- index_iThe index i of ijkl for the tensor to output (0, 1, 2)
C++ Type:unsigned int
Controllable:No
Description:The index i of ijkl for the tensor to output (0, 1, 2)
- index_jThe index j of ijkl for the tensor to output (0, 1, 2)
C++ Type:unsigned int
Controllable:No
Description:The index j of ijkl for the tensor to output (0, 1, 2)
- index_kThe index k of ijkl for the tensor to output (0, 1, 2)
C++ Type:unsigned int
Controllable:No
Description:The index k of ijkl for the tensor to output (0, 1, 2)
- index_lThe index l of ijkl for the tensor to output (0, 1, 2)
C++ Type:unsigned int
Controllable:No
Description:The index l of ijkl for the tensor to output (0, 1, 2)
- rank_four_tensorThe rank four material tensor name
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:The rank four material tensor name
- variableThe name of the variable that this object applies to
C++ Type:AuxVariableName
Unit:(no unit assumed)
Controllable:No
Description:The name of the variable that this object applies to
Rank Four Aux
Access a component of a RankFourTensor
Description
The AuxKernel RankFourAux
is used to save single components of Rank-4 tensors into an AuxVariable for visualization and/or post-processing purposes, similar to the functionality provided by RankTwoAux for Rank-2 tensors RankFourAux
is commonly used to output components of the elasticity (or stiffness) tensor, Cijkl, in mechanics simulations.
The RankFourAux
takes as arguments the values of the index_i
, index_j
, index_k
, and index_l
for the single Rank-4 tensor component to save into an AuxVariable. Cijkl⟹⟹textbook notation⎣⎡C11C21C31C41C51C61C12C22C32C42C52C62C13C23C33C43C53C63C14C24C34C44C54C64C15C25C35C45C55C65C16C26C36C46C56C66⎦⎤Rank Four Aux indices⎣⎡C0000C1100C2200C1200C2000C0100C0011C1111C2211C1211C2011C0111C0022C1122C2222C1222C2022C0122C0012C1112C2212C1212C2012C0112C0020C1120C2220C1220C2020C0120C0001C1101C2201C1201C2001C0101⎦⎤(1) Eq. (1) shows the index values for a linear hyperelastic stiffness tensor with 21 independent material parameters; the various available elasticity tensor symmetry options is discussed in the material ComputeElasticityTensor documentation.
Example Input File Syntax
[./matl_C25]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
An AuxVariable is required to store the RankFourAux
AuxKernel information. Note that the name of the AuxVariable is used as the argument for the variable
input parameter in the RankFourAux
block.
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
Input Parameters
- blockThe list of blocks (ids or names) that this object will be applied
C++ Type:std::vector<SubdomainName>
Controllable:No
Description:The list of blocks (ids or names) that this object will be applied
- boundaryThe list of boundaries (ids or names) from the mesh where this object applies
C++ Type:std::vector<BoundaryName>
Controllable:No
Description:The list of boundaries (ids or names) from the mesh where this object applies
- check_boundary_restrictedTrueWhether to check for multiple element sides on the boundary in the case of a boundary restricted, element aux variable. Setting this to false will allow contribution to a single element's elemental value(s) from multiple boundary sides on the same element (example: when the restricted boundary exists on two or more sides of an element, such as at a corner of a mesh
Default:True
C++ Type:bool
Controllable:No
Description:Whether to check for multiple element sides on the boundary in the case of a boundary restricted, element aux variable. Setting this to false will allow contribution to a single element's elemental value(s) from multiple boundary sides on the same element (example: when the restricted boundary exists on two or more sides of an element, such as at a corner of a mesh
- execute_onLINEAR TIMESTEP_ENDThe list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
Default:LINEAR TIMESTEP_END
C++ Type:ExecFlagEnum
Options:XFEM_MARK, FORWARD, ADJOINT, HOMOGENEOUS_FORWARD, ADJOINT_TIMESTEP_BEGIN, ADJOINT_TIMESTEP_END, NONE, INITIAL, LINEAR, NONLINEAR_CONVERGENCE, NONLINEAR, POSTCHECK, TIMESTEP_END, TIMESTEP_BEGIN, MULTIAPP_FIXED_POINT_END, MULTIAPP_FIXED_POINT_BEGIN, FINAL, CUSTOM, PRE_DISPLACE
Controllable:No
Description:The list of flag(s) indicating when this object should be executed. For a description of each flag, see https://mooseframework.inl.gov/source/interfaces/SetupInterface.html.
Optional Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector<std::string>
Controllable:No
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Controllable:Yes
Description:Set the enabled status of the MooseObject.
- seed0The seed for the master random number generator
Default:0
C++ Type:unsigned int
Controllable:No
Description:The seed for the master random number generator
- use_displaced_meshFalseWhether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Default:False
C++ Type:bool
Controllable:No
Description:Whether or not this object should use the displaced mesh for computation. Note that in the case this is true but no displacements are provided in the Mesh block the undisplaced mesh will still be used.
Advanced Parameters
- prop_getter_suffixAn optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
C++ Type:MaterialPropertyName
Unit:(no unit assumed)
Controllable:No
Description:An optional suffix parameter that can be appended to any attempt to retrieve/get material properties. The suffix will be prepended with a '_' character.
- use_interpolated_stateFalseFor the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Default:False
C++ Type:bool
Controllable:No
Description:For the old and older state use projected material properties interpolated at the quadrature points. To set up projection use the ProjectedStatefulMaterialStorageAction.
Material Property Retrieval Parameters
Input Files
- (modules/combined/test/tests/linear_elasticity/linear_anisotropic_material.i)
- (modules/combined/examples/phase_field-mechanics/poly_grain_growth_2D_eldrforce.i)
- (modules/combined/test/tests/linear_elasticity/tensor.i)
- (modules/solid_mechanics/test/tests/crystal_plasticity/stress_update_material_based/orthotropic_rotation_Cijkl.i)
- (modules/solid_mechanics/test/tests/crystal_plasticity/monolithic_material_based/orthotropic_rotation_Cijkl.i)
- (modules/solid_mechanics/test/tests/elasticitytensor/rotation_matrix_2_rotations.i)
- (modules/solid_mechanics/test/tests/ad_linear_elasticity/tensor.i)
- (modules/solid_mechanics/test/tests/crystal_plasticity/user_object_based/orthotropic_rotation_Cijkl.i)
- (modules/combined/test/tests/concentration_dependent_elasticity_tensor/concentration_dependent_elasticity_tensor.i)
- (modules/combined/examples/phase_field-mechanics/EBSD_reconstruction_grain_growth_mech.i)
- (modules/combined/examples/phase_field-mechanics/hex_grain_growth_2D_eldrforce.i)
- (modules/combined/test/tests/ACGrGrElasticDrivingForce/bicrystal.i)
- (modules/solid_mechanics/test/tests/elasticitytensor/composite.i)
- (modules/solid_mechanics/test/tests/elasticitytensor/rotation_matrix_1_rotation.i)
(modules/combined/test/tests/linear_elasticity/tensor.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
xmin = 0
xmax = 2
ymin = 0
ymax = 2
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Physics/SolidMechanics/QuasiStatic/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1111 1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = '2'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = '0 2'
value = 0.5
[../]
[./disp_x_BC2]
type = DirichletBC
