
  detail = "the surface is on the XY plane"
  heavy = true
[]

[shell_dynamics_bending_moment_free_orientation_inclined]
  type = 'CSVDiff'
  input = 'shell_dynamics_bending_moment_free_orientation_inclined.i'
  csvdiff = 'shell_dynamics_bending_moment_free_orientation_inclined_out.csv'
  detail = "the surface is at a 45 deg. angle w.r.t. the Y axis"
  heavy = true
[]

[shell_dynamics_bending_moment_free_orientation_inclined_hht]
  type = 'CSVDiff'
  input = 'shell_dynamics_bending_moment_free_orientation_inclined_hht.i'
  csvdiff = 'shell_dynamics_bending_moment_free_orientation_inclined_hht_out.csv'
  detail = "the surface is at a 45 deg. angle w.r.t. the Y axis and HHT input is provided"
  heavy = true
[]

[beam_bending]
  type = 'Exodiff'
  input = 'beam_bending_moment_AD.i'
  exodiff = 'beam_bending_moment_AD_out.e'

  requirement = "The mechanics system shall accurately compute the deflection of a cantilever beam when it is modeled using shell elements."
[]

[rotated_beam_bending]
  type = 'Exodiff'
  input = 'beam_bending_moment_AD_2.i'
  exodiff = 'beam_bending_moment_AD_2_out.e'

  requirement = "The mechanics system shall accurately compute the deflection of a rotated cantilever beam when it is modeled using shell elements."
[]

[large_beam_bending]
  type = 'Exodiff'
  input = 'large_strain_m_40_AD.i'
  exodiff = 'large_strain_m_40_AD_out.e'
  petsc_version = '>=3.9.0'
  requirement = "The mechanics system shall accurately compute the deflection of a cantilever beam when it is modeled using shell elements under large strain and rotations are included."
[]

[beam_bending_jacobian]
  type = 'PetscJacobianTester'
  input = 'beam_bending_moment_AD.i'

  requirement = "The mechanics system shall accurately compute the Jacobian for a small strain quasi-static shell element."
[]

[large_beam_bending_jacobian]
  type = 'PetscJacobianTester'
  input = 'large_strain_m_40_AD.i'
  cli_args = 'Executioner/num_steps=1'
  petsc_version = '>=3.9.0'
  requirement = "The mechanics system shall accurately compute the Jacobian for a large strain quasi-static shell element."
[]

[plate_bending]
  type = 'Exodiff'
  input = 'plate_bending.i'
  exodiff = 'plate_bending_out.e'
  heavy = true

  requirement = "The mechanics system shall accurately model the deflection of a simply supported under uniform loading."
[]

[plate_bending2]
  type = 'Exodiff'
  input = plate_bending2.i
  exodiff = 'plate_bending2_out.e'

  requirement = "The mechanics system shall accurately model deflection of a plate with multiple force and moment boundary conditions."
[]

[pinched_cylinder]
  type = 'CSVDiff'
  input = pinched_cylinder_symm.i
  csvdiff = 'pinched_cylinder_symm_out.csv'
  requirement = "The mechanics system shall converge to the analytic displacement of a cylinder modeled with shell elements, with point loading applied in the x direction."
[]

[pinched_cylinder_y]
  type = 'CSVDiff'
  input = pinched_cylinder_symm.i
  cli_args = "DiracKernels/point/variable=disp_y DiracKernels/point/point='0 1 1' Outputs/file_base=pinched_cylinder_symm_y_out"
  csvdiff = 'pinched_cylinder_symm_y_out.csv'
  requirement = "The mechanics system shall converge to the analytic displacement of a cylinder modeled with shell elements, with point loading applied in the y direction."
[]

[inclined_plane]
  type = 'Exodiff'
  input = inclined_straintest.i
  exodiff = 'inclined_straintest_out.e'

  requirement = "The mechanics system shall accurately model the deflection of a inclined shell elements."
[]

[straintest_axial]
  type = 'Exodiff'
  input = straintest.i
  exodiff = 'straintest_out.e'

  requirement = "The mechanics system shall accurately compute the axial stress and strain of the shell elements."
[]

[finite_straintest_axial]
  type = 'Exodiff'
  input = finite_straintest.i
  exodiff = 'finite_straintest_out.e'

  issues = '#25266'

  requirement = "The mechanics system shall accurately compute the axial stress and strain of the shell elements using the finite strain formulation."
[]

[straintest_shear]
  type = 'Exodiff'
  input = straintest_shear.i
  exodiff = 'straintest_shear_out.e'

  requirement = "The mechanics system shall accurately compute the stress and strain of the shell elements subjected to shear deformation."
[]

[tapered]
  type = 'Exodiff'
  input = tapered.i
  exodiff = 'tapered_out.e'

  requirement = "The mechanics system shall accurately compute the stress and strain of the tapered shell elements."
[]

[qp_error]
  type = 'RunException'
  input = pressure_error.i
  expect_err = 'Shell element needs to have exactly four quadrature points.'

  requirement = "The system shall generate an error if the shell strain material is evaluated when the number of quadrature points does not equal 4."
[]

[pinched_cylinder_symm_unstructured]
  type = 'Exodiff'
  input = pinched_cylinder_symm_unstructured.i
  exodiff = 'pinched_cylinder_symm_unstructured_out.e'

  requirement = "Shell elements should have compatible stresses even for unstructured meshes."
[]

[shell_dynamics]
  type = 'CSVDiff'
  input = 'shell_dynamics_bending_moment.i'
  cli_args = 'Executioner/num_steps=5'
  csvdiff = 'shell_dynamics_bending_moment_out.csv'
  design = "ADInertialForceShell.md"
  requirement = "The mechanics system shall accurately predict the dynamic behavior of a shell element."
  issues = "#15067"
[]

[cracking]
  type = Exodiff
  input = cracking.i
  allow_warnings = true #Ignore warning about missing cracked_elasticity_type
  exodiff = cracking_out.e
  custom_cmp = cracking.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in cartesian coordinates.'
[]

[cracking_rz]
  type = Exodiff
  input = cracking_rz.i
  exodiff = cracking_rz_out.e
  custom_cmp = cracking_rz.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate cracking on a specimen under tension in rz coordinates.'
[]

[cracking_function]
  type = Exodiff
  input = cracking_function.i
  exodiff = cracking_function_out.e
  custom_cmp = cracking_function.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate cracking while the cracking strength is prescribed by an elemental AuxVariable.'
[]

[exponential]
  type = Exodiff
  input = cracking_exponential.i
  exodiff = cracking_exponential_out.e
  custom_cmp = cracking_exponential.cmp
  use_old_floor = true
  requirement = 'The MOOSE SolidMechanics module shall simulate exponential stress release.'
[]

[rz_exponential]
  type = Exodiff
  input = cracking_rz_exponential.i
  exodiff = cracking_rz_exponential_out.e
  custom_cmp = cracking_rz_exp.cmp
  exodiff_opts = '-steps 0:1200:1'
  requirement = 'The MOOSE SolidMechanics module shall simulate exponential stress relase while using the rz coordinate system.'
[]

[power]
  type = Exodiff
  input = cracking_power.i
  exodiff = cracking_power_out.e
  requirement = 'The MOOSE SolidMechanics module shall demonstrate softening using the power law for smeared cracking.'
[]

[multiple_softening]
  type = Exodiff
  input = cracking_multiple_softening.i
  exodiff = cracking_multiple_softening_out.e
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the prescribed softening laws in three directions, power law (x), exponential (y), and abrupt (z).'
[]

[xyz]
  type = Exodiff
  input = cracking_xyz.i
  exodiff = cracking_xyz_out.e
  use_old_floor = true
  custom_cmp = cracking_xyz.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate smeared cracking in the x y and z directions.'
[]

[plane_stress]
  type = Exodiff
  input = cracking_plane_stress.i
  exodiff = cracking_plane_stress_out.e
  use_old_floor = true
  custom_cmp = cracking_pln_str.cmp
  requirement = 'The MOOSE SolidMechanics module shall simulate smeared cracking under plane stress conditions.'
[]

[cracking_rotation]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  max_parallel = 1
  requirement = 'The MOOSE SolidMechanics module shall demonstrate that the smeared cracking model correctly handles finite rotation of cracked elements.'
[]

[cracking_rotation_pres_dir_x]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  #Prescribe the first crack to be in x (which doesn't crack), and reorder crack_flags to match original case
  cli_args = 'Materials/cracking_stress/prescribed_crack_directions=x AuxKernels/crack_flags3/component=1 AuxKernels/crack_flags2/component=2'
  max_parallel = 1
  prereq = cracking_rotation
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in x.'
[]

[cracking_rotation_pres_dir_z]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  #Prescribe the first crack to be in z (which doesn't crack), and reorder crack_flags to match original case
  cli_args = 'Materials/cracking_stress/prescribed_crack_directions=z AuxKernels/crack_flags3/component=1 AuxKernels/crack_flags2/component=2'
  max_parallel = 1
  prereq = cracking_rotation_pres_dir_x
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where the crack is prescribed in z.'
[]

[cracking_rotation_pres_dir_xz]
  type = Exodiff
  input = cracking_rotation.i
  exodiff = cracking_rotation_out.e
  use_old_floor = true
  custom_cmp = cracking_rotation.cmp
  #Prescribe the first two cracks to be in x and z (which dosn't crack), and reorder crack_flags to match original case
  cli_args = "Materials/cracking_stress/prescribed_crack_directions='x z' AuxKernels/crack_flags3/component=0 AuxKernels/crack_flags2/component=1 AuxKernels/crack_flags1/component=2"
  max_parallel = 1
  prereq = cracking_rotation_pres_dir_z
  requirement = 'The MOOSE SolidMechanics module shall demonstrate the finite rotation of cracked elements where two cracks are prescribed in x and z.'
[]

[cracking_err_diagonal]
  prereq = cracking
  type = RunException
  input = cracking.i
  expect_err = "Defaulting to the legacy option of 'DIAGONAL', but the 'FULL' option is preferred"
  requirement = "The ComputeSmearedCrackingStress model shall generate a warning if 'cracked_elasticity_type' is not specified"
[]

[cracking_err_softening]
  prereq = cracking_err_diagonal
  allow_warnings = true #Ignore warning about missing cracked_elasticity_type
  type = RunException
  input = cracking.i
  cli_args = "Materials/elastic_stress/softening_models='abrupt_softening abrupt_softening'"
  expect_err = "Either 1 or 3 softening models must be specified"
  requirement = "The ComputeSmearedCrackingStress model shall generate an error if an invalid number of softening models is specified"
[]

[incr_elas]
  type = 'CSVDiff'
  input = 'incr_model.i'
  csvdiff = 'incr_model_out.csv'
  rel_err = 1e-6
  abs_zero = 1e-8
  design = 'StrainEnergyDensity.md'
  requirement = 'The system shall be capable of calculating strain energy density incrementally in materials with elastic stress and finite strain.'
[]

[incr_chk1]
  type = 'RunException'
  input = 'incr_model.i'
  cli_args = 'Materials/strain_energy_density/incremental=false'
  design = 'StrainEnergyDensity.md'
  expect_err = 'StrainEnergyDensity: Specified incremental = false, but material model is incremental.'
  requirement = 'The system shall be capable of informing a user when they incorrectly choose not to use the incremental strain energy density formulation with an incremental material model.'
[]

[tot_elas]
  type = 'CSVDiff'
  input = 'tot_model.i'
  csvdiff = 'tot_model_out.csv'
  rel_err = 1e-6
  design = 'StrainEnergyDensity.md'
  requirement = 'The system shall be capable of calculating strain energy density for materials with elastic stress and small strain.'
[]