variable = disp_x
boundary = '1 3'
value = 0.01
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = '0 2'
value = 0.8
[../]
[./disp_y_BC2]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.02
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/linear_elasticity/tensor.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
xmin = 0
xmax = 2
ymin = 0
ymax = 2
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Physics/SolidMechanics/QuasiStatic/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1111 1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = '2'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = '0 2'
value = 0.5
[../]
[./disp_x_BC2]
type = DirichletBC
variable = disp_x
boundary = '1 3'
value = 0.01
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = '0 2'
value = 0.8
[../]
[./disp_y_BC2]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.02
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/linear_elasticity/linear_anisotropic_material.i)
# This input file is designed to test the LinearGeneralAnisotropicMaterial class. This test is
# for regression testing. This just takes the material properties and puts them into
# aux variables; the diffusion kernel is just to have a simple kernel to run the test.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 10
nz = 0
xmin = 0
xmax = 50
ymin = 0
ymax = 50
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./diffused]
[../]
[]
[Physics/SolidMechanics/QuasiStatic/All]
strain = SMALL
incremental = true
add_variables = true
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1.0 2.0 3.0 4.0 5.0 6.0 7.0 8.0 9.0 10.0 11.0 12.0 13.0 14.0 15.0 16.0 17.0 18.0 19.0 20.0 21.0'
[../]
[./stress]
type = ComputeStrainIncrementBasedStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = '2'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = '0 1 2 3'
value = 0.0
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = '0 1 2 3'
value = 0.0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
exodus = true
[]
(modules/combined/examples/phase_field-mechanics/poly_grain_growth_2D_eldrforce.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
nz = 0
xmax = 1000
ymax = 1000
zmax = 0
elem_type = QUAD4
uniform_refine = 2
[]
[GlobalParams]
op_num = 8
var_name_base = gr
grain_num = 36
[]
[Variables]
[./PolycrystalVariables]
[../]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[UserObjects]
[./euler_angle_file]
type = EulerAngleFileReader
file_name = grn_36_rand_2D.tex
[../]
[./voronoi]
type = PolycrystalVoronoi
coloring_algorithm = bt
[../]
[./grain_tracker]
type = GrainTrackerElasticity
threshold = 0.2
compute_var_to_feature_map = true
execute_on = 'initial timestep_begin'
flood_entity_type = ELEMENTAL
C_ijkl = '1.27e5 0.708e5 0.708e5 1.27e5 0.708e5 1.27e5 0.7355e5 0.7355e5 0.7355e5'
fill_method = symmetric9
euler_angle_provider = euler_angle_file
[../]
[]
[ICs]
[./PolycrystalICs]
[./PolycrystalColoringIC]
polycrystal_ic_uo = voronoi
[../]
[../]
[]
[AuxVariables]
[./bnds]
order = FIRST
family = LAGRANGE
[../]
[./elastic_strain11]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain22]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain12]
order = CONSTANT
family = MONOMIAL
[../]
[./unique_grains]
order = CONSTANT
family = MONOMIAL
[../]
[./var_indices]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./C1111]
order = CONSTANT
family = MONOMIAL
[../]
[./euler_angle]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./PolycrystalKernel]
[../]
[./PolycrystalElasticDrivingForce]
[../]
[./TensorMechanics]
use_displaced_mesh = true
displacements = 'disp_x disp_y'
[../]
[]
[AuxKernels]
[./BndsCalc]
type = BndsCalcAux
variable = bnds
execute_on = timestep_end
[../]
[./elastic_strain11]
type = RankTwoAux
variable = elastic_strain11
rank_two_tensor = elastic_strain
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain22]
type = RankTwoAux
variable = elastic_strain22
rank_two_tensor = elastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain12]
type = RankTwoAux
variable = elastic_strain12
rank_two_tensor = elastic_strain
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
execute_on = timestep_end
flood_counter = grain_tracker
field_display = UNIQUE_REGION
[../]
[./var_indices]
type = FeatureFloodCountAux
variable = var_indices
execute_on = timestep_end
flood_counter = grain_tracker
field_display = VARIABLE_COLORING
[../]
[./C1111]
type = RankFourAux
variable = C1111
rank_four_tensor = elasticity_tensor
index_l = 0
index_j = 0
index_k = 0
index_i = 0
execute_on = timestep_end
[../]
[./vonmises_stress]
type = RankTwoScalarAux
variable = vonmises_stress
rank_two_tensor = stress
scalar_type = VonMisesStress
execute_on = timestep_end
[../]
[./euler_angle]
type = OutputEulerAngles
variable = euler_angle
euler_angle_provider = euler_angle_file
grain_tracker = grain_tracker
output_euler_angle = 'phi1'
execute_on = 'initial timestep_end'
[../]
[]
[BCs]
[./Periodic]
[./All]
auto_direction = 'x'
variable = 'gr0 gr1 gr2 gr3 gr4 gr5 gr6 gr7'
[../]
[../]
[./top_displacement]
type = DirichletBC
variable = disp_y
boundary = top
value = -50.0
[../]
[./x_anchor]
type = DirichletBC
variable = disp_x
boundary = 'left right'
value = 0.0
[../]
[./y_anchor]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[]
[Materials]
[./Copper]
type = GBEvolution
block = 0
T = 500 # K
wGB = 15 # nm
GBmob0 = 2.5e-6 # m^4/(Js) from Schoenfelder 1997
Q = 0.23 # Migration energy in eV
GBenergy = 0.708 # GB energy in J/m^2
[../]
[./ElasticityTensor]
type = ComputePolycrystalElasticityTensor
grain_tracker = grain_tracker
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[]
[Postprocessors]
[./ngrains]
type = FeatureFloodCount
variable = bnds
threshold = 0.7
[../]
[./dofs]
type = NumDOFs
[../]
[./dt]
type = TimestepSize
[../]
[./run_time]
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
coupled_groups = 'disp_x,disp_y'
[../]
[]
[Executioner]
type = Transient
scheme = bdf2
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart -pc_hypre_boomeramg_strong_threshold'
petsc_options_value = 'hypre boomeramg 31 0.7'
l_tol = 1.0e-4
l_max_its = 30
nl_max_its = 25
nl_rel_tol = 1.0e-7
start_time = 0.0
num_steps = 50
[./TimeStepper]
type = IterationAdaptiveDT
dt = 1.5
growth_factor = 1.2
cutback_factor = 0.8
optimal_iterations = 8
[../]
[./Adaptivity]
initial_adaptivity = 2
refine_fraction = 0.8
coarsen_fraction = 0.05
max_h_level = 3
[../]
[]
[Outputs]
file_base = poly36_grtracker
exodus = true
[]
(modules/combined/test/tests/linear_elasticity/tensor.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
nz = 0
xmin = 0
xmax = 2
ymin = 0
ymax = 2
zmin = 0
zmax = 0
elem_type = QUAD4
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Physics/SolidMechanics/QuasiStatic/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[]
[Kernels]
[./diff]
type = Diffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1111 1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./stress]
type = ComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = '1'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = '2'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = '0 2'
value = 0.5
[../]
[./disp_x_BC2]
type = DirichletBC
variable = disp_x
boundary = '1 3'
value = 0.01
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = '0 2'
value = 0.8
[../]
[./disp_y_BC2]
type = DirichletBC
variable = disp_y
boundary = '1 3'
value = 0.02
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/solid_mechanics/test/tests/crystal_plasticity/stress_update_material_based/orthotropic_rotation_Cijkl.i)
# This test is designed to test the correct application of the Euler angle
# rotations to the elasticity tensor. The test uses values for the nine C_ijkl
# entries that correspond to the engineering notation placement:
# e.g. C11 = 11e3, c12 = 12e3, c13 = 13e3, c22 = 22e3 ..... c66 = 66e3
#
# A rotation of (0, 90, 0) is applied to the 1x1x1 cube, such that the values of
# c12 and c13 switch, c22 and c33 switch, and c55 and c66 switch. Postprocessors
# are used to verify this switch (made simple with the value convention above)
# and to verify that the unrotated components along the x-axis remain constant.
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[lage_xx]
order = CONSTANT
family = MONOMIAL
[]
[lage_yy]
order = CONSTANT
family = MONOMIAL
[]
[pk2_yy]
order = CONSTANT
family = MONOMIAL
[]
[lage_zz]
order = CONSTANT
family = MONOMIAL
[]
[fp_yy]
order = CONSTANT
family = MONOMIAL
[]
[c11]
order = CONSTANT
family = MONOMIAL
[]
[c12]
order = CONSTANT
family = MONOMIAL
[]
[c13]
order = CONSTANT
family = MONOMIAL
[]
[c22]
order = CONSTANT
family = MONOMIAL
[]
[c23]
order = CONSTANT
family = MONOMIAL
[]
[c33]
order = CONSTANT
family = MONOMIAL
[]
[c44]
order = CONSTANT
family = MONOMIAL
[]
[c55]
order = CONSTANT
family = MONOMIAL
[]
[c66]
order = CONSTANT
family = MONOMIAL
[]
[]
[Functions]
[tdisp]
type = ParsedFunction
expression = 0.01*t
[]
[]
[Physics/SolidMechanics/QuasiStatic]
[all]
strain = FINITE
add_variables = true
[]
[]
[AuxKernels]
[lage_xx]
type = RankTwoAux
rank_two_tensor = total_lagrangian_strain
variable = lage_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[]
[lage_yy]
type = RankTwoAux
rank_two_tensor = total_lagrangian_strain
variable = lage_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[pk2_yy]
type = RankTwoAux
variable = pk2_yy
rank_two_tensor = second_piola_kirchhoff_stress
index_j = 1
index_i = 1
execute_on = timestep_end
[]
[lage_zz]
type = RankTwoAux
rank_two_tensor = total_lagrangian_strain
variable = lage_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[]
[fp_yy]
type = RankTwoAux
variable = fp_yy
rank_two_tensor = plastic_deformation_gradient
index_i = 1
index_j = 1
execute_on = timestep_end
[]
[c11]
type = RankFourAux
variable = c11
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
execute_on = timestep_end
[]
[c12]
type = RankFourAux
variable = c12
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
execute_on = timestep_end
[]
[c13]
type = RankFourAux
variable = c13
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
execute_on = timestep_end
[]
[c22]
type = RankFourAux
variable = c22
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
execute_on = timestep_end
[]
[c23]
type = RankFourAux
variable = c23
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
execute_on = timestep_end
[]
[c33]
type = RankFourAux
variable = c33
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
execute_on = timestep_end
[]
[c44]
type = RankFourAux
variable = c44
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
execute_on = timestep_end
[]
[c55]
type = RankFourAux
variable = c55
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 0
index_k = 2
index_l = 0
execute_on = timestep_end
[]
[c66]
type = RankFourAux
variable = c66
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
execute_on = timestep_end
[]
[]
[BCs]
[bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[]
[left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[]
[back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[]
[top]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = tdisp
[]
[]
[Materials]
[elasticity_tensor]
type = ComputeElasticityTensorCP
C_ijkl = '11e3 12e3 13e3 22e3 23e3 33e3 44e3 55e3 66e3'
fill_method = symmetric9
euler_angle_1 = 0.0
euler_angle_2 = 45.0
euler_angle_3 = 45.0
[]
[stress]
type = ComputeMultipleCrystalPlasticityStress
crystal_plasticity_models = 'trial_xtalpl'
tan_mod_type = exact
[]
[trial_xtalpl]
type = CrystalPlasticityKalidindiUpdate
number_slip_systems = 12
slip_sys_file_name = input_slip_sys.txt
[]
[]
[Postprocessors]
[lage_xx]
type = ElementAverageValue
variable = lage_xx
[]
[pk2_yy]
type = ElementAverageValue
variable = pk2_yy
[]
[lage_yy]
type = ElementAverageValue
variable = lage_yy
[]
[lage_zz]
type = ElementAverageValue
variable = lage_zz
[]
[fp_yy]
type = ElementAverageValue
variable = fp_yy
[]
[c11]
type = ElementAverageValue
variable = c11
[]
[c12]
type = ElementAverageValue
variable = c12
[]
[c13]
type = ElementAverageValue
variable = c13
[]
[c22]
type = ElementAverageValue
variable = c22
[]
[c23]
type = ElementAverageValue
variable = c23
[]
[c33]
type = ElementAverageValue
variable = c33
[]
[c44]
type = ElementAverageValue
variable = c44
[]
[c55]
type = ElementAverageValue
variable = c55
[]
[c66]
type = ElementAverageValue
variable = c66
[]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_tol = 1e-3
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 1 lu gmres 200'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-10
dtmax = 0.1
dtmin = 1.0e-3
dt = 0.05
end_time = 0.5
[]
[Outputs]
exodus = false
csv = true
[]
(modules/solid_mechanics/test/tests/crystal_plasticity/monolithic_material_based/orthotropic_rotation_Cijkl.i)
# This test is designed to test the correct application of the Euler angle
# rotations to the elasticity tensor. The test uses values for the nine C_ijkl
# entries that correspond to the engineering notation placement:
# e.g. C11 = 11e3, c12 = 12e3, c13 = 13e3, c22 = 22e3 ..... c66 = 66e3
#
# A rotation of (0, 90, 0) is applied to the 1x1x1 cube, such that the values of
# c12 and c13 switch, c22 and c33 switch, and c55 and c66 switch. Postprocessors
# are used to verify this switch (made simple with the value convention above)
# and to verify that the unrotated components along the x-axis remain constant.
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./lage_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./lage_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./pk2_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./lage_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./fp_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./c11]
order = CONSTANT
family = MONOMIAL
[../]
[./c12]
order = CONSTANT
family = MONOMIAL
[../]
[./c13]
order = CONSTANT
family = MONOMIAL
[../]
[./c22]
order = CONSTANT
family = MONOMIAL
[../]
[./c23]
order = CONSTANT
family = MONOMIAL
[../]
[./c33]
order = CONSTANT
family = MONOMIAL
[../]
[./c44]
order = CONSTANT
family = MONOMIAL
[../]
[./c55]
order = CONSTANT
family = MONOMIAL
[../]
[./c66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./tdisp]
type = ParsedFunction
expression = 0.01*t
[../]
[]
[Physics/SolidMechanics/QuasiStatic]
[./all]
strain = FINITE
add_variables = true
[../]
[]
[AuxKernels]
[./lage_xx]
type = RankTwoAux
rank_two_tensor = lage
variable = lage_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./lage_yy]
type = RankTwoAux
rank_two_tensor = lage
variable = lage_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./pk2_yy]
type = RankTwoAux
variable = pk2_yy
rank_two_tensor = pk2
index_j = 1
index_i = 1
execute_on = timestep_end
[../]
[./lage_zz]
type = RankTwoAux
rank_two_tensor = lage
variable = lage_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./fp_yy]
type = RankTwoAux
variable = fp_yy
rank_two_tensor = fp
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./c11]
type = RankFourAux
variable = c11
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
execute_on = timestep_end
[../]
[./c12]
type = RankFourAux
variable = c12
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
execute_on = timestep_end
[../]
[./c13]
type = RankFourAux
variable = c13
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
execute_on = timestep_end
[../]
[./c22]
type = RankFourAux
variable = c22
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
execute_on = timestep_end
[../]
[./c23]
type = RankFourAux
variable = c23
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
execute_on = timestep_end
[../]
[./c33]
type = RankFourAux
variable = c33
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
execute_on = timestep_end
[../]
[./c44]
type = RankFourAux
variable = c44
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
execute_on = timestep_end
[../]
[./c55]
type = RankFourAux
variable = c55
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 0
index_k = 2
index_l = 0
execute_on = timestep_end
[../]
[./c66]
type = RankFourAux
variable = c66
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
execute_on = timestep_end
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = tdisp
[../]
[]
[Materials]
[./crysp]
type = FiniteStrainCrystalPlasticity
block = 0
gtol = 1e-2
slip_sys_file_name = input_slip_sys.txt
nss = 12
num_slip_sys_flowrate_props = 2 #Number of properties in a slip system
flowprops = '1 4 0.001 0.1 5 8 0.001 0.1 9 12 0.001 0.1'
hprops = '1.0 541.5 60.8 109.8 2.5'
gprops = '1 4 60.8e3 5 8 60.8e3 9 12 60.8e3'
tan_mod_type = exact
[../]
[./elasticity_tensor]
type = ComputeElasticityTensorCP
C_ijkl = '11e3 12e3 13e3 22e3 23e3 33e3 44e3 55e3 66e3'
fill_method = symmetric9
euler_angle_1 = 0.0
euler_angle_2 = 90.0
euler_angle_3 = 0.0
[../]
[]
[Postprocessors]
[./lage_xx]
type = ElementAverageValue
variable = lage_xx
[../]
[./pk2_yy]
type = ElementAverageValue