[tot_chk1]
  type = 'RunException'
  input = 'tot_model.i'
  cli_args = 'Materials/strain_energy_density/incremental=true'
  design = 'StrainEnergyDensity.md'
  expect_err = "StrainEnergyDensity: Specified incremental = true, but material model is not incremental."
  requirement = 'The system shall be capable of informing a user when they incorrectly choose to use the incremental strain energy density formulation in a material utilizing small strain.'
[]

[incr_elas_plas]
  type = 'CSVDiff'
  input = 'incr_model_elas_plas.i'
  csvdiff = 'incr_model_elas_plas_out.csv'
  rel_err = 1e-6
  design = 'StrainEnergyDensity.md'
  requirement = 'The system shall be capable of calculating strain energy density incrementally in materials with inelastic stress and isotropic plasticity.'
[]

[tot_elas_stress_name]
  type = 'CSVDiff'
  issues = '#25202'
  input = 'tot_model_stress_name.i'
  csvdiff = 'tot_model_stress_name_out.csv'
  rel_err = 1e-6
  design = 'StrainEnergyDensity.md'
  requirement = 'The system shall be capable of calculating strain energy density for materials with a user-specified stress by name and small strain.'
[]

[incr_model_sensitivity]
  type = 'Exodiff'
  input = 'incr_model_sensitivity.i'
  exodiff = 'incr_model_sensitivity_out.e'
  design = 'ComplianceSensitivity.md'
  abs_zero = 1.0e-6
  requirement = 'The system shall be able to create a compliance sensitivity material.'
[]

[rate_model]
  type = 'CSVDiff'
  input = 'rate_model.i'
  csvdiff = 'rate_model_out.csv'
  rel_err = 1e-6
  abs_zero = 1e-8
  design = 'StrainEnergyRateDensity.md'
  requirement = 'The system shall be capable of calculating strain energy rate density with elastic stress and finite strain.'
[]

[rate_model_small]
  type = 'CSVDiff'
  input = 'rate_model_small.i'
  csvdiff = 'rate_model_small_out.csv'
  rel_err = 1e-6
  design = 'StrainEnergyRateDensity.md'
  requirement = 'The system shall be capable of calculating strain energy rate density when using small strain assumptions.'
[]

[ad_rate_model_weak_plane]
  type = 'CSVDiff'
  input = 'ad_rate_model_weak_plane.i'
  csvdiff = 'ad_rate_model_weak_plane_out.csv'
  rel_err = 1e-6
  abs_zero = 1e-8
  design = 'StrainEnergyRateDensity.md'
  requirement = 'The system shall be capable of calculating strain energy rate density when using automatic differentiation and weak plane stress.'
[]

[nonAD_rate_model_weak_plane]
  type = 'CSVDiff'
  input = 'nonAD_rate_model_weak_plane.i'
  csvdiff = 'nonAD_rate_model_weak_plane_out.csv'
  rel_err = 1e-6
  abs_zero = 1e-8
  design = 'StrainEnergyRateDensity.md'
  requirement = 'The system shall be capable of calculating strain energy rate density when using hand-coded Jacobian and weak plane stress.'
[]

[ad_power_law]
  type = 'RunException'
  input = 'ad_power_law_creep.i'
  expect_err = 'Exceeded maximum iterations in material return mapping iterations.'
  cli_args = 'Materials/power_law_creep/use_substepping=NONE Executioner/dtmin=0.1 Outputs/file_base=ad_power_law_out'
  requirement = 'The system shall report diverged return mapping solve due to large deformation imposed in one step using automatic differentiation'
[]

[ad_power_law_substepping]
  type = 'Exodiff'
  input = 'ad_power_law_creep.i'
  cli_args = "Materials/power_law_creep/use_substepping=INCREMENT_BASED Materials/power_law_creep/maximum_number_substeps=500 Executioner/dtmin=0.1 Outputs/file_base=ad_power_law_substepping_out"
  exodiff = 'ad_power_law_substepping_out.e'
  valgrind = HEAVY
  requirement = 'The system shall converge under large deformation owing to the help of substepping using automatic differentiation'
[]

[ad_power_law_adaptive_substepping_increment]
  # We only check that the simulation converges with adaptive substepping
  type = 'RunException'
  input = 'ad_power_law_creep.i'
  cli_args = "Materials/power_law_creep/use_substepping=INCREMENT_BASED Materials/power_law_creep/adaptive_substepping=true Materials/power_law_creep/max_inelastic_increment=100 Materials/power_law_creep/maximum_number_substeps=2 Executioner/dt=100 Executioner/dtmin=100 Executioner/end_time=100 Outputs/file_base=ad_power_law_adaptive_substepping_out"
  expect_err = 'Adaptive substepping failed. Maximum number of substeps exceeded.'
  requirement = "The system shall converge under large deformation owing to the help of adaptive substepping using automatic differentiation with an increment based substepping criterion"
[]

[ad_power_law_adaptive_substepping_error]
  # We only check that the simulation converges with adaptive substepping
  type = 'RunException'
  input = 'ad_power_law_creep.i'
  cli_args = "Materials/power_law_creep/use_substepping=ERROR_BASED Materials/power_law_creep/adaptive_substepping=true Materials/power_law_creep/substep_strain_tolerance=100 Materials/power_law_creep/maximum_number_substeps=2 Executioner/dt=100 Executioner/dtmin=100 Executioner/end_time=100 Outputs/file_base=ad_power_law_adaptive_substepping_out"
  expect_err = 'Adaptive substepping failed. Maximum number of substeps exceeded.'
  requirement = "The system shall converge under large deformation owing to the help of adaptive substepping using automatic differentiation with an error based substepping criterion"
[]

[power_law]
  type = 'RunException'
  input = 'power_law_creep.i'
  expect_err = 'Exceeded maximum iterations in material return mapping iterations.'
  cli_args = 'Executioner/dtmin=0.1 Outputs/file_base=power_law_out'
  requirement = 'The system shall report diverged return mapping solve due to large deformation imposed in one step'
[]

[power_law_substepping]
  type = 'Exodiff'
  input = 'power_law_creep.i'
  cli_args = "Materials/power_law_creep/use_substepping=INCREMENT_BASED Materials/power_law_creep/maximum_number_substeps=500 Executioner/dtmin=0.1 Outputs/file_base=power_law_substepping_out"
  exodiff = 'power_law_substepping_out.e'
  requirement = 'The system shall converge under large deformation owing to the help of substepping'
[]

[power_law_adaptive_substepping_increment]
  # We only check that the simulation converges with adaptive substepping
  type = 'RunException'
  input = 'power_law_creep.i'
  cli_args = "Materials/power_law_creep/use_substepping=INCREMENT_BASED Materials/power_law_creep/adaptive_substepping=true Materials/power_law_creep/max_inelastic_increment=100 Materials/power_law_creep/maximum_number_substeps=2 Executioner/dt=100 Executioner/dtmin=100 Executioner/end_time=100 Outputs/file_base=power_law_adaptive_substepping_out"
  expect_err = 'Adaptive substepping failed. Maximum number of substeps exceeded.'
  requirement = "The system shall converge under large deformation owing to the help of adaptive substepping with an increment based substepping criterion"
[]

[power_law_adaptive_substepping_error]
  # We only check that the simulation converges with adaptive substepping
  type = 'RunException'
  input = 'power_law_creep.i'
  cli_args = "Materials/power_law_creep/use_substepping=INCREMENT_BASED Materials/power_law_creep/adaptive_substepping=true Materials/power_law_creep/substep_strain_tolerance=100 Materials/power_law_creep/maximum_number_substeps=2 Executioner/dt=100 Executioner/dtmin=100 Executioner/end_time=100 Outputs/file_base=power_law_adaptive_substepping_out"
  expect_err = 'Adaptive substepping failed. Maximum number of substeps exceeded.'
  requirement = "The system shall converge under large deformation owing to the help of adaptive substepping with an error based substepping criterion"
[]

[output]
  type = 'RunApp'
  input = 'power_law_creep.i'
  cli_args = "Materials/power_law_creep/use_substepping=INCREMENT_BASED Executioner/num_steps=1 Materials/power_law_creep/internal_solve_full_iteration_history=true Materials/power_law_creep/internal_solve_output_on=always Executioner/nl_rel_tol=1e-8"
  expect_out = "iteration=0 trial_stress="
  requirement = 'The system shall output verbose information about radial return iterations.'
[]

[./test]
  issues = '#7043'
  design = 'TemperatureDependentHardeningStressUpdate.md'
  type = 'Exodiff'
  input = 'temp_dep_hardening.i'
  exodiff = 'temp_dep_hardening_out.e'
  requirement = 'The system shall compute the stress as a function of temperature and plastic strain from user-supplied hardening functions not using automatic differentiation.'
[../]

[./ADtest]
  issues = '#18454'
  design = 'TemperatureDependentHardeningStressUpdate.md'
  type = 'Exodiff'
  input = 'ADtemp_dep_hardening.i'
  exodiff = 'temp_dep_hardening_out.e'
  requirement = 'The system shall compute the stress as a function of temperature and plastic strain from user-supplied hardening functions using automatic differentiation.'
[../]

[./smallstrain_3D]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using small strain."
[../]

[./incrementalstrain_3D]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallstrain_3D'
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using incremental small strain."
[../]

[./finitestrain_3D]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_3D.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=FINITE
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalstrain_3D'
  requirement = "The mechanics system shall correctly compute the jacobian for 3D problems using finite strain."
[../]

[./smallstrain_RZ]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using small strain."
[../]

[./incrementalstrain_RZ]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallstrain_RZ'
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using incremental small strain."
[../]

[./finitestrain_RZ]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_RZ.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=FINITE
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalstrain_RZ'
  requirement = "The mechanics system shall correctly compute the jacobian for RZ problems using finite strain."
[../]

[./smallplanestrain]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneSmallStrain
                Materials/stress/type=ComputeLinearElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using small strain."
[../]

[./incrementalplanestrain]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneIncrementalStrain
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-12
  difference_tol = 1E10
  prereq = 'smallplanestrain'
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using incremental small strain."
[../]

[./finiteplanestrain]
  type = 'PetscJacobianTester'
  input = 'jacobian_test_planestrain.i'
  cli_args = 'Materials/strain/type=ComputePlaneFiniteStrain
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 1E-7
  difference_tol = 1E10
  prereq = 'incrementalplanestrain'
  requirement = "The mechanics system shall correctly compute the jacobian for planestrain problems using finite strain."
[../]

[./smallstrain_spherical]
  type = 'PetscJacobianTester'
  input = 'jacobian_spherical.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=false
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL'
  ratio_tol = 2e-10
  difference_tol = 2e5
  requirement = "The mechanics system shall correctly compute the jacobian for spherical problems using small strain."
[../]

[./incrementalstrain_spherical]
  type = 'PetscJacobianTester'
  input = 'jacobian_spherical.i'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/incremental=true
                Physics/SolidMechanics/QuasiStatic/all/strain=SMALL
                Materials/stress/type=ComputeFiniteStrainElasticStress'
  ratio_tol = 2e-10
  difference_tol = 2e5
  requirement = "The mechanics system shall correctly compute the jacobian for spherical problems using small, incremental strain."
[../]

[./constant_expansion_coeff]
  type = 'Exodiff'
  input = 'constant_expansion_coeff.i'
  exodiff = 'constant_expansion_coeff_out.e'
  requirement = 'The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion.'
  design = 'ComputeThermalExpansionEigenstrain.md'
  issues = '#7457'
[../]

[./constant_expansion_coeff_restart]
  type = 'Exodiff'
  input = 'constant_expansion_coeff_restart.i'
  exodiff = 'constant_expansion_coeff_restart_out.e'
  prereq = 'constant_expansion_coeff'
  requirement = 'The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion when restarting the simulation.'
  design = 'ComputeThermalExpansionEigenstrain.md'
  issues = '#7457'
[../]

[./constant_expansion_stress_free_temp]
  type = 'Exodiff'
  input = 'constant_expansion_stress_free_temp.i'
  exodiff = 'constant_expansion_stress_free_temp_out.e'
  requirement = 'The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion with an initial strain due to the difference between the stress free temperature and initial temperature of the material.'
  design = 'ComputeThermalExpansionEigenstrain.md RankTwoAux.md'
  issues = '#8909'
[../]

[./multiple_thermal_eigenstrains]
  type = 'Exodiff'
  input = 'multiple_thermal_eigenstrains.i'
  exodiff = 'multiple_thermal_eigenstrains_out.e'
  requirement = 'The tensor mechanics module shall have the capability to combine multiple eigenstrains to correctly calculate an eigenstrain tensor resulting from isotropic thermal expansion.'
  design = 'ComputeThermalExpansionEigenstrain.md RankTwoAux.md'
  issues = '#7457'
[../]

[./ad_constant_expansion_coeff]
  type = 'Exodiff'
  input = 'ad_constant_expansion_coeff.i'
  exodiff = 'ad_constant_expansion_coeff_out.e'
  requirement = 'The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion.'
  design = 'ComputeThermalExpansionEigenstrain.md'
  issues = '#13091'
[../]

[./ad_constant_expansion_coeff_old]
  type = 'Exodiff'
  input = 'ad_constant_expansion_coeff.i'
  exodiff = 'ad_constant_expansion_coeff_out.e'
  requirement = 'The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion using the previous timestep.'
  design = 'ComputeThermalExpansionEigenstrain.md'
  issues = '#13091'
[../]

[./ad_constant_expansion_coeff-jac]
  type = 'PetscJacobianTester'
  input = 'ad_constant_expansion_coeff.i'
  run_sim = 'True'
  cli_args = 'Outputs/exodus=false Outputs/csv=false Executioner/num_steps=2'
  difference_tol = 1e-5
  issues = '#13091'
  design = 'ComputeThermalExpansionEigenstrain.md'
  requirement = 'The Jacobian for the AD eigenstrain tensor resulting from isotropic thermal expansion shall be perfect'
[../]

[./ad_constant_expansion_stress_free_temp]
  type = 'Exodiff'
  input = 'ad_constant_expansion_stress_free_temp.i'
  exodiff = 'ad_constant_expansion_stress_free_temp_out.e'
  requirement = 'The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion with an initial strain due to the difference between the stress free temperature and initial temperature of the material.'
  design = 'ComputeThermalExpansionEigenstrain.md'
  issues = '#13091'
[../]

[./ad_constant_expansion_stress_free_temp-jac]
  type = 'PetscJacobianTester'
  input = 'ad_constant_expansion_stress_free_temp.i'
  run_sim = 'True'
  cli_args = 'Outputs/exodus=false Executioner/num_steps=2'
  difference_tol = 1e-5
  issues = '#13091'
  design = 'ComputeThermalExpansionEigenstrain.md'
  requirement = 'The Jacobian for the AD eigenstrain tensor resulting from isotropic thermal expansion with an initial strain shall be perfect'
[../]

[./constant_expansion_stress_free_temp]
  type = 'Exodiff'
  input = 'constant_expansion_stress_free_temp.i'
  exodiff = 'constant_expansion_stress_free_temp_out.e'
  requirement = 'The tensor mechanics module shall have the capability to calculate the eigenstrain tensor resulting from isotropic thermal expansion with an initial strain due to the difference between the stress free temperature and initial temperature of the material.'
  design = 'ComputeThermalExpansionEigenstrain.md RankTwoAux.md'
  issues = '#8909'
[../]

[./multiple_thermal_eigenstrains]
  type = 'Exodiff'
  input = 'multiple_thermal_eigenstrains.i'
  exodiff = 'multiple_thermal_eigenstrains_out.e'
  requirement = 'The tensor mechanics module shall have the capability to combine multiple eigenstrains to correctly calculate an eigenstrain tensor resulting from isotropic thermal expansion.'
  design = 'ComputeThermalExpansionEigenstrain.md RankTwoAux.md'
  issues = '#7457'
[../]

[non-ad]
  type = Exodiff
  input = 'torque_small.i'
  exodiff = 'torque_small_out.e'
  abs_zero = 1e-9
  requirement = 'The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations.'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[]

[ad]
  type = Exodiff
  input = 'ad_torque_small.i'
  exodiff = 'ad_torque_small_out.e'
  abs_zero = 1e-9
  requirement = 'The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations with automatic differentiation.'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[]

[non-ad]
  type = Exodiff
  input = 'torque_small.i'
  exodiff = 'torque_small_out.e'
  abs_zero = 1e-9
  requirement = 'The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations.'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[]

[ad]
  type = Exodiff
  input = 'ad_torque_small.i'
  exodiff = 'ad_torque_small_out.e'
  abs_zero = 1e-9
  requirement = 'The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations with automatic differentiation.'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[]

[non-ad]
  type = Exodiff
  input = 'torque_small.i'
  exodiff = 'torque_small_out.e'
  abs_zero = 1e-9
  requirement = 'The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations.'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[]

[ad]
  type = Exodiff
  input = 'ad_torque_small.i'
  exodiff = 'ad_torque_small_out.e'
  abs_zero = 1e-9
  requirement = 'The mechanics system shall provide a way to apply a torque to a boundary for small strain simulations with automatic differentiation.'
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[]

[./torque_reaction_2D]
  design = TorqueReaction.md
  issues = '#6484'
  requirement = 'The system shall compute the torque for an applied deformation at the end of a beam in 2D'
  type = 'Exodiff'
  input = 'torque_reaction.i'
  exodiff = 'torque_reaction_out.e'
[../]

[./torque_reaction_3D]
  design = TorqueReaction.md
  issues = '#6484'
  requirement = 'The system shall compute the torque for an applied deformation at the end of a beam in 3D'
  type = 'Exodiff'
  input = 'torque_reaction_3D.i'
  exodiff = 'torque_reaction_3D_out.e'
  abs_zero = 1.e-8
[../]

[./torque_reaction_cylinder]
  design = 'TorqueReaction.md DisplacementAboutAxis.md'
  issues = '#6484'
  requirement = 'The system shall compute the torque resulting from twisting applied using DisplacementAboutAxis to the end of an elastic cylinder'
  type = 'Exodiff'
  input = 'torque_reaction_cylinder.i'
  exodiff = 'torque_reaction_cylinder_out.e'
  abs_zero = 5.e-7
[../]

[./torque_reaction_cylinder]
  design = 'TorqueReaction.md DisplacementAboutAxis.md'
  issues = '#6484'
  requirement = 'The system shall compute the torque resulting from twisting applied using DisplacementAboutAxis to the end of an elastic cylinder'
  type = 'Exodiff'
  input = 'torque_reaction_cylinder.i'
  exodiff = 'torque_reaction_cylinder_out.e'
  abs_zero = 5.e-7
[../]

[./disp_about_axis_motion]
  design = DisplacementAboutAxis.md
  issues = '#15092'
  requirement = 'The system shall provide a boundary condition that applies pure finite rigid body rotation to a surface of an elastic body'
  type = 'CSVDiff'
  input = 'disp_about_axis_axial_motion.i'
  csvdiff = 'disp_about_axis_axial_motion_out.csv'
  rel_err = 1E-5
  abs_zero = 1e-10
[../]

[./disp_about_axis_motion_incremental]
  design = DisplacementAboutAxis.md
  requirement = 'The system shall provide a boundary condition that applies pure finite rigid body rotation to a surface of an elastic body incrementally'
  type = 'CSVDiff'
  cli_args = 'BCs/top_x/angular_velocity=true BCs/top_x/function=1 BCs/top_y/angular_velocity=true BCs/top_y/function=1  Outputs/file_base=disp_about_axis_axial_motion_incremental_out'
  input = 'disp_about_axis_axial_motion.i'
  csvdiff = 'disp_about_axis_axial_motion_incremental_out.csv'
  rel_err = 1E-5
  abs_zero = 1e-10
  issues = '#15388'
[../]

[./disp_about_axis_axial_motion_delayed]
  design = DisplacementAboutAxis.md
  requirement = 'The system shall be able to use disaplcement about axis after applying an arbitraty deformation'
  type = 'CSVDiff'
  input = 'disp_about_axis_axial_motion_delayed.i'
  csvdiff = 'disp_about_axis_axial_motion_delayed_out.csv'
  rel_err = 1E-5
  abs_zero = 1e-10
  issues = '#15388'
[../]

[./disp_about_axis_error1]
  design = DisplacementAboutAxis.md
  issues = '#15092'
  requirement = 'The system shall generate an error if the DisplacementAboutAxis boundary condition is applied to a component outside the range applicable for the dimensionality of the model'
  type = 'RunException'
  input = 'disp_about_axis_errors.i'
  cli_args = 'BCs/top_y/component=3 BCs/top_y/axis_direction="0. 0. 1."'
  expect_err = 'Invalid component given for top_y: 3.'
[../]

[./disp_about_axis_error2]
  design = DisplacementAboutAxis.md
  issues = '#15092'
  requirement = 'The system shall generate an error if the vector prescribed using the axis_direction parameter in the DisplacementAboutAxis boundary condition has a length of zero'
  type = 'RunException'
  input = 'disp_about_axis_errors.i'
  cli_args = 'BCs/top_y/component=1 BCs/top_y/axis_direction="0. 0. 0."'
  expect_err = 'Please specify a non-zero direction vector for the axis_direction in top_y'
[../]

[test]
  type = Exodiff
  method = '!dbg'
  valgrind = 'none'
  input = parent.i
  exodiff = 'parent_out.e'
  requirement = 'The system shall be able to transfer a field from a displaced source domain to a target domain, using shape function evaluations in the source domain.'
[]

[./truss_3d]
  type = 'Exodiff'
  input = 'truss_3d.i'
  exodiff = 'truss_3d_out.e'
  abs_zero = 1e-7
  requirement = "The mechanics system shall accurately model the axial response of 3D truss elements."
[../]

[./truss_hex]
  type = 'Exodiff'
  input = 'truss_hex.i'
  exodiff = 'truss_hex_out.e'
  abs_zero = 1e-7
  requirement = "The truss element shall work correctly when hex elements are also included in the same input or mesh file."
[../]

[./truss_2d]
  type = 'Exodiff'
  input = 'truss_2d.i'
  exodiff = 'truss_2d_out.e'
  abs_zero = 1e-7
  max_parallel = 1
  requirement = "The mechanics system shall accurately model the static response of a 2D frame modeled using truss elements."
[../]

[./truss_3d_action]
  type = 'Exodiff'
  input = 'truss_3d_action.i'
  exodiff = 'truss_3d_out.e'
  abs_zero = 1e-7
  prereq = 'truss_3d'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 3D truss elements."
[../]

[./truss_hex_action]
  type = 'Exodiff'
  input = 'truss_hex_action.i'
  exodiff = 'truss_hex_out.e'
  abs_zero = 1e-7
  prereq = 'truss_hex'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using truss and hex elements."
[../]

[./truss_2d_action]
  type = 'Exodiff'
  input = 'truss_2d_action.i'
  exodiff = 'truss_2d_out.e'
  abs_zero = 1e-7
  max_parallel = 1
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block/area=area'
  prereq = 'truss_2d'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 2D truss elements."
[../]