variable = pk2_yy
[../]
[./lage_yy]
type = ElementAverageValue
variable = lage_yy
[../]
[./lage_zz]
type = ElementAverageValue
variable = lage_zz
[../]
[./fp_yy]
type = ElementAverageValue
variable = fp_yy
[../]
[./c11]
type = ElementAverageValue
variable = c11
[../]
[./c12]
type = ElementAverageValue
variable = c12
[../]
[./c13]
type = ElementAverageValue
variable = c13
[../]
[./c22]
type = ElementAverageValue
variable = c22
[../]
[./c23]
type = ElementAverageValue
variable = c23
[../]
[./c33]
type = ElementAverageValue
variable = c33
[../]
[./c44]
type = ElementAverageValue
variable = c44
[../]
[./c55]
type = ElementAverageValue
variable = c55
[../]
[./c66]
type = ElementAverageValue
variable = c66
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_tol = 1e-3
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 1 lu gmres 200'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-10
dtmax = 0.1
dtmin = 1.0e-3
dt = 0.05
end_time = 0.5
[]
[Outputs]
exodus = false
csv = true
[]
(modules/solid_mechanics/test/tests/elasticitytensor/rotation_matrix_2_rotations.i)
# This input file is designed to rotate an elasticity tensor both with euler angles
# and a rotation matrix. The rotated tensor components should match between the
# two methods.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmax = 1
[]
[AuxVariables]
[./C1111_aux_matrix] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_matrix] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_matrix] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_matrix] # C16
order = CONSTANT
family = MONOMIAL
[../]
[./C1111_aux_euler] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_euler] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_euler] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_euler] # C16
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_C1111_matrix] # C11
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_matrix
execute_on = initial
[../]
[./matl_C1122_matrix] # C12
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_matrix
execute_on = initial
[../]
[./matl_C1133_matrix] # C13
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_matrix
execute_on = initial
[../]
[./matl_C1112_matrix] # C16
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_matrix
execute_on = initial
[../]
[./matl_C1111_euler] # C11
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_euler
execute_on = initial
[../]
[./matl_C1122_euler] # C12
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_euler
execute_on = initial
[../]
[./matl_C1133_euler] # C13
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_euler
execute_on = initial
[../]
[./matl_C1112_euler] # C16
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_euler
execute_on = initial
[../]
[]
[Materials]
[./elasticity_matrix]
type = ComputeElasticityTensor
block = 0
base_name = 'rotation_matrix'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
# rotation matrix for rotating a vector
# 1. 45 degrees about z-axis
# 2. ~54.7 degrees (arccos(1/sqrt(3)) radians) about x-axis
# then taking the tranpose to give sample-to-crystal rotation,
# ie. R*([0,0,1]) = [1,1,1], meaning the <001> direction of the sample
# (or simulation) frame points along the <111> direction of the crystal
rotation_matrix = '0.70710678 0.40824829 0.57735027
-0.70710678 0.40824829 0.57735027
0. -0.81649658 0.57735027'
[../]
[./elasticity_euler]
type = ComputeElasticityTensor
block = 0
base_name = 'euler'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
# the angles here are the same as used to build the rotation matrix above because
# we build the _transpose_ from euler angles in MOOSE, but we also transposed
# the matrix for this example, so it goes back to the original;
# the reversed order is due to the "extrinsic" convention used by MOOSE
euler_angle_1 = 0.
euler_angle_2 = 54.73561032
euler_angle_3 = 45.
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
# corresponding values in "matrix" and "euler" postprocessors should match
[./C11_matrix]
type = ElementAverageValue
variable = C1111_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_matrix]
type = ElementAverageValue
variable = C1122_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_matrix]
type = ElementAverageValue
variable = C1133_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_matrix]
type = ElementAverageValue
variable = C1112_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C11_euler]
type = ElementAverageValue
variable = C1111_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_euler]
type = ElementAverageValue
variable = C1122_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_euler]
type = ElementAverageValue
variable = C1133_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_euler]
type = ElementAverageValue
variable = C1112_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[]
[Outputs]
exodus = true
[]
(modules/solid_mechanics/test/tests/ad_linear_elasticity/tensor.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[Mesh]
type = GeneratedMesh
dim = 2
nx = 2
ny = 2
xmax = 2
ymax = 2
[]
[Variables]
[./diffused]
[./InitialCondition]
type = RandomIC
[../]
[../]
[]
[AuxVariables]
[./C11]
order = CONSTANT
family = MONOMIAL
[../]
[./C12]
order = CONSTANT
family = MONOMIAL
[../]
[./C13]
order = CONSTANT
family = MONOMIAL
[../]
[./C14]
order = CONSTANT
family = MONOMIAL
[../]
[./C15]
order = CONSTANT
family = MONOMIAL
[../]
[./C16]
order = CONSTANT
family = MONOMIAL
[../]
[./C22]
order = CONSTANT
family = MONOMIAL
[../]
[./C23]
order = CONSTANT
family = MONOMIAL
[../]
[./C24]
order = CONSTANT
family = MONOMIAL
[../]
[./C25]
order = CONSTANT
family = MONOMIAL
[../]
[./C26]
order = CONSTANT
family = MONOMIAL
[../]
[./C33]
order = CONSTANT
family = MONOMIAL
[../]
[./C34]
order = CONSTANT
family = MONOMIAL
[../]
[./C35]
order = CONSTANT
family = MONOMIAL
[../]
[./C36]
order = CONSTANT
family = MONOMIAL
[../]
[./C44]
order = CONSTANT
family = MONOMIAL
[../]
[./C45]
order = CONSTANT
family = MONOMIAL
[../]
[./C46]
order = CONSTANT
family = MONOMIAL
[../]
[./C55]
order = CONSTANT
family = MONOMIAL
[../]
[./C56]
order = CONSTANT
family = MONOMIAL
[../]
[./C66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Physics/SolidMechanics/QuasiStatic/All]
strain = SMALL
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
use_automatic_differentiation = true
[]
[Kernels]
[./diff]
type = ADDiffusion
variable = diffused
[../]
[]
[AuxKernels]
[./matl_C11]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C11
[../]
[./matl_C12]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C12
[../]
[./matl_C13]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C13
[../]
[./matl_C14]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 2
variable = C14
[../]
[./matl_C15]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 2
variable = C15
[../]
[./matl_C16]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C16
[../]
[./matl_C22]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
variable = C22
[../]
[./matl_C23]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
variable = C23
[../]
[./matl_C24]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 2
variable = C24
[../]
[./matl_C25]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 2
variable = C25
[../]
[./matl_C26]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 0
index_l = 1
variable = C26
[../]
[./matl_C33]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
variable = C33
[../]
[./matl_C34]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 1
index_l = 2
variable = C34
[../]
[./matl_C35]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C35
[../]
[./matl_C36]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 1
variable = C36
[../]
[./matl_C44]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
variable = C44
[../]
[./matl_C45]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 2
variable = C45
[../]
[./matl_C46]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 0
index_l = 1
variable = C46
[../]
[./matl_C55]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 2
variable = C55
[../]
[./matl_C56]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 2
index_k = 0
index_l = 1
variable = C56
[../]
[./matl_C66]
type = ADRankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
variable = C66
[../]
[]
[Materials]
[./elasticity_tensor]
type = ADComputeElasticityTensor
fill_method = symmetric21
C_ijkl ='1111 1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./stress]
type = ADComputeLinearElasticStress
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = diffused
boundary = 'right'
value = 1
[../]
[./top]
type = DirichletBC
variable = diffused
boundary = 'top'
value = 0
[../]
[./disp_x_BC]
type = DirichletBC
variable = disp_x
boundary = 'bottom top'
value = 0.5
[../]
[./disp_x_BC2]
type = DirichletBC
variable = disp_x
boundary = 'left right'
value = 0.01
[../]
[./disp_y_BC]
type = DirichletBC
variable = disp_y
boundary = 'bottom top'
value = 0.8
[../]
[./disp_y_BC2]
type = DirichletBC
variable = disp_y
boundary = 'left right'
value = 0.02
[../]
[]
[Preconditioning]
[./full]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = 'PJFNK'
[]
[Outputs]
exodus = true
[]
(modules/solid_mechanics/test/tests/crystal_plasticity/user_object_based/orthotropic_rotation_Cijkl.i)