[./action_error_1]
  type = 'RunException'
  input = 'truss_2d_action.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false'
  expect_err = 'LineElementAction: `area` should be provided as input for'
  requirement = "The LineElementAction shall produce an error if `area` is not provided as input for truss elements."
[../]

[./action_error_2]
  type = 'RunException'
  input = 'truss_2d_action.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false Physics/SolidMechanics/LineElement/QuasiStatic/block/area=area Physics/SolidMechanics/LineElement/QuasiStatic/block/rotations="rot_x"'
  expect_err = 'LineElementAction: Rotational variables cannot be set for truss elements.'
  requirement = "The LineElementAction shall produce an error if rotational variables are provided as input for truss elements."
[../]

[./truss_3d]
  type = 'Exodiff'
  input = 'truss_3d.i'
  exodiff = 'truss_3d_out.e'
  abs_zero = 1e-7
  requirement = "The mechanics system shall accurately model the axial response of 3D truss elements."
[../]

[./truss_hex]
  type = 'Exodiff'
  input = 'truss_hex.i'
  exodiff = 'truss_hex_out.e'
  abs_zero = 1e-7
  requirement = "The truss element shall work correctly when hex elements are also included in the same input or mesh file."
[../]

[./truss_2d]
  type = 'Exodiff'
  input = 'truss_2d.i'
  exodiff = 'truss_2d_out.e'
  abs_zero = 1e-7
  max_parallel = 1
  requirement = "The mechanics system shall accurately model the static response of a 2D frame modeled using truss elements."
[../]

[./truss_3d_action]
  type = 'Exodiff'
  input = 'truss_3d_action.i'
  exodiff = 'truss_3d_out.e'
  abs_zero = 1e-7
  prereq = 'truss_3d'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 3D truss elements."
[../]

[./truss_hex_action]
  type = 'Exodiff'
  input = 'truss_hex_action.i'
  exodiff = 'truss_hex_out.e'
  abs_zero = 1e-7
  prereq = 'truss_hex'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using truss and hex elements."
[../]

[./truss_2d_action]
  type = 'Exodiff'
  input = 'truss_2d_action.i'
  exodiff = 'truss_2d_out.e'
  abs_zero = 1e-7
  max_parallel = 1
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block/area=area'
  prereq = 'truss_2d'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 2D truss elements."
[../]

[./action_error_1]
  type = 'RunException'
  input = 'truss_2d_action.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false'
  expect_err = 'LineElementAction: `area` should be provided as input for'
  requirement = "The LineElementAction shall produce an error if `area` is not provided as input for truss elements."
[../]

[./action_error_2]
  type = 'RunException'
  input = 'truss_2d_action.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false Physics/SolidMechanics/LineElement/QuasiStatic/block/area=area Physics/SolidMechanics/LineElement/QuasiStatic/block/rotations="rot_x"'
  expect_err = 'LineElementAction: Rotational variables cannot be set for truss elements.'
  requirement = "The LineElementAction shall produce an error if rotational variables are provided as input for truss elements."
[../]

[./truss_3d]
  type = 'Exodiff'
  input = 'truss_3d.i'
  exodiff = 'truss_3d_out.e'
  abs_zero = 1e-7
  requirement = "The mechanics system shall accurately model the axial response of 3D truss elements."
[../]

[./truss_hex]
  type = 'Exodiff'
  input = 'truss_hex.i'
  exodiff = 'truss_hex_out.e'
  abs_zero = 1e-7
  requirement = "The truss element shall work correctly when hex elements are also included in the same input or mesh file."
[../]

[./truss_2d]
  type = 'Exodiff'
  input = 'truss_2d.i'
  exodiff = 'truss_2d_out.e'
  abs_zero = 1e-7
  max_parallel = 1
  requirement = "The mechanics system shall accurately model the static response of a 2D frame modeled using truss elements."
[../]

[./truss_3d_action]
  type = 'Exodiff'
  input = 'truss_3d_action.i'
  exodiff = 'truss_3d_out.e'
  abs_zero = 1e-7
  prereq = 'truss_3d'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 3D truss elements."
[../]

[./truss_hex_action]
  type = 'Exodiff'
  input = 'truss_hex_action.i'
  exodiff = 'truss_hex_out.e'
  abs_zero = 1e-7
  prereq = 'truss_hex'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using truss and hex elements."
[../]

[./truss_2d_action]
  type = 'Exodiff'
  input = 'truss_2d_action.i'
  exodiff = 'truss_2d_out.e'
  abs_zero = 1e-7
  max_parallel = 1
  cli_args = 'Physics/SolidMechanics/LineElement/QuasiStatic/block/area=area'
  prereq = 'truss_2d'
  requirement = "The LineElementAction shall correctly create the objects required for modeling the response of a mechanics system using 2D truss elements."
[../]

[./action_error_1]
  type = 'RunException'
  input = 'truss_2d_action.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false'
  expect_err = 'LineElementAction: `area` should be provided as input for'
  requirement = "The LineElementAction shall produce an error if `area` is not provided as input for truss elements."
[../]

[./action_error_2]
  type = 'RunException'
  input = 'truss_2d_action.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false Physics/SolidMechanics/LineElement/QuasiStatic/block/area=area Physics/SolidMechanics/LineElement/QuasiStatic/block/rotations="rot_x"'
  expect_err = 'LineElementAction: Rotational variables cannot be set for truss elements.'
  requirement = "The LineElementAction shall produce an error if rotational variables are provided as input for truss elements."
[../]

[./tensile]
  type = 'Exodiff'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/file_base=truss_plastic_tensile_out Materials/truss/hardening_constant=1e7'
  exodiff = 'truss_plastic_tensile_out.e'
  design = "source/materials/PlasticTruss.md"
  requirement = "The system shall correctly model the plastic response of truss elements with a linear hardening model under tension."
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./tensile_nohardening]
  type = 'Exodiff'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/file_base=truss_nohardening_tension_out Materials/truss/hardening_constant=0.0'
  exodiff = 'truss_nohardening_tension_out.e'
  design = "source/materials/PlasticTruss.md"
  requirement = "The system shall correctly model the plastic response of truss elements with perfect plasticity under tension."
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./tensile_hardeningfn]
  type = 'Exodiff'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/file_base=truss_hardeningfn_tension_out Materials/truss/hardening_function=hf'
  exodiff = 'truss_hardeningfn_tension_out.e'
  design = "source/materials/PlasticTruss.md"
  requirement = "The system shall correctly model the plastic response of truss elements with a user-defined hardening function model under tension."
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./compressive]
  type = 'Exodiff'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/file_base=truss_plastic_compression_out BCs/load/function=-t Materials/truss/hardening_constant=1e7'
  exodiff = 'truss_plastic_compression_out.e'
  design = "source/materials/PlasticTruss.md"
  requirement = "The system shall correctly model the plastic response of truss elements with a linear hardening model under compression."
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./compressive_nohardening]
  type = 'Exodiff'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/file_base=truss_nohardening_compression_out BCs/load/function=-t Materials/truss/hardening_constant=0.0'
  exodiff = 'truss_nohardening_compression_out.e'
  design = "source/materials/PlasticTruss.md"
  requirement = "The system shall correctly model the plastic response of truss elements with perfect plasticity under compression."
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./compressive_hardeningfn]
  type = 'Exodiff'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/file_base=truss_hardeningfn_compression_out BCs/load/function=-t Materials/truss/hardening_function=hf'
  exodiff = 'truss_hardeningfn_compression_out.e'
  design = "source/materials/PlasticTruss.md"
  requirement = "The system shall correctly model the plastic response of truss elements with a user-defined hardening function model under compression."
  # PR #26848. Clang 16 Apple Si is not compatible.
  machine = X86_64
[../]

[./error_nohardening]
  type = 'RunException'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false'
  expect_err = 'PlasticTruss: Either hardening_constant or hardening_function must be defined'
  design = "source/materials/PlasticTruss.md"
  requirement = "PlasticTruss material should produce error if neither the hardening constant nor a hardening function is provided."
[../]

[./error_hardening]
  type = 'RunException'
  input = 'truss_plastic.i'
  cli_args = 'Outputs/exodus=false Outputs/csv=false Materials/truss/hardening_function=hf Materials/truss/hardening_constant=0.0'
  expect_err = 'PlasticTruss: Only the hardening_constant or only the hardening_function can be defined but not both'
  design = "source/materials/PlasticTruss.md"
  requirement = "PlasticTruss material should produce error if both hardening constant and hardening function are provided."
[../]

[build_uel_tri_tests]
  type = RunCommand
  command = "cd ../../../examples/uel_tri_tests; make"
  use_shell = True
  requirement = "The UEL tri tests example shall be built."
  method = 'opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[build_uel_tri_states_tests]
  type = RunCommand
  command = "cd ../../../examples/uel_tri_states_tests; make"
  use_shell = True
  requirement = "The UEL tri states tests example shall be built."
  method = 'opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[build_uel_build_tests]
  type = RunCommand
  command = "cd ../../../examples/uel_build_tests; make"
  use_shell = True
  requirement = "The UEL build tests example shall be built."
  method = 'opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[build_uel_tri_tests_dbg]
  type = RunCommand
  command = "cd ../../../examples/uel_tri_tests; METHOD=dbg make"
  use_shell = True
  requirement = "The UEL tri tests example shall be built."
  method = 'dbg'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[build_uel_tri_states_tests_dbg]
  type = RunCommand
  command = "cd ../../../examples/uel_tri_states_tests; METHOD=dbg make"
  use_shell = True
  requirement = "The UEL tri states tests example shall be built."
  method = 'dbg'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[build_uel_build_tests_dbg]
  type = RunCommand
  command = "cd ../../../examples/uel_build_tests; METHOD=dbg make"
  use_shell = True
  requirement = "The UEL build tests example shall be built."
  method = 'dbg'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[reference]
  type = Exodiff
  input = reference.i
  exodiff = reference_out.e
  abs_zero = 5e-12
  requirement = "The system shall be able to solve a simple mechanics problem with small elastic deformation with a triangular mesh using MOOSE capabilities."
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
[]

[small]
  type = Exodiff
  input = small.i
  exodiff = small_out.e
  abs_zero = 5e-12
  requirement = "The system shall be able to solve a simple mechanics problem with small elastic deformation with a triangular mesh using a UEL plugin."
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[small_test]
  type = Exodiff
  input = small_test.i
  exodiff = small_test_out.e
  abs_zero = 5e-12
  requirement = "The system shall be able to solve a simple mechanics problem with small elastic deformation with a triangular mesh using a UEL plugin calling a UMAT routine with its standard interface."
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[uel_test_print]
  type = RunApp
  input = uel_test_print.i
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  # Testing output
  max_parallel = 1
  errors = 'StringThatWillNotBePresentInOutput'
  expect_out = 'Number of predefined variables:            2\n External field number            1  for node            1  is:    1500.0000000000000     \n External field number            1  for node            2  is:    1500.0000000000000     \n External field number            1  for node            3  is:    1500.0000000000000     \n External field number            1  for node            4  is:    1500.0000000000000     \n External field number            1  for node            5  is:    1500.0000000000000     \n External field number            1  for node            6  is:    1500.0000000000000     \n External field number            1  for node            7  is:    1500.0000000000000     \n External field number            1  for node            8  is:    1500.0000000000000     \n External field number            2  for node            1  is:    210.00000000000000     \n External field number            2  for node            2  is:    210.00000000000000     \n External field number            2  for node            3  is:    210.00000000000000     \n External field number            2  for node            4  is:    210.00000000000000     \n External field number            2  for node            5  is:    210.00000000000000     \n External field number            2  for node            6  is:    210.00000000000000     \n External field number            2  for node            7  is:    210.00000000000000     \n External field number            2  for node            8  is:    210.00000000000000     \n Time increment is:    10.000000000000000     \n Coordinates for node            1  are:   0.66666666666666663      ,   0.33333333333333331      ,   0.66666666666666663     \n Coordinates for node            2  are:    1.0000000000000000      ,   0.33333333333333331      ,   0.66666666666666663     \n Coordinates for node            3  are:    1.0000000000000000      ,   0.66666666666666663      ,   0.66666666666666663     \n Coordinates for node            4  are:   0.66666666666666663      ,   0.66666666666666663      ,   0.66666666666666663     \n Coordinates for node            5  are:   0.66666666666666663      ,   0.33333333333333331      ,    1.0000000000000000     \n Coordinates for node            6  are:    1.0000000000000000      ,   0.33333333333333331      ,    1.0000000000000000     \n Coordinates for node            7  are:    1.0000000000000000      ,   0.66666666666666663      ,    1.0000000000000000     \n Coordinates for node            8  are:   0.66666666666666663      ,   0.66666666666666663      ,    1.0000000000000000     \n Element number is:           25\n Number of coordinates at a node:            3\n Element type is:           10\n Number of UEL properties is:            5\n Property            1  is:    2.0000000000000000     \n Property            2  is:    1.0000000000000000     \n Property            3  is:    2.0000000000000000     \n Property            4  is:    210000.00000000000     \n Property            5  is:   0.29999999999999999     \n Number of nodes in this element:            8\n Number of state variables is:           96\n State variable            1  is:    0.0000000000000000     \n State variable            2  is:    0.0000000000000000     \n State variable            3  is:    0.0000000000000000     \n'
  requirement = 'The Abaqus UEL interface shall be able to pass initial correct values of coordinates into a user-defined UEL routine for a hexahedral element and a non-trivial setup.'
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[small_test_uel_umat]
  type = Exodiff
  input = small_test_expanded.i
  exodiff = small_test_expanded_out.e
  requirement = 'The Abaqus UEL interface shall be able to interface with a UEL that calls a UMAT interface and must yield the same results for a triangular element as a UEL routine that computes internal forces without calling a UMAT routine.'
  abs_zero = 1e-12
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[small_test_moose_umat]
  type = Exodiff
  input = small_test_expanded_umat.i
  exodiff = small_test_expanded_umat_out.e
  requirement = 'The Abaqus UMAT interface shall be able to yield the same results for a triangular element as a UEL routine that computes internal forces without calling a UMAT routine or an analogous UEL interface that calls a UMAT routine for computing the stress vector and the Jacobian.'
  abs_zero = 1e-12
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[small_test_uel_states_fields]
  type = Exodiff
  input = small_test_uel_states_fields.i
  exodiff = small_test_uel_states_fields_out.e
  requirement = 'The Abaqus UEL interface, calling a UMAT routine, shall be able to yield the same results for a triangular element that a UMAT routine that computes internal forces when the solution depends on system states and two external fields, including temperature.'
  abs_zero = 1e-12
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[small_test_umat_states_fields]
  type = Exodiff
  input = small_test_umat_states_fields.i
  exodiff = small_test_umat_states_fields_out.e
  requirement = 'The Abaqus UMAT interface shall be able to yield the same results for a triangular element that a UEL routine that computes internal forces, calling a UMAT routine, when the solution depends on system states and two external fields, including temperature.'
  abs_zero = 1e-12
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[small_test_umat_states_fields_gradient]
  type = Exodiff
  input = small_test_umat_states_fields_gradient.i
  exodiff = small_test_umat_states_fields_gradient_out.e
  requirement = 'The Abaqus UMAT interface shall be able to yield the same results for a triangular element that a UEL routine that computes internal forces, calling a UMAT routine, when the solution depends on system states and two external fields, including temperature, which vary significantly with space.'
  abs_zero = 1e-12
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[small_test_uel_states_fields_gradient]
  type = Exodiff
  input = small_test_uel_states_fields_gradient.i
  exodiff = small_test_uel_states_fields_gradient_out.e
  requirement = 'The Abaqus UEL interface shall be able to yield the same results for a triangular element that a UMAT routine that computes internal forces when the solution depends on system states and two external fields, including temperature, which vary significantly with space. Therefore, the system shall properly handle state and external fields whose values depend on element location.'
  abs_zero = 1e-12
  # Only test plugins in dbg and opt.
  method = 'dbg opt'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[initial]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'UserObjects/uexternaldb/execute_on=INITIAL'
  expect_out = 'UEXTERNALDB           0 '
  detail = 'beginning of the simulation.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[timestep_begin]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'UserObjects/uexternaldb/execute_on=TIMESTEP_BEGIN'
  expect_out = 'UEXTERNALDB           1 '
  detail = 'beginning of each MOOSE time step.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[timestep_end]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'UserObjects/uexternaldb/execute_on=TIMESTEP_END'
  expect_out = 'UEXTERNALDB           2 '
  detail = 'end of each MOOSE time step.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[final]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'UserObjects/uexternaldb/execute_on=FINAL'
  expect_out = 'UEXTERNALDB           3 '
  detail = 'end of the simulation.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[steps]
  type = 'RunApp'
  input = 'utility_functions_steps.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  expect_out = 'Loading step is           1'
  requirement = 'The Abaqus UEXTERNALDB interface shall interface with a general user object to obtain the proper loading step and pass it to the user routine.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[getoutdir]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'UserObjects/uexternaldb/execute_on=INITIAL'
  expect_out = 'getoutdir           1 \. '
  requirement = 'The Abaqus UEXTERNALDB interface shall provide the Abaqus API to obtain the simulation output directory.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[getjobname]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'UserObjects/uexternaldb/execute_on=INITIAL'
  expect_out = 'getjobname          17 utility_functions '
  requirement = 'The Abaqus UEXTERNALDB interface shall provide the Abaqus API to obtain the simulation job name.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[info]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'UserObjects/uexternaldb/execute_on=INITIAL'
  expect_out = '\*\* Abaqus Info \*\*\nInline message 1 2 0.100000 0.200000 0.300000 ONE      TWO     !'
  detail = 'info level.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[warning]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = "UserObjects/step_uo/step_start_times='0.0 0.1 0.2' UserObjects/uexternaldb/execute_on=TIMESTEP_END"
  expect_out = '\*\* Abaqus Warning \*\*\nInline message 1 2 0.100000 0.200000 0.300000 ONE      TWO     !'
  detail = 'warning level.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[non_fatal]
  type = 'RunApp'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = "UserObjects/step_uo/step_start_times='0.0 0.1 0.2 0.3' UserObjects/uexternaldb/execute_on=TIMESTEP_END"
  expect_out = '\*\* Abaqus Non-fatal Error \*\*\nInline message 1 2 0.100000 0.200000 0.300000 ONE      TWO     !'
  detail = 'non-fatal error level.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[error]
  type = 'RunException'
  input = 'utility_functions.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = "UserObjects/step_uo/step_start_times='0.0 0.1 0.2 0.3 0.4' UserObjects/uexternaldb/execute_on=TIMESTEP_END"
  expect_err = '\*\*\* ERROR \*\*\*\nInline message 1 2 0.100000 0.200000 0.300000 ONE      TWO     !'
  detail = 'fatal error level.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[single_thread]
  type = 'RunApp'
  input = 'mutex_test.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  min_threads = 1
  max_threads = 1
  expect_out = 'sum = 1000.'
  detail = 'supporting single threaded execution.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[two_threads]
  type = 'RunApp'
  input = 'mutex_test.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  min_threads = 2
  max_threads = 2
  expect_out = 'sum = 2000.'
  detail = 'supporting at least 2 threads.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[four_threads]
  type = 'RunApp'
  input = 'mutex_test.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  min_threads = 4
  max_threads = 4
  expect_out = 'sum = 4000.'
  detail = 'supporting at least 4 threads.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[single_thread]
  type = 'RunApp'
  input = 'sma_memory.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  expect_out = '3lop 40.5 1950'
  detail = 'supporting single threaded execution.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[two_threads]
  type = 'RunApp'
  input = 'sma_memory.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  min_threads = 2
  max_threads = 2
  expect_out = '3lop 40.5 1950'
  detail = 'supporting two threaded execution.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[four_threads]
  type = 'RunApp'
  input = 'sma_memory.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  min_threads = 4
  max_threads = 4
  expect_out = '3lop 40.5 1950'
  detail = 'supporting four threaded execution.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[linear_strain_hardening]
  type = 'Exodiff'
  input = 'linear_strain_hardening.i'
  exodiff = 'linear_strain_hardening_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for stateful properties'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[total_strain_error]
  type = 'RunException'
  input = 'linear_strain_hardening.i'
  library_mode = 'DYNAMIC'
  expect_err = 'AbaqusUMATStress \'constant\': Incremental strain quantities are not available'
  cli_args = 'Physics/SolidMechanics/QuasiStatic/all/strain=SMALL'
  valgrind = 'NONE'
  requirement = 'The system shall raise an error if a UMAT that requires incremental quantities is being used with a total strain formulation'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic]
  type = 'Exodiff'
  input = 'elastic.i'
  cli_args = "Materials/active='umat'"
  exodiff = 'elastic_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials written in Fortran77 as constitutive models, with support for finite strain elastic material models'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_small]
  type = 'Exodiff'
  input = 'elastic.i'
  cli_args = "Materials/active='umat' Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Physics/SolidMechanics/QuasiStatic/all/incremental=true Outputs/file_base=elastic_small"
  exodiff = 'elastic_small.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials written in Fortran77 as constitutive models, with support for small strain elastic material models'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_C]
  type = 'Exodiff'
  input = 'elastic.i'
  cli_args = "Materials/active='umat' Materials/umat/plugin=../../../plugins/elastic2"
  exodiff = 'elastic_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials written in C/C++ as constitutive models, with support for finite strain elastic material models'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_reference]
  type = 'Exodiff'
  input = 'elastic.i'
  cli_args = "Materials/active='elastic stress'"
  exodiff = 'elastic_out.e'
  requirement = 'The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for finite strain elasticity'
[]

[elastic_small_reference]
  type = 'Exodiff'
  input = 'elastic.i'
  cli_args = "Materials/active='elastic stress' Materials/stress/type=ComputeLinearElasticStress Physics/SolidMechanics/QuasiStatic/all/strain=SMALL Outputs/file_base=elastic_small"
  exodiff = 'elastic_small.e'
  requirement = 'The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for small strain elasticity'
[]