# This test is designed to test the correct application of the Euler angle
# rotations to the elasticity tensor. The test uses values for the nine C_ijkl
# entries that correspond to the engineering notation placement:
# e.g. C11 = 11e3, c12 = 12e3, c13 = 13e3, c22 = 22e3 ..... c66 = 66e3
#
# A rotation of (0, 90, 0) is applied to the 1x1x1 cube, such that the values of
# c12 and c13 switch, c22 and c33 switch, and c55 and c66 switch. Postprocessors
# are used to verify this switch (made simple with the value convention above)
# and to verify that the unrotated components along the x-axis remain constant.
[Mesh]
type = GeneratedMesh
dim = 3
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[AuxVariables]
[./lage_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./lage_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./pk2_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./lage_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./fp_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./c11]
order = CONSTANT
family = MONOMIAL
[../]
[./c12]
order = CONSTANT
family = MONOMIAL
[../]
[./c13]
order = CONSTANT
family = MONOMIAL
[../]
[./c22]
order = CONSTANT
family = MONOMIAL
[../]
[./c23]
order = CONSTANT
family = MONOMIAL
[../]
[./c33]
order = CONSTANT
family = MONOMIAL
[../]
[./c44]
order = CONSTANT
family = MONOMIAL
[../]
[./c55]
order = CONSTANT
family = MONOMIAL
[../]
[./c66]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./tdisp]
type = ParsedFunction
expression = 0.01*t
[../]
[]
[Physics/SolidMechanics/QuasiStatic]
[./all]
strain = FINITE
add_variables = true
[../]
[]
[AuxKernels]
[./lage_xx]
type = RankTwoAux
rank_two_tensor = lage
variable = lage_xx
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./lage_yy]
type = RankTwoAux
rank_two_tensor = lage
variable = lage_yy
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./pk2_yy]
type = RankTwoAux
variable = pk2_yy
rank_two_tensor = pk2
index_j = 1
index_i = 1
execute_on = timestep_end
[../]
[./lage_zz]
type = RankTwoAux
rank_two_tensor = lage
variable = lage_zz
index_i = 2
index_j = 2
execute_on = timestep_end
[../]
[./fp_yy]
type = RankTwoAux
variable = fp_yy
rank_two_tensor = fp
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./c11]
type = RankFourAux
variable = c11
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
execute_on = timestep_end
[../]
[./c12]
type = RankFourAux
variable = c12
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
execute_on = timestep_end
[../]
[./c13]
type = RankFourAux
variable = c13
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
execute_on = timestep_end
[../]
[./c22]
type = RankFourAux
variable = c22
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 1
index_l = 1
execute_on = timestep_end
[../]
[./c23]
type = RankFourAux
variable = c23
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 1
index_k = 2
index_l = 2
execute_on = timestep_end
[../]
[./c33]
type = RankFourAux
variable = c33
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 2
index_l = 2
execute_on = timestep_end
[../]
[./c44]
type = RankFourAux
variable = c44
rank_four_tensor = elasticity_tensor
index_i = 1
index_j = 2
index_k = 1
index_l = 2
execute_on = timestep_end
[../]
[./c55]
type = RankFourAux
variable = c55
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 0
index_k = 2
index_l = 0
execute_on = timestep_end
[../]
[./c66]
type = RankFourAux
variable = c66
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 1
index_k = 0
index_l = 1
execute_on = timestep_end
[../]
[]
[BCs]
[./bottom]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = back
value = 0
[../]
[./top]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = tdisp
[../]
[]
[Materials]
[./crysp]
type = FiniteStrainUObasedCP
stol = 1e-2
tan_mod_type = exact
uo_slip_rates = 'slip_rate_gss'
uo_slip_resistances = 'slip_resistance_gss'
uo_state_vars = 'state_var_gss'
uo_state_var_evol_rate_comps = 'state_var_evol_rate_comp_gss'
[../]
[./elasticity_tensor]
type = ComputeElasticityTensorCP
C_ijkl = '11e3 12e3 13e3 22e3 23e3 33e3 44e3 55e3 66e3'
fill_method = symmetric9
euler_angle_1 = 0.0
euler_angle_2 = 45.0
euler_angle_3 = 45.0
[../]
[]
[UserObjects]
[./slip_rate_gss]
type = CrystalPlasticitySlipRateGSS
variable_size = 12
slip_sys_file_name = input_slip_sys.txt
num_slip_sys_flowrate_props = 2
flowprops = '1 4 0.001 0.1 5 8 0.001 0.1 9 12 0.001 0.1'
uo_state_var_name = state_var_gss
[../]
[./slip_resistance_gss]
type = CrystalPlasticitySlipResistanceGSS
variable_size = 12
uo_state_var_name = state_var_gss
[../]
[./state_var_gss]
type = CrystalPlasticityStateVariable
variable_size = 12
groups = '0 4 8 12'
group_values = '60.8 60.8 60.8' #strength units in MPa
uo_state_var_evol_rate_comp_name = state_var_evol_rate_comp_gss
scale_factor = 1.0
[../]
[./state_var_evol_rate_comp_gss]
type = CrystalPlasticityStateVarRateComponentGSS
variable_size = 12
hprops = '1.0 541.5 109.8 2.5'
uo_slip_rate_name = slip_rate_gss
uo_state_var_name = state_var_gss
[../]
[]
[Postprocessors]
[./lage_xx]
type = ElementAverageValue
variable = lage_xx
[../]
[./pk2_yy]
type = ElementAverageValue
variable = pk2_yy
[../]
[./lage_yy]
type = ElementAverageValue
variable = lage_yy
[../]
[./lage_zz]
type = ElementAverageValue
variable = lage_zz
[../]
[./fp_yy]
type = ElementAverageValue
variable = fp_yy
[../]
[./c11]
type = ElementAverageValue
variable = c11
[../]
[./c12]
type = ElementAverageValue
variable = c12
[../]
[./c13]
type = ElementAverageValue
variable = c13
[../]
[./c22]
type = ElementAverageValue
variable = c22
[../]
[./c23]
type = ElementAverageValue
variable = c23
[../]
[./c33]
type = ElementAverageValue
variable = c33
[../]
[./c44]
type = ElementAverageValue
variable = c44
[../]
[./c55]
type = ElementAverageValue
variable = c55
[../]
[./c66]
type = ElementAverageValue
variable = c66
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
l_tol = 1e-3
petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
petsc_options_value = ' asm 1 lu gmres 200'
nl_abs_tol = 1e-10
nl_rel_tol = 1e-10
dtmax = 0.1
dtmin = 1.0e-3
dt = 0.05
end_time = 0.5
[]
[Outputs]
exodus = false
csv = true
[]
(modules/combined/test/tests/concentration_dependent_elasticity_tensor/concentration_dependent_elasticity_tensor.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 20
xmin = -0.5
ymin = -0.5
xmax = 0.5
ymax = 0.5
elem_type = QUAD4
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[Kernels]
[./TensorMechanics]
disp_x = disp_x
disp_y = disp_y
[../]
[]
[AuxVariables]
[./c]
[../]
[./C11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./s11_aux]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_s11]
type = RankTwoAux
variable = s11_aux
rank_two_tensor = stress
index_i = 0
index_j = 0
[../]
[./matl_C11]
type = RankFourAux
variable = C11_aux
rank_four_tensor = elasticity_tensor
index_l = 0
index_j = 0
index_k = 0
index_i = 0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeConcentrationDependentElasticityTensor
block = 0
c = c
C1_ijkl = '6 6'
C0_ijkl = '1 1'
fill_method1 = symmetric_isotropic
fill_method0 = symmetric_isotropic
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[./strain]
type = ComputeSmallStrain
block = 0
disp_x = disp_x
disp_y = disp_y
[../]
[]
[BCs]
[./bottom_y]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0
[../]
[./left_x]
type = DirichletBC
variable = disp_x
boundary = left
value = 0
[../]
[./right_x]
type = DirichletBC
variable = disp_x
boundary = right
value = 0
[../]
[./top_y]
type = DirichletBC
variable = disp_y
boundary = top
value = 0.5
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
full = true
[../]
[]
[Executioner]
type = Steady
solve_type = NEWTON
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
petsc_options_value = 'hypre boomeramg 31'
l_max_its = 20
nl_max_its = 10
l_tol = 1.0e-4
nl_rel_tol = 1.0e-6
nl_abs_tol = 1.0e-8
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
[ICs]
[./c_IC]
int_width = 0.2
x1 = 0
y1 = 0
radius = 0.25
outvalue = 0
variable = c
invalue = 1
type = SmoothCircleIC
[../]
[]
(modules/combined/examples/phase_field-mechanics/EBSD_reconstruction_grain_growth_mech.i)
# This example reconstructs the grain structure from an EBSD data file
# Then, an isotropic grain model is run with linear elasticity and an anisotropic
# elasticity tensor that uses the measured EBSD angles.
[Mesh]
[ebsd_mesh]
type = EBSDMeshGenerator
uniform_refine = 2 #Mesh can go two levels coarser than the EBSD grid
filename = IN100_128x128.txt
[]
[]
[GlobalParams]
op_num = 8
var_name_base = gr
displacements = 'disp_x disp_y'
[]
[Variables]
[PolycrystalVariables] #Polycrystal variable generation (30 order parameters)
[]
[disp_x]
[]
[disp_y]
[]
[]
[AuxVariables]
[bnds]
[]
[gt_indices]
order = CONSTANT
family = MONOMIAL
[]
[unique_grains]
order = CONSTANT
family = MONOMIAL
[]
[vonmises_stress]
order = CONSTANT
family = MONOMIAL
[]
[C1111]
order = CONSTANT
family = MONOMIAL
[]
[phi1]
order = CONSTANT
family = MONOMIAL
[]
[Phi]
order = CONSTANT
family = MONOMIAL
[]
[phi2]
order = CONSTANT
family = MONOMIAL
[]
[EBSD_grain]
family = MONOMIAL
order = CONSTANT
[]
[]
[ICs]
[PolycrystalICs]
[ReconVarIC]
ebsd_reader = ebsd
coloring_algorithm = bt
[]
[]
[]
[Kernels]
[PolycrystalKernel]
[]
[PolycrystalElasticDrivingForce]
[]
[TensorMechanics]
[]
[]
[AuxKernels]
[BndsCalc]
type = BndsCalcAux
variable = bnds
execute_on = 'initial timestep_end'
[]
[gt_indices]
type = FeatureFloodCountAux
variable = gt_indices
execute_on = 'initial timestep_end'
flood_counter = grain_tracker
field_display = VARIABLE_COLORING
[]
[unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
execute_on = 'initial timestep_end'
flood_counter = grain_tracker
field_display = UNIQUE_REGION
[]
[C1111]
type = RankFourAux
variable = C1111
rank_four_tensor = elasticity_tensor
index_l = 0
index_j = 0
index_k = 0
index_i = 0
execute_on = timestep_end
[]
[vonmises_stress]
type = RankTwoScalarAux
variable = vonmises_stress
rank_two_tensor = stress
scalar_type = VonMisesStress
execute_on = timestep_end
[]
[phi1]
type = OutputEulerAngles
variable = phi1
euler_angle_provider = ebsd
grain_tracker = grain_tracker
output_euler_angle = 'phi1'
execute_on = 'initial'
[]
[Phi]
type = OutputEulerAngles
variable = Phi
euler_angle_provider = ebsd
grain_tracker = grain_tracker
output_euler_angle = 'Phi'
execute_on = 'initial'
[]
[phi2]
type = OutputEulerAngles
variable = phi2
euler_angle_provider = ebsd
grain_tracker = grain_tracker
output_euler_angle = 'phi2'
execute_on = 'initial'
[]
[grain_aux]
type = EBSDReaderPointDataAux
variable = EBSD_grain
ebsd_reader = ebsd
data_name = 'feature_id'
execute_on = 'initial'
[]
[]
[BCs]
[top_displacement]
type = DirichletBC
variable = disp_y
boundary = top
value = -2.0
[]
[x_anchor]
type = DirichletBC
variable = disp_x
boundary = 'left right'
value = 0.0
[]
[y_anchor]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[]
[]
[Modules]
[PhaseField]
[EulerAngles2RGB]
crystal_structure = cubic
euler_angle_provider = ebsd
grain_tracker = grain_tracker
[]
[]
[]
[Materials]
[Copper]
# T = 500 # K
type = GBEvolution
block = 0
T = 500
wGB = 0.6 # um
GBmob0 = 2.5e-6 # m^4/(Js) from Schoenfelder 1997
Q = 0.23 # Migration energy in eV
GBenergy = 0.708 # GB energy in J/m^2
molar_volume = 7.11e-6; # Molar volume in m^3/mol
length_scale = 1.0e-6
time_scale = 1.0e-6
[]
[ElasticityTensor]
type = ComputePolycrystalElasticityTensor
grain_tracker = grain_tracker
[]
[strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y'
[]
[stress]
type = ComputeLinearElasticStress
block = 0
[]
[]
[Postprocessors]
[dt]
type = TimestepSize
[]
[n_elements]
type = NumElements
execute_on = 'initial timestep_end'
[]
[n_nodes]
type = NumNodes
execute_on = 'initial timestep_end'
[]
[DOFs]
type = NumDOFs
[]
[]
[UserObjects]
[ebsd]
type = EBSDReader
[]
[grain_tracker]
type = GrainTrackerElasticity
compute_var_to_feature_map = true
ebsd_reader = ebsd
fill_method = symmetric9
C_ijkl = '1.27e5 0.708e5 0.708e5 1.27e5 0.708e5 1.27e5 0.7355e5 0.7355e5 0.7355e5'
euler_angle_provider = ebsd
[]
[]
[Executioner]
type = Transient
scheme = bdf2
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type -pc_hypre_boomeramg_strong_threshold'
petsc_options_value = ' hypre boomeramg 0.7'
l_tol = 1.0e-4
l_max_its = 20
nl_max_its = 20
nl_rel_tol = 1.0e-8
start_time = 0.0
num_steps = 30
dt = 10
[Adaptivity]
initial_adaptivity = 0
refine_fraction = 0.7
coarsen_fraction = 0.1
max_h_level = 2
[]
[TimeStepper]
type = IterationAdaptiveDT
cutback_factor = 0.9
dt = 10.0
growth_factor = 1.1
optimal_iterations = 7
[]
[]
[Outputs]
csv = true
exodus = true
[]
(modules/combined/examples/phase_field-mechanics/hex_grain_growth_2D_eldrforce.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 20
ny = 17
nz = 0
xmax = 1000
ymax = 866
zmax = 0
elem_type = QUAD4
uniform_refine = 2
[]
[GlobalParams]
op_num = 3
var_name_base = gr
[]
[Variables]
[./PolycrystalVariables]
[../]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[UserObjects]
[./hex_ic]
type = PolycrystalHex
coloring_algorithm = bt
grain_num = 36
x_offset = 0.0
output_adjacency_matrix = true
[../]
[./euler_angle_file]
type = EulerAngleFileReader
file_name = grn_36_test2_2D.tex
[../]
[./grain_tracker]
type = GrainTrackerElasticity
threshold = 0.2
compute_var_to_feature_map = true
execute_on = 'initial timestep_begin'
flood_entity_type = ELEMENTAL
fill_method = symmetric9
C_ijkl = '1.27e5 0.708e5 0.708e5 1.27e5 0.708e5 1.27e5 0.7355e5 0.7355e5 0.7355e5'
euler_angle_provider = euler_angle_file
[../]
[]
[ICs]
[./PolycrystalICs]
[./PolycrystalColoringIC]
polycrystal_ic_uo = hex_ic
[../]
[../]
[]
[AuxVariables]
[./bnds]
order = FIRST
family = LAGRANGE
[../]
[./elastic_strain11]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain22]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain12]
order = CONSTANT
family = MONOMIAL
[../]
[./unique_grains]
order = CONSTANT
family = MONOMIAL
[../]
[./var_indices]
order = CONSTANT
family = MONOMIAL
[../]
[./C1111]
order = CONSTANT
family = MONOMIAL
[../]
[./vonmises_stress]
order = CONSTANT
family = MONOMIAL
[../]
[./euler_angle]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./PolycrystalKernel]
[../]
[./PolycrystalElasticDrivingForce]
[../]
[./TensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[AuxKernels]
[./BndsCalc]
type = BndsCalcAux
variable = bnds
execute_on = 'initial timestep_end'
[../]
[./elastic_strain11]
type = RankTwoAux
variable = elastic_strain11
rank_two_tensor = elastic_strain
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain22]
type = RankTwoAux
variable = elastic_strain22
rank_two_tensor = elastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain12]
type = RankTwoAux
variable = elastic_strain12
rank_two_tensor = elastic_strain
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
execute_on = timestep_end
flood_counter = grain_tracker
field_display = UNIQUE_REGION
[../]
[./var_indices]
type = FeatureFloodCountAux
variable = var_indices