[elastic_incremental]
  type = 'Exodiff'
  input = 'elastic.i'
  cli_args = "Materials/active='umat' Materials/umat/plugin='../../../plugins/elastic_incremental'"
  exodiff = 'elastic_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for incremental strain elastic material models'
  issues = '#18843'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_shear_reference]
  type = 'Exodiff'
  input = 'elastic_shear.i'
  cli_args = "Executioner/dt='1.0' Outputs/time_step_interval='10' GlobalParams/decomposition_method=HughesWinget"
  exodiff = 'elastic_shear_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The Abaqus UMAT interface shall produce the correct stresses for the hyperelasticNeo-Hookean model under shear loading. The results shall not depend on the time step size.Reference computation with fine time stepping.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_shear]
  type = 'Exodiff'
  input = 'elastic_shear.i'
  cli_args = "Executioner/dt='10.0' GlobalParams/decomposition_method=HughesWinget"
  exodiff = 'elastic_shear_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The Abaqus UMAT interface shall produce the correct stresses for the hyperelasticNeo-Hookean model under shear loading. The results shall not depend on the time step size.Comparison with coarse time stepping.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[multiple_blocks]
  type = 'Exodiff'
  input = 'multiple_blocks.i'
  exodiff = 'multiple_blocks_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with the ability to provide different parameters for different blocks using the same interface plug-in.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[multiple_blocks_two_materials]
  type = 'Exodiff'
  input = 'multiple_blocks_two_materials.i'
  exodiff = 'multiple_blocks_two_materials_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with the ability to provide different parameters for different blocks using distinct interface plug-ins.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[multiple_blocks_two_materials_parallel]
  type = 'Exodiff'
  input = 'multiple_blocks_two_materials_parallel.i'
  exodiff = 'multiple_blocks_two_materials_parallel_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with the ability to provide different parameters for different blocks using distinct interface plug-ins in multi processor runs.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[rve_multimaterial_umat]
  type = 'Exodiff'
  input = 'rve_multimaterial.i'
  exodiff = 'rve_multimaterial_umat_out.e'
  cli_args = "Materials/active='umat_1 umat_2' Outputs/file_base=rve_multimaterial_umat_out"
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  # A demonstration test, no need run this through a debug executable, which is already tested
  method = opt
  requirement = 'The system shall be able to simulate a multiblock solid mechanics test in which the blocks are meshed contiguously using the UMAT interface.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[rve_multimaterial_moose]
  type = 'Exodiff'
  input = 'rve_multimaterial.i'
  exodiff = 'rve_multimaterial_moose_out.e'
  cli_args = "Materials/active='stress elastic_1 elastic_2' Outputs/file_base=rve_multimaterial_moose_out"
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  # A demonstration test, no need run this through a debug executable, which is already tested
  method = opt
  requirement = 'The system shall be able to simulate a multiblock solid mechanics test in which the blocks are meshed contiguously.'
[]

[predef]
  type = 'Exodiff'
  input = 'predef.i'
  cli_args = "Materials/active='umat'"
  exodiff = 'predef_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with an external field (not temperature) affecting material behavior '
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[predef_reference]
  type = 'Exodiff'
  input = 'predef.i'
  cli_args = "Materials/active='elasticity_tensor strain_dependent_elasticity_tensor stress prefactor_material_block'"
  exodiff = 'predef_out.e'
  requirement = 'The system shall avoid regression in a simple mechanical problem where a strain field modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external field verification'
[]

[dpredef]
  type = 'Exodiff'
  input = 'dpredef.i'
  cli_args = "Materials/active='umat'"
  exodiff = 'dpredef_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with an external field (not temperature) step increment affecting material behavior '
  rel_err = 5.0e-5
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[dpredef_reference]
  type = 'Exodiff'
  input = 'dpredef.i'
  cli_args = "Materials/active='elasticity_tensor strain_dependent_elasticity_tensor stress prefactor_material_block'"
  exodiff = 'dpredef_out.e'
  requirement = 'The system shall avoid regression in a simple mechanical problem where a real number representing the strain increment modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external field increment verification'
[]

[predef_multiple]
  type = 'Exodiff'
  input = 'predef_multiple.i'
  cli_args = "Materials/active='umat'"
  exodiff = 'predef_multiple_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with two external fields (not temperature) affecting material behavior '
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[predef_multiple_reference]
  type = 'Exodiff'
  input = 'predef_multiple.i'
  cli_args = "Materials/active='elasticity_tensor strain_dependent_elasticity_tensor stress prefactor_material_block'"
  exodiff = 'predef_multiple_out.e'
  requirement = 'The system shall avoid regression in a simple mechanical problem where two strain fields modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external field verification'
[]

[predef_multiple_mat]
  type = 'Exodiff'
  input = 'predef_multiple_mat.i'
  cli_args = "Materials/active='umat strain_xx strain_yy'"
  exodiff = 'predef_multiple_mat_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with two external material properties affecting material behavior '
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[predef_multiple_reference_mat]
  type = 'Exodiff'
  input = 'predef_multiple_mat.i'
  cli_args = "Materials/active='elasticity_tensor strain_dependent_elasticity_tensor stress prefactor_material_block strain_xx strain_yy'"
  exodiff = 'predef_multiple_mat_out.e'
  requirement = 'The system shall avoid regression in a simple mechanical problem where two strain fields modifies the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT external material property verification'
[]

[predef]
  type = 'RunApp'
  input = 'print.i'
  cli_args = "Materials/active='umat'"
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  expect_out = 'STRAIN_ 1   -0.0000030\n DSTRAIN_ 1   -0.0000030\n STRAIN_ 2    0.0000100\n DSTRAIN_ 2    0.0000100\n STRAIN_ 3   -0.0000030\n DSTRAIN_ 3   -0.0000030\n STRAIN_ 4   [ -]0.0000000\n DSTRAIN_ 4   [ -]0.0000000\n STRAIN_ 5   [ -]0.0000000\n DSTRAIN_ 5   [ -]0.0000000\n STRAIN_ 6   [ -]0.0000000\n DSTRAIN_ 6   [ -]0.0000000\n COORDS_ 1    0.2886751\n COORDS_ 2    0.5000000\n COORDS_ 3    0.2886751\n DFGRD0_ 1 1    0.9999970\n DFGRD0_ 1 2   [ -]0.0000000\n DFGRD0_ 1 3   [ -]0.0000000\n DFGRD0_ 2 1   [ -]0.0000000\n DFGRD0_ 2 2    1.0000100\n DFGRD0_ 2 3   [ -]0.0000000\n DFGRD0_ 3 1   [ -]0.0000000\n DFGRD0_ 3 2   [ -]0.0000000\n DFGRD0_ 3 3    0.9999970\n DFGRD1_ 1 1    0.9999940\n DFGRD1_ 1 2   [ -]0.0000000\n DFGRD1_ 1 3   [ -]0.0000000\n DFGRD1_ 2 1   [ -]0.0000000\n DFGRD1_ 2 2    1.0000200\n DFGRD1_ 2 3   [ -]0.0000000\n DFGRD1_ 3 1   [ -]0.0000000\n DFGRD1_ 3 2   [ -]0.0000000\n DFGRD1_ 3 3    0.9999940\n DROT_ 1 1    1.0000000\n DROT_ 1 2   [ -]0.0000000\n DROT_ 1 3   [ -]0.0000000\n DROT_ 2 1   [ -]0.0000000\n DROT_ 2 2    1.0000000\n DROT_ 2 3   [ -]0.0000000\n DROT_ 3 1   [ -]0.0000000\n DROT_ 3 2   [ -]0.0000000\n DROT_ 3 3    1.0000000\n TIME_ 1   10.0000000\n TIME_ 2   10.0000000\n CELENT 1.0000000\n CMNAME: umat_face\s*\n NDI_ 3\n NSHR_ 3\n NTENS_ 6\n NOEL_ 1\n NPT_ 3\n LAYER_-1\n KSPT_-1\n KSTEP_ 1\n KINC_ 2\n'
  requirement = 'The Abaqus UMAT interface shall pass correct values for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when a single element is subjected to axial loading. Values are checked against verified references '
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_shear]
  type = 'Exodiff'
  input = 'print_shear.i'
  cli_args = "Materials/active='umat'"
  exodiff = 'print_shear_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The Abaqus UMAT interface shall produce the same results (stress, strain, displacements) as the built-in MOOSE capabilities for a mechanical problem with two external fields (not temperature) step increment affecting material behavior and shear deformation '
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_shear_reference]
  type = 'Exodiff'
  input = 'print_shear.i'
  cli_args = "Materials/active='elasticity_tensor strain_dependent_elasticity_tensor stress prefactor_material_block'"
  exodiff = 'print_shear_out.e'
  requirement = 'The system shall avoid regression in a simple mechanical problem where two strain increments modify the stiffness of the material through CompositeElasticityTensor. This test also serves as a reference for UMAT behavior in the presence of shear deformation. '
[]

[print_shear_print]
  type = 'RunApp'
  input = 'print_shear.i'
  cli_args = "Materials/active='umat'"
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  expect_out = 'STRAIN_ 1   [ -]0.0000000\n DSTRAIN_ 1   -0.0000299\n STRAIN_ 2   [ -]0.0000000\n DSTRAIN_ 2    0.0001463\n STRAIN_ 3   [ -]0.0000000\n DSTRAIN_ 3   -0.0000388\n STRAIN_ 4   [ -]0.0000000\n DSTRAIN_ 4    0.0045930\n STRAIN_ 5   [ -]0.0000000\n DSTRAIN_ 5   -0.0024651\n STRAIN_ 6   [ -]0.0000000\n DSTRAIN_ 6    0.0000219\n COORDS_ 1   [ -]0.0000000\n COORDS_ 2    0.3872983\n COORDS_ 3   -0.3872983\n DFGRD0_ 1 1    1.0000000\n DFGRD0_ 1 2   [ -]0.0000000\n DFGRD0_ 1 3   [ -]0.0000000\n DFGRD0_ 2 1   [ -]0.0000000\n DFGRD0_ 2 2    1.0000000\n DFGRD0_ 2 3   [ -]0.0000000\n DFGRD0_ 3 1   [ -]0.0000000\n DFGRD0_ 3 2   [ -]0.0000000\n DFGRD0_ 3 3    1.0000000\n DFGRD1_ 1 1    0.9998834\n DFGRD1_ 1 2    0.0180418\n DFGRD1_ 1 3   [ -]0.0000000\n DFGRD1_ 2 1   -0.0134463\n DFGRD1_ 2 2    0.9999889\n DFGRD1_ 2 3   [ -]0.0000000\n DFGRD1_ 3 1   -0.0024650\n DFGRD1_ 3 2    0.0000163\n DFGRD1_ 3 3    0.9999627\n DROT_ 1 1    0.9998753\n DROT_ 1 2    0.0157422\n DROT_ 1 3    0.0012320\n DROT_ 2 1   -0.0157422\n DROT_ 2 2    0.9998761\n DROT_ 2 3   -0.0000401\n DROT_ 3 1   -0.0012325\n DROT_ 3 2    0.0000207\n DROT_ 3 3    0.9999992\n TIME_ 1   [ -]0.0000000\n TIME_ 2   [ -]0.0000000\n CELENT 1.0000000\n CMNAME: umat\s*\n NDI_ 3\n NSHR_ 3\n NTENS_ 6\n NOEL_ 1\n NPT_ 8\n LAYER_-1\n KSPT_-1\n KSTEP_ 1\n KINC_ 1\n FIELD1_[ -]0.0000000\n FIELD2_[ -]0.0000000\n DFIELD1_ 0.0000739\n DFIELD2_ 0.0022982'
  requirement = 'The Abaqus UMAT interface shall pass the correct values for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when shear deformation (causing nontrivial rotation kinematics) is present. '
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_shear_defgrad]
  type = 'RunApp'
  input = 'print_shear_defgrad.i'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  expect_out = 'DFGRD1_ 1 1    1.0000000\n DFGRD1_ 1 2    0.5000000\n DFGRD1_ 1 3   [ -]0.0000000\n DFGRD1_ 2 1   [ -]0.0000000\n DFGRD1_ 2 2    1.0000000\n DFGRD1_ 2 3   [ -]0.0000000\n DFGRD1_ 3 1   [ -]0.0000000\n DFGRD1_ 3 2   [ -]0.0000000\n DFGRD1_ 3 3    1.0000000\n DROT_ 1 1    0.9921623\n DROT_ 1 2    0.1249561\n DROT_ 1 3   [ -]0.0000000\n DROT_ 2 1   -0.1249561\n DROT_ 2 2    0.9921623\n DROT_ 2 3   [ -]0.0000000\n DROT_ 3 1   [ -]0.0000000\n DROT_ 3 2   [ -]0.0000000\n DROT_ 3 3    1.0000000\n '