execute_on = timestep_end
flood_counter = grain_tracker
field_display = VARIABLE_COLORING
[../]
[./C1111]
type = RankFourAux
variable = C1111
rank_four_tensor = elasticity_tensor
index_l = 0
index_j = 0
index_k = 0
index_i = 0
execute_on = timestep_end
[../]
[./vonmises_stress]
type = RankTwoScalarAux
variable = vonmises_stress
rank_two_tensor = stress
scalar_type = VonMisesStress
[../]
[./euler_angle]
type = OutputEulerAngles
variable = euler_angle
euler_angle_provider = euler_angle_file
grain_tracker = grain_tracker
output_euler_angle = 'phi1'
[../]
[]
[BCs]
[./Periodic]
[./All]
auto_direction = 'x y'
variable = 'gr0 gr1 gr2'
[../]
[../]
[./top_displacement]
type = DirichletBC
variable = disp_y
boundary = top
value = -50.0
[../]
[./x_anchor]
type = DirichletBC
variable = disp_x
boundary = 'left right'
value = 0.0
[../]
[./y_anchor]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[]
[Materials]
[./Copper]
type = GBEvolution
block = 0
T = 500 # K
wGB = 15 # nm
GBmob0 = 2.5e-6 # m^4/(Js) from Schoenfelder 1997
Q = 0.23 # Migration energy in eV
GBenergy = 0.708 # GB energy in J/m^2
[../]
[./ElasticityTensor]
type = ComputePolycrystalElasticityTensor
block = 0
grain_tracker = grain_tracker
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[]
[Postprocessors]
[./dofs]
type = NumDOFs
[../]
[./dt]
type = TimestepSize
[../]
[./run_time]
type = PerfGraphData
section_name = "Root"
data_type = total
[../]
[./bnd_length]
type = GrainBoundaryArea
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
off_diag_row = 'disp_x disp_y'
off_diag_column = 'disp_y disp_x'
[../]
[]
[Executioner]
type = Transient
scheme = bdf2
solve_type = PJFNK
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart -pc_hypre_boomeramg_strong_threshold'
petsc_options_value = 'hypre boomeramg 31 0.7'
l_tol = 1.0e-4
l_max_its = 30
nl_max_its = 40
nl_rel_tol = 1.0e-7
start_time = 0.0
num_steps = 50
[./TimeStepper]
type = IterationAdaptiveDT
dt = 1.5
growth_factor = 1.2
cutback_factor = 0.8
optimal_iterations = 8
[../]
[./Adaptivity]
initial_adaptivity = 2
refine_fraction = 0.8
coarsen_fraction = 0.05
max_h_level = 3
[../]
[]
[Outputs]
exodus = true
[]
(modules/combined/test/tests/ACGrGrElasticDrivingForce/bicrystal.i)
[Mesh]
type = GeneratedMesh
dim = 2
nx = 10
ny = 3
xmax = 1000
ymax = 1000
elem_type = QUAD4
uniform_refine = 2
[]
[GlobalParams]
op_num = 2
var_name_base = gr
[]
[Variables]
[./PolycrystalVariables]
[../]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[ICs]
[./PolycrystalICs]
[./BicrystalBoundingBoxIC]
x1 = 0
y1 = 0
x2 = 500
y2 = 1000
[../]
[../]
[]
[AuxVariables]
[./bnds]
order = FIRST
family = LAGRANGE
[../]
[./elastic_strain11]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain22]
order = CONSTANT
family = MONOMIAL
[../]
[./elastic_strain12]
order = CONSTANT
family = MONOMIAL
[../]
[./unique_grains]
order = CONSTANT
family = MONOMIAL
[../]
[./var_indices]
order = CONSTANT
family = MONOMIAL
[../]
[./C1111]
order = CONSTANT
family = MONOMIAL
[../]
[./active_bounds_elemental]
order = CONSTANT
family = MONOMIAL
[../]
[./euler_angle]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./PolycrystalKernel]
[../]
[./PolycrystalElasticDrivingForce]
[../]
[./TensorMechanics]
displacements = 'disp_x disp_y'
[../]
[]
[AuxKernels]
[./bnds_aux]
type = BndsCalcAux
variable = bnds
execute_on = timestep_end
[../]
[./elastic_strain11]
type = RankTwoAux
variable = elastic_strain11
rank_two_tensor = elastic_strain
index_i = 0
index_j = 0
execute_on = timestep_end
[../]
[./elastic_strain22]
type = RankTwoAux
variable = elastic_strain22
rank_two_tensor = elastic_strain
index_i = 1
index_j = 1
execute_on = timestep_end
[../]
[./elastic_strain12]
type = RankTwoAux
variable = elastic_strain12
rank_two_tensor = elastic_strain
index_i = 0
index_j = 1
execute_on = timestep_end
[../]
[./unique_grains]
type = FeatureFloodCountAux
variable = unique_grains
flood_counter = grain_tracker
execute_on = 'initial timestep_begin'
field_display = UNIQUE_REGION
[../]
[./var_indices]
type = FeatureFloodCountAux
variable = var_indices
flood_counter = grain_tracker
execute_on = 'initial timestep_begin'
field_display = VARIABLE_COLORING
[../]
[./C1111]
type = RankFourAux
variable = C1111
rank_four_tensor = elasticity_tensor
index_l = 0
index_j = 0
index_k = 0
index_i = 0
execute_on = timestep_end
[../]
[./active_bounds_elemental]
type = FeatureFloodCountAux
variable = active_bounds_elemental
field_display = ACTIVE_BOUNDS
execute_on = 'initial timestep_begin'
flood_counter = grain_tracker
[../]
[./euler_angle]
type = OutputEulerAngles
variable = euler_angle
euler_angle_provider = euler_angle_file
grain_tracker = grain_tracker
output_euler_angle = 'phi1'
[../]
[]
[BCs]
[./top_displacement]
type = DirichletBC
variable = disp_y
boundary = top
value = -10.0
[../]
[./x_anchor]
type = DirichletBC
variable = disp_x
boundary = 'left right'
value = 0.0
[../]
[./y_anchor]
type = DirichletBC
variable = disp_y
boundary = bottom
value = 0.0
[../]
[]
[Materials]
[./Copper]
type = GBEvolution
block = 0
T = 500 # K
wGB = 75 # nm
GBmob0 = 2.5e-6 #m^4/(Js) from Schoenfelder 1997
Q = 0.23 #Migration energy in eV
GBenergy = 0.708 #GB energy in J/m^2
time_scale = 1.0e-6
[../]
[./ElasticityTensor]
type = ComputePolycrystalElasticityTensor
grain_tracker = grain_tracker
[../]
[./strain]
type = ComputeSmallStrain
block = 0
displacements = 'disp_x disp_y'
[../]
[./stress]
type = ComputeLinearElasticStress
block = 0
[../]
[]
[UserObjects]
[./euler_angle_file]
type = EulerAngleFileReader
file_name = test.tex
[../]
[./grain_tracker]
type = GrainTrackerElasticity
connecting_threshold = 0.05
compute_var_to_feature_map = true
flood_entity_type = elemental
execute_on = 'initial timestep_begin'
euler_angle_provider = euler_angle_file
fill_method = symmetric9
C_ijkl = '1.27e5 0.708e5 0.708e5 1.27e5 0.708e5 1.27e5 0.7355e5 0.7355e5 0.7355e5'
outputs = none
[../]
[]
[Postprocessors]
[./dt]
type = TimestepSize
[../]
[./gr0_area]
type = ElementIntegralVariablePostprocessor
variable = gr0
[../]
[]
[Preconditioning]
[./SMP]
type = SMP
coupled_groups = 'gr0,gr1 disp_x,disp_y'
[../]
[]
[Executioner]
type = Transient
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart -pc_hypre_boomeramg_strong_threshold'
petsc_options_value = 'hypre boomeramg 31 0.7'
l_max_its = 30
l_tol = 1e-4
nl_max_its = 30
nl_rel_tol = 1e-9
start_time = 0.0
num_steps = 3
dt = 0.2
[./Adaptivity]
initial_adaptivity = 2
refine_fraction = 0.7
coarsen_fraction = 0.1
max_h_level = 2
[../]
[]
[Outputs]
execute_on = 'timestep_end'
exodus = true
[]
(modules/solid_mechanics/test/tests/elasticitytensor/composite.i)
# This input file is designed to test the RankTwoAux and RankFourAux
# auxkernels, which report values out of the Tensors used in materials
# properties.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmax = 1
[]