  requirement = 'The Abaqus UMAT interface shall pass the correct values for the deformation gradient DFGRD1 and the rotation increment DROT, accounting for the fact, that the calling C++ code is row majorand the called Fortran code is column major.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_shear_defgrad_deformed]
  type = 'RunApp'
  issues = '#22880'
  input = 'print_shear.i'
  cli_args = 'Materials/active=umat Materials/umat/use_displaced_mesh=true'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  expect_out = 'STRAIN_ 1   [ -]0.0000000\n DSTRAIN_ 1   -0.0000299\n STRAIN_ 2   [ -]0.0000000\n DSTRAIN_ 2    0.0001463\n STRAIN_ 3   [ -]0.0000000\n DSTRAIN_ 3   -0.0000388\n STRAIN_ 4   [ -]0.0000000\n DSTRAIN_ 4    0.0045930\n STRAIN_ 5   [ -]0.0000000\n DSTRAIN_ 5   -0.0024651\n STRAIN_ 6   [ -]0.0000000\n DSTRAIN_ 6    0.0000219\n COORDS_ 1   [ -]0.0160084\n COORDS_ 2    0.3872885\n COORDS_ 3   -0.3872839\n DFGRD0_ 1 1    1.0000000\n DFGRD0_ 1 2   [ -]0.0000000\n DFGRD0_ 1 3   [ -]0.0000000\n DFGRD0_ 2 1   [ -]0.0000000\n DFGRD0_ 2 2    1.0000000\n DFGRD0_ 2 3   [ -]0.0000000\n DFGRD0_ 3 1   [ -]0.0000000\n DFGRD0_ 3 2   [ -]0.0000000\n DFGRD0_ 3 3    1.0000000\n DFGRD1_ 1 1    0.9998834\n DFGRD1_ 1 2    0.0180418\n DFGRD1_ 1 3   [ -]0.0000000\n DFGRD1_ 2 1   -0.0134463\n DFGRD1_ 2 2    0.9999889\n DFGRD1_ 2 3   [ -]0.0000000\n DFGRD1_ 3 1   -0.0024650\n DFGRD1_ 3 2    0.0000163\n DFGRD1_ 3 3    0.9999627\n DROT_ 1 1    0.9998753\n DROT_ 1 2    0.0157422\n DROT_ 1 3    0.0012320\n DROT_ 2 1   -0.0157422\n DROT_ 2 2    0.9998761\n DROT_ 2 3   -0.0000401\n DROT_ 3 1   -0.0012325\n DROT_ 3 2    0.0000207\n DROT_ 3 3    0.9999992\n TIME_ 1   [ -]0.0000000\n TIME_ 2   [ -]0.0000000\n CELENT 1.0000114\n CMNAME: umat\s*\n NDI_ 3\n NSHR_ 3\n NTENS_ 6\n NOEL_ 1\n NPT_ 8\n LAYER_-1\n KSPT_-1\n KSTEP_ 1\n KINC_ 1\n FIELD1_[ -]0.0000000\n FIELD2_[ -]0.0000000\n DFIELD1_ 0.0000739\n DFIELD2_ 0.0022982'
  requirement = 'The Abaqus UMAT interface shall pass the values for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when shear deformation is present and large deformation kinematics is true, which captures variables or properties that may rely on the displaced mesh, such as COORDS and CELENT.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_c]
  type = 'RunApp'
  input = 'print_c.i'
  cli_args = "Materials/active='umat'"
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  expect_out = 'stran 0 = -?0.0000000\nstran 1 = -?0.0000000\nstran 2 = -?0.0000000\nstran 3 = 0.0000000\nstran 4 = -?0.0000000\nstran 5 = -?0.0000000\ndstran 0 = -0.0000143\ndstran 1 = 0.0000476\ndstran 2 = -0.0000143\ndstran 3 = -?0.0000000\ndstran 4 = -?0.0000000\ndstran 5 = -?0.0000000\nstress 0 = -?0.0000000\nstress 1 = 10.0000000\nstress 2 = -?0.0000000\nstress 3 = -?0.0000000\nstress 4 = -?0.0000000\nstress 5 = -?0.0000000\ncoords 0 = 0.2886751\ncoords 1 = 0.2886751\ncoords 2 = 0.2886751\ndfgrd0 0 = 1.0000000\ndfgrd0 1 = -?0.0000000\ndfgrd0 2 = -?0.0000000\ndfgrd0 3 = 0.0000000\ndfgrd0 4 = 1.0000000\ndfgrd0 5 = -?0.0000000\ndfgrd0 6 = -?0.0000000\ndfgrd0 7 = -?0.0000000\ndfgrd0 8 = 1.0000000\ndfgrd1 0 = 0.9999857\ndfgrd1 1 = -?0.0000000\ndfgrd1 2 = -?0.0000000\ndfgrd1 3 = -?0.0000000\ndfgrd1 4 = 1.0000476\ndfgrd1 5 = -?0.0000000\ndfgrd1 6 = -?0.0000000\ndfgrd1 7 = -?0.0000000\ndfgrd1 8 = 0.9999857\ndrot 0 = 1.0000000\ndrot 1 = -?0.0000000\ndrot 2 = -?0.0000000\ndrot 3 = -?0.0000000\ndrot 4 = 1.0000000\ndrot 5 = -?0.0000000\ndrot 6 = -?0.0000000\ndrot 7 = -?0.0000000\ndrot 8 = 1.0000000\ntime 0 = 0.0000000\ntime 1 = 0.0000000\ncelent = 1.0000000\nndi = 3\nnshr = 3\nntens = 6\nnoel = 1\nnpt = 8\nlayer = -1\nkspt = -1\nkstep = 1\nkinc = 1\ncmname = umat'
  requirement = 'The Abaqus UMAT interface shall pass correct values into a C UMAT routine for STRAN, DSTRAN, TIME, CMNAME, NDI, NSHR, NTENS, COORDS, DROT, CELENT, DFGRD0, DFGRD1, NOEL, NPT, and KINC, when a single element is subjected to axial loading. Values are checked against verified references '
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_compare_c]
  type = 'Exodiff'
  input = 'print_compare_c.i'
  cli_args = "Materials/active='umat_c'"
  exodiff = 'print_compare_c_out.e'
  requirement = 'The system shall generate identical numerical results regardless of whether the UMAT interface is written in Fortran or C. Generation of reference results.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_compare_f]
  type = 'Exodiff'
  input = 'print_compare_c.i'
  cli_args = "Materials/active='umat_f'"
  exodiff = 'print_compare_c_out.e'
  requirement = 'The system shall generate identical numerical results regardless of whether the UMAT interface is written in Fortran or C. Verification.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[print_eigen]
  type = 'RunApp'
  input = 'print_compare_c.i'
  cli_args = "Materials/active='umat_eigen'"
  expect_out = 'Eigenvalues 0 769.231\nEigenvalues 1 2500\nEigenvalues 2 769.231\nEigenvalues 3 384.615\nEigenvalues 4 384.615\nEigenvalues 5 384.615\n'
  requirement = 'The system shall allow for the correct use of Eigen matrices in C UMAT functions.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[shear_order_umat_umat_x]
  type = 'Exodiff'
  input = 'shear_order_umat.i'
  cli_args = "Materials/active='umat' BCs/pull_function/variable=disp_x Outputs/file_base=shear_order_umat_x_out"
  exodiff = 'shear_order_umat_x_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  rel_err = 2.0e-4
  requirement = 'UMAT shall generate the correct shear deformation and stress when a single element is sheared via a Dirichlet boundary condition on the XY plane with anisotropic shear stiffness; results must coincide with those of MOOSE.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[shear_order_umat_umat_z]
  type = 'Exodiff'
  input = 'shear_order_umat.i'
  cli_args = "Materials/active='umat' BCs/pull_function/variable=disp_z Outputs/file_base=shear_order_umat_z_out"
  exodiff = 'shear_order_umat_z_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  rel_err = 2.0e-4
  requirement = 'UMAT shall generate the correct shear deformation and stress when a single element is sheared via a Dirichlet boundary condition on the YZ plane with anisotropic shear stiffness; results must coincide with those of MOOSE.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[shear_order_umat_moose_x]
  type = 'Exodiff'
  input = 'shear_order_umat.i'
  cli_args = "Materials/active='elastic stress' BCs/pull_function/variable=disp_x Outputs/file_base=shear_order_moose_x_out"
  exodiff = 'shear_order_moose_x_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall generate reference results of a sheared finite element on the XY plane.'
[]

[shear_order_umat_moose_z]
  type = 'Exodiff'
  input = 'shear_order_umat.i'
  cli_args = "Materials/active='elastic stress' BCs/pull_function/variable=disp_z Outputs/file_base=shear_order_moose_z_out"
  exodiff = 'shear_order_moose_z_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall generate reference results of a sheared finite element on the YZ plane.'
[]

[shear_order_umat_umat_z_jacobian]
  type = PetscJacobianTester
  input = 'shear_order_umat.i'
  cli_args = "Materials/active='umat' BCs/pull_function/variable=disp_z Outputs/file_base=shear_order_umat_z_out Executioner/end_time=2.0"
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  ratio_tol = 0.04
  difference_tol = 2500
  requirement = 'The system shall generate a system Jacobian from the UMAT routines using large strain kinematics that is of the same order as the one generated by MOOSE using Rashid strain incrementation when the shear stiffness is anisotropic.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature_steps]
  type = 'Exodiff'
  input = 'elastic_temperature_steps.i'
  exodiff = 'elastic_temperature_steps_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature_steps_uo]
  type = 'Exodiff'
  input = 'elastic_temperature_steps_uo.i'
  exodiff = 'elastic_temperature_steps_uo_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature_steps_uo_durations]
  type = 'Exodiff'
  input = 'elastic_temperature_steps_uo_durations.i'
  exodiff = 'elastic_temperature_steps_uo_durations_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object, to which the user only provides the step durations.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature_steps_uo_intervals]
  type = 'Exodiff'
  input = 'elastic_temperature_steps_uo_intervals.i'
  exodiff = 'elastic_temperature_steps_uo_intervals_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object, to which the user only provides the number of steps and the total time interval.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature_steps_uo_sync]
  type = 'Exodiff'
  input = 'elastic_temperature_steps_uo.i'
  exodiff = 'elastic_temperature_steps_uo_sync_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  cli_args = 'Outputs/file_base=elastic_temperature_steps_uo_sync_out Functions/top_pull_step2/expression="(t-4.5)/20" UserObjects/step_uo/step_start_times="0 4.5"'
  requirement = 'The system shall ensure that solution synchronization times are enforced by default when employing a user object to determine the steps of the simulation.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature_steps_uo_input]
  type = 'Exodiff'
  input = 'elastic_temperature_steps_uo.i'
  exodiff = 'elastic_temperature_steps_uo_input_out.e'
  cli_args = 'Materials/umat/step_user_object=step_uo Outputs/file_base=elastic_temperature_steps_uo_input_out'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence with the ability to switch boundary conditions according to the controls system using loading steps from a general user object.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature]
  type = 'Exodiff'
  input = 'elastic_temperature.i'
  cli_args = "Materials/active='umat'"
  exodiff = 'elastic_temperature_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_temperature_reference]
  type = 'Exodiff'
  input = 'elastic_temperature.i'
  cli_args = "Materials/active='elastic stress'"
  exodiff = 'elastic_temperature_out.e'
  requirement = 'The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for finite strain elasticity and temperature dependence'
[]