[AuxVariables]
[./c]
order = FIRST
family = LAGRANGE
[./InitialCondition]
type = FunctionIC
function = x
[../]
[../]
[./C1111_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./C3313_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC1111_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC1122_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC1133_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./dC3313_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C1111_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C1122_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C1133_aux]
order = CONSTANT
family = MONOMIAL
[../]
[./d2C3313_aux]
order = CONSTANT
family = MONOMIAL
[../]
[]
#[Kernels]
# [./diff]
# type = Diffusion
# variable = diffused
# [../]
#[]
[AuxKernels]
[./matl_C1111]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux
execute_on = initial
[../]
[./matl_C1122]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux
execute_on = initial
[../]
[./matl_C1133]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux
execute_on = initial
[../]
[./matl_C3313]
type = RankFourAux
rank_four_tensor = elasticity_tensor
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = C3313_aux
execute_on = initial
[../]
[./matl_dC1111]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = dC1111_aux
execute_on = initial
[../]
[./matl_dC1122]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = dC1122_aux
execute_on = initial
[../]
[./matl_dC1133]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = dC1133_aux
execute_on = initial
[../]
[./matl_dC3313]
type = RankFourAux
rank_four_tensor = delasticity_tensor/dc
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = dC3313_aux
execute_on = initial
[../]
[./matl_d2C1111]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = d2C1111_aux
execute_on = initial
[../]
[./matl_d2C1122]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = d2C1122_aux
execute_on = initial
[../]
[./matl_d2C1133]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = d2C1133_aux
execute_on = initial
[../]
[./matl_d2C3313]
type = RankFourAux
rank_four_tensor = d^2elasticity_tensor/dc^2
index_i = 2
index_j = 2
index_k = 0
index_l = 2
variable = d2C3313_aux
execute_on = initial
[../]
[]
[Materials]
[./Ca]
type = ComputeElasticityTensor
base_name = Ca
block = 0
fill_method = symmetric21
C_ijkl ='1111 .1122 1133 1123 1113 1112 2222 2233 2223 2213 2212 3333 3323 3313 3312 2323 2313 2312 1313 1312 1212'
[../]
[./Cb]
type = ComputeElasticityTensor
base_name = Cb
block = 0
fill_method = symmetric21
C_ijkl ='.1111 1122 .1133 .1123 .1113 .1112 .2222 .2233 .2223 .2213 .2212 .3333 .3323 .3313 .3312 .2323 .2313 .2312 .1313 .1312 .1212'
[../]
[./Fa]
type = DerivativeParsedMaterial
block = 0
property_name = Fa
expression = c^2
coupled_variables = c
[../]
[./Fb]
type = DerivativeParsedMaterial
block = 0
property_name = Fb
expression = (1-c)^3
coupled_variables = c
[../]
[./C]
type = CompositeElasticityTensor
block = 0
args = c
tensors = 'Ca Cb'
weights = 'Fa Fb'
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Outputs]
exodus = true
[]
(modules/solid_mechanics/test/tests/elasticitytensor/rotation_matrix_1_rotation.i)
# This input file is designed to rotate an elasticity tensor both with euler angles
# and a rotation matrix. The rotated tensor components should match between the
# two methods.
[Mesh]
type = GeneratedMesh
dim = 1
nx = 20
xmax = 1
[]
[AuxVariables]
[./C1111_aux_matrix] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_matrix] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_matrix] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_matrix] # C16
order = CONSTANT
family = MONOMIAL
[../]
[./C1111_aux_euler] # C11
order = CONSTANT
family = MONOMIAL
[../]
[./C1122_aux_euler] # C12
order = CONSTANT
family = MONOMIAL
[../]
[./C1133_aux_euler] # C13
order = CONSTANT
family = MONOMIAL
[../]
[./C1112_aux_euler] # C16
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./matl_C1111_matrix] # C11
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_matrix
execute_on = initial
[../]
[./matl_C1122_matrix] # C12
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_matrix
execute_on = initial
[../]
[./matl_C1133_matrix] # C13
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_matrix
execute_on = initial
[../]
[./matl_C1112_matrix] # C16
type = RankFourAux
rank_four_tensor = rotation_matrix_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_matrix
execute_on = initial
[../]
[./matl_C1111_euler] # C11
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 0
variable = C1111_aux_euler
execute_on = initial
[../]
[./matl_C1122_euler] # C12
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 1
index_l = 1
variable = C1122_aux_euler
execute_on = initial
[../]
[./matl_C1133_euler] # C13
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 2
index_l = 2
variable = C1133_aux_euler
execute_on = initial
[../]
[./matl_C1112_euler] # C16
type = RankFourAux
rank_four_tensor = euler_elasticity_tensor
index_i = 0
index_j = 0
index_k = 0
index_l = 1
variable = C1112_aux_euler
execute_on = initial
[../]
[]
[Materials]
[./elasticity_matrix]
type = ComputeElasticityTensor
block = 0
base_name = 'rotation_matrix'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
# rotation matrix for rotating a vector 30 degrees about the z-axis
rotation_matrix = '0.8660254 -0.5 0.
0.5 0.8660254 0
0 0 1'
[../]
[./elasticity_euler]
type = ComputeElasticityTensor
block = 0
base_name = 'euler'
fill_method = symmetric9
C_ijkl = '1111 1122 1133 2222 2233 3333 2323 1313 1212'
euler_angle_1 = -30. # same as above but opposite direction because _transpose_ gets built from these angles
euler_angle_2 = 0.
euler_angle_3 = 0.
[../]
[]
[Problem]
kernel_coverage_check = false
solve = false
[]
[Executioner]
type = Steady
[]
[Postprocessors]
# corresponding values in "matrix" and "euler" postprocessors should match
[./C11_matrix]
type = ElementAverageValue
variable = C1111_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_matrix]
type = ElementAverageValue
variable = C1122_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_matrix]
type = ElementAverageValue
variable = C1133_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_matrix]
type = ElementAverageValue
variable = C1112_aux_matrix
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C11_euler]
type = ElementAverageValue
variable = C1111_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C12_euler]
type = ElementAverageValue
variable = C1122_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C13_euler]
type = ElementAverageValue
variable = C1133_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[./C16_euler]
type = ElementAverageValue
variable = C1112_aux_euler
execute_on = 'INITIAL TIMESTEP_END'
[../]
[]
[Outputs]
exodus = true
[]