[elastic_dtemperature]
  type = 'Exodiff'
  input = 'elastic_dtemperature.i'
  cli_args = "Materials/active='umat'"
  exodiff = 'elastic_dtemperature_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials as constitutive models, with support for finite strain elastic material models and temperature dependence, include the temperature step increment'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[elastic_dtemperature_reference]
  type = 'Exodiff'
  input = 'elastic_dtemperature.i'
  cli_args = "Materials/active='elastic stress'"
  exodiff = 'elastic_dtemperature_out.e'
  requirement = 'The Abaqus UMAT interface shall produce the same results as the built-in MOOSE material models for finite strain elasticity and temperature dependence, including the temperature step increment'
[]

[elastic_timestep]
  type = 'Exodiff'
  input = 'elastic_timestep.i'
  exodiff = 'elastic_timestep_out.e'
  library_mode = 'DYNAMIC'
  valgrind = 'NONE'
  requirement = 'The system shall provide an interface to use Abaqus UMAT materials that allows the user to control the time step increment within the UMAT routine and combine it with MOOSE native time step controls, including cutback and growth factors, and soft terminations.'
  # skip test if test is being run out-of-tree. Issue Ref: #25279
  installation_type = in_tree
[]

[./elastic]
  type = 'CSVDiff'
  input = 'elastic_stress.i'
  csvdiff = 'elastic_stress_out.csv'

  requirement = "The ComputeDeformGradBasedStress class shall correctly compute the stress based on the lagrangian strain."
  design = "source/materials/ComputeDeformGradBasedStress.md"
  issues = "#6604"
[../]

[./elastic_Bbar]
  type = 'CSVDiff'
  input = 'elastic_stress.i'
  cli_args = 'Kernels/SolidMechanics/volumetric_locking_correction=true Materials/strain/volumetric_locking_correction=true'
  csvdiff = 'elastic_stress_out.csv'
  prereq = 'elastic'
  requirement = "The ComputeDeformGradBasedStress class shall correctly compute the stress from lagrangian strain when volumetric locking correction is used."
  design = "source/materials/ComputeDeformGradBasedStress.md VolumetricLocking.md"
  issues = "#6604"
[../]

[./interface]
  type = 'CSVDiff'
  input = 'volumetric_strain_interface.i'
  csvdiff = 'volumetric_strain_interface_out.csv'
  requirement = "The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration."
  design = "source/materials/ComputeVolumetricDeformGrad.md"
  issues = "#6604"
[../]

[./interface_Bbar]
  type = 'CSVDiff'
  input = 'volumetric_strain_interface.i'
  csvdiff = 'volumetric_strain_interface_out.csv'
  prereq = 'interface'
  cli_args = 'Kernels/SolidMechanics/volumetric_locking_correction=true Materials/strain/volumetric_locking_correction=true'
  requirement = "The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration when volumetric locking correction is used."
  design = "source/materials/ComputeVolumetricDeformGrad.md source/materials/VolumeDeformGradCorrectedStress.md VolumetricLocking.md"
  issues = "#6604"
[../]

[./interface_Bbar]
  type = 'CSVDiff'
  input = 'volumetric_strain_interface.i'
  csvdiff = 'volumetric_strain_interface_out.csv'
  prereq = 'interface'
  cli_args = 'Kernels/SolidMechanics/volumetric_locking_correction=true Materials/strain/volumetric_locking_correction=true'
  requirement = "The ComputeVolumeDeformGrad and the VolumeDeformGradCorrectedStress classes shall correctly compute the volumetric deformation gradient, total deformation gradient and transform the stress from previous configuration to the current configuration when volumetric locking correction is used."
  design = "source/materials/ComputeVolumetricDeformGrad.md source/materials/VolumeDeformGradCorrectedStress.md VolumetricLocking.md"
  issues = "#6604"
[../]

[volumetric_eigenstrain]
  type = 'CSVDiff'
  input = 'volumetric_eigenstrain.i'
  csvdiff = 'volumetric_eigenstrain_out.csv'
  requirement = "The system shall correctly compute an eigenstrain tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain."
  design = "source/materials/ComputeVolumetricEigenstrain.md RankTwoScalarAux.md"
  issues = "#8615 #11743"
[]

[volumetric_mechanical]
  type = 'CSVDiff'
  input = 'volumetric_mechanical.i'
  csvdiff = 'volumetric_mechanical_out.csv'
  requirement = "The volumetric strain computed using RankTwoScalarAux for a unit cube with imposed displacements shall be identical to that obtained by imposing an eigenstrain that causes the same deformation of that model."
  design = "source/materials/ComputeVolumetricEigenstrain.md RankTwoScalarAux.md"
  issues = "#8615 #11743"
[]

[ad_volumetric_eigenstrain]
  type = 'CSVDiff'
  input = 'ad_volumetric_eigenstrain.i'
  csvdiff = 'ad_volumetric_eigenstrain_out.csv'
  requirement = "The system shall correctly compute an eigenstrain using AD tensor that results in a solution that exactly recovers the specified volumetric expansion, and the reported volumetric strain computed by RankTwoScalarAux shall match the prescribed volumetric strain."
  design = "source/materials/ADComputeVolumetricEigenstrain.md RankTwoScalarAux.md"
  issues = "#8615 #11743 #26880"
[]

[except1]
  type = 'RunException'
  input = 'except1.i'
  expect_err = 'Weak-Plane-Shear friction angle must not be less than Weak-Plane-Shear dilation angle'
  requirement = 'The system shall not allow a weak plane shear friction angle less than the dilation angle.'
[]

[except2]
  type = 'RunException'
  input = 'except2.i'
  expect_err = 'ComputeMultiPlasticityStress: transverse_direction vector must not have zero length'
  requirement = 'The system shall not allow a zero length transverse direction vector'
[]

[small1]
  type = 'CSVDiff'
  input = 'small_deform1.i'
  csvdiff = 'small_deform1_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-3
  recover = false
  detail = 'return a value of shear of 1 and a normal stress value of 0 when the apex of the shear envelope is (0,2);'
[]

[small2]
  type = 'CSVDiff'
  input = 'small_deform2.i'
  csvdiff = 'small_deform2_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-3
  recover = false
  detail = 'utlize the small smoother parameter under both pure tension and pure shear to solve;'
[]

[small3]
  type = 'CSVDiff'
  input = 'small_deform3.i'
  csvdiff = 'small_deform3_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-6
  heavy = true
  detail = 'return the stress state to the yield surface under random loading;'
[]

[small4]
  type = 'CSVDiff'
  input = 'small_deform4.i'
  csvdiff = 'small_deform4_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-6
  recover = false
  detail = 'utilize the cap smoothing functionality under both pure tension and pure shear to solve the simulation.'
[]

[large1]
  type = 'Exodiff'
  input = 'large_deform1.i'
  exodiff = 'large_deform1_out.e'
  abs_zero = 1.0E-6
  detail = 'produce a solution without plasticity after the mesh is rotated by 90 degrees;'
[]

[large2]
  type = 'Exodiff'
  input = 'large_deform2.i'
  exodiff = 'large_deform2_out.e'
  abs_zero = 1.0E-1
  detail = 'return the stress state to the yield surface under pure tensile loading conditions after the mesh is rotated by 45 degrees;'
[]

[large3]
  type = 'CSVDiff'
  input = 'large_deform3.i'
  csvdiff = 'large_deform3_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-6
  heavy = true
  detail = 'return the stress state to the yield surface under pseudo-random loading directions;'
[]

[large4]
  type = 'CSVDiff'
  input = 'large_deform4.i'
  csvdiff = 'large_deform4_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-6
  heavy = true
  detail = 'return the stress state to the yield surface under pseudo-random loading while using the cap-tip yeild surface scheme.'
[]

[small_harden1]
  type = 'CSVDiff'
  input = 'small_deform_harden1.i'
  csvdiff = 'small_deform_harden1_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-6
  recover = false
  detail = 'with repeated stretch loading;'
[]

[small_harden2]
  type = 'CSVDiff'
  input = 'small_deform_harden2.i'
  csvdiff = 'small_deform_harden2_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-3
  recover = false
  detail = 'for pure tension and then pure shear to map out the yield function;'
[]

[small_harden3]
  type = 'CSVDiff'
  input = 'small_deform_harden3.i'
  csvdiff = 'small_deform_harden3_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-3
  recover = false
  detail = 'with linearly increasing loading and an exponential hardening model;'
[]

[small_harden4]
  type = 'CSVDiff'
  input = 'small_deform_harden4.i'
  csvdiff = 'small_deform_harden4_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-3
  recover = false
  detail = 'with a linearly increasing load and a cubic hardening model.'
[]

[large_harden3]
  type = 'CSVDiff'
  input = 'large_deform_harden3.i'
  csvdiff = 'large_deform_harden3_out.csv'
  rel_err = 1.0E-5
  abs_zero = 1.0E-3
  heavy = true
  requirement = 'The system shall return the stress state to the yield surface under random large deformation loads.'
[]

[except1]
  type = 'RunException'
  input = 'except1.i'
  expect_err = 'Weak plane tensile strength must not be negative'
  requirement = 'The system shall not allow a negative tensile strength value.'
[]

[small1]
  type = 'CSVDiff'
  input = 'small_deform1.i'
  csvdiff = 'small_deform1_out.csv'
  rel_err = 1.0E-5
  detail = 'return the stress state to the yield surface when the applied stress is above the yield surface tensile strength;'
[]

[small2]
  type = 'CSVDiff'
  input = 'small_deform2.i'
  csvdiff = 'small_deform2_out.csv'
  rel_err = 1.0E-5
  detail = 'not calculate a plastic solution because the applied stress is lower than the tension cutoff for the yield surface.'
[]

[large1]
  type = 'Exodiff'
  input = 'large_deform1.i'
  exodiff = 'large_deform1_out.e'
  abs_zero = 1.0E-6
  recover = false
  detail = 'calculate a solution without plasticity after the mesh is rotated by 90 degrees;'
[]

[large2]
  type = 'Exodiff'
  input = 'large_deform2.i'
  exodiff = 'large_deform2_out.e'
  abs_zero = 1.0E-6
  recover = false
  detail = 'return the stress state to the yield surface under pure tensile loading after the mesh is rotated by 45 degrees.'
[]

[small_hard1]
  type = 'CSVDiff'
  input = 'small_deform_hard1.i'
  csvdiff = 'small_deform_hard1_out.csv'
  rel_err = 1.0E-5
  recover = false
  detail = 'the deformation shall produce increments of plastic strain in response to incremental loading steps;'
[]

[small_hard2]
  type = 'CSVDiff'
  input = 'small_deform_hard2.i'
  csvdiff = 'small_deform_hard2_out.csv'
  rel_err = 1.0E-5
  recover = false
  detail = 'evolve the plastic internal state variable for an exponential hardening model;'
[]

[small_hard3]
  type = 'CSVDiff'
  input = 'small_deform_hard3.i'
  csvdiff = 'small_deform_hard3_out.csv'
  rel_err = 1.0E-5
  recover = false
  detail = 'return the stress state to the evolving yield surface when loaded solely in the z-direction for an exponential hardening model;'
[]

[small_hard_cubic]
  type = 'CSVDiff'
  input = 'small_deform_hard_cubic.i'
  csvdiff = 'small_deform_hard_cubic_out.csv'
  rel_err = 1.0E-5
  recover = false
  detail = 'return the stress state to the evolving yield surface when loaded solely in the z-direction for an cubic hardening model;'
[]

Introduction
Definitions and Acronyms
Design Stakeholders and Concerns
System Design
Requirements Cross - Reference
References