- propertyThe scalar material property name
C++ Type:MaterialPropertyName
Description:The scalar material property name
- variableThe name of the variable that this object applies to
C++ Type:AuxVariableName
Description:The name of the variable that this object applies to
MaterialRealVectorValueAux
under construction:Undocumented Class
The MaterialRealVectorValueAux has not been documented. The content listed below should be used as a starting point for documenting the class, which includes the typical automatic documentation associated with a MooseObject; however, what is contained is ultimately determined by what is necessary to make the documentation clear for users.
# MaterialRealVectorValueAux
!syntax description /AuxKernels/MaterialRealVectorValueAux
## Overview
!! Replace these lines with information regarding the MaterialRealVectorValueAux object.
## Example Input File Syntax
!! Describe and include an example of how to use the MaterialRealVectorValueAux object.
!syntax parameters /AuxKernels/MaterialRealVectorValueAux
!syntax inputs /AuxKernels/MaterialRealVectorValueAux
!syntax children /AuxKernels/MaterialRealVectorValueAux
!syntax description /AuxKernels/MaterialRealVectorValueAux
Input Parameters
- blockThe list of block ids (SubdomainID) that this object will be applied
C++ Type:std::vector
Options:
Description:The list of block ids (SubdomainID) that this object will be applied
- boundaryThe list of boundary IDs from the mesh where this boundary condition applies
C++ Type:std::vector
Options:
Description:The list of boundary IDs from the mesh where this boundary condition applies
- component0The vector component to consider for this kernel
Default:0
C++ Type:unsigned int
Options:
Description:The vector component to consider for this kernel
- execute_onLINEAR TIMESTEP_ENDThe list of flag(s) indicating when this object should be executed, the available options include NONE, INITIAL, LINEAR, NONLINEAR, TIMESTEP_END, TIMESTEP_BEGIN, FINAL, CUSTOM, PRE_DISPLACE.
Default:LINEAR TIMESTEP_END
C++ Type:ExecFlagEnum
Options:NONE INITIAL LINEAR NONLINEAR TIMESTEP_END TIMESTEP_BEGIN FINAL CUSTOM PRE_DISPLACE
Description:The list of flag(s) indicating when this object should be executed, the available options include NONE, INITIAL, LINEAR, NONLINEAR, TIMESTEP_END, TIMESTEP_BEGIN, FINAL, CUSTOM, PRE_DISPLACE.
- factor1The factor by which to multiply your material property for visualization
Default:1
C++ Type:double
Options:
Description:The factor by which to multiply your material property for visualization
- offset0The offset to add to your material property for visualization
Default:0
C++ Type:double
Options:
Description:The offset to add to your material property for visualization
Optional Parameters
- control_tagsAdds user-defined labels for accessing object parameters via control logic.
C++ Type:std::vector
Options:
Description:Adds user-defined labels for accessing object parameters via control logic.
- enableTrueSet the enabled status of the MooseObject.
Default:True
C++ Type:bool
Options:
Description:Set the enabled status of the MooseObject.
- seed0The seed for the master random number generator
Default:0
C++ Type:unsigned int
Options:
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
Options:
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
Input Files
- modules/tensor_mechanics/test/tests/smeared_cracking/cracking_rotation.i
- modules/solid_mechanics/test/tests/cracking/cracking_plane_stress.i
- modules/solid_mechanics/test/tests/cracking/cracking_function.i
- modules/tensor_mechanics/test/tests/cp_user_object/save_euler.i
- modules/tensor_mechanics/test/tests/crystal_plasticity/crysp_save_euler.i
- test/tests/materials/types/test.i
- modules/tensor_mechanics/test/tests/smeared_cracking/cracking_function.i
- modules/solid_mechanics/test/tests/cracking/cracking_xyz.i
modules/tensor_mechanics/test/tests/smeared_cracking/cracking_rotation.i
# This test is to ensure that the smeared cracking model correctly handles finite
# rotation of cracked elements.
# This consists of a single element that is first subjected to tensile loading
# in the y-direction via a prescribed displacement. This loading is sufficiently
# high to crack the material in that direction, but not completely unload. The
# prescribed displacement is then reversed so that the element is returned to its
# original configuration.
# In the next phase of the analysis, this element is then rotated 90 degrees by
# prescribing the displacement of the bottom of the element. The prescribed
# displacement BC used to crack the element in the first phase is deactivated.
# Once the element is fully rotated, a new BC is activated on what was originally
# the top surface (but is now the surface on the right hand side) to pull in
# the x-direction.
# If everything is working correctly, the model should re-load on the original
# crack (which should be rotated along with the elemnent) up to the peak stress
# in the first phase of the analysis, and then continue the unloading process
# as the crack strains continue to increase. Throughout this analysis, there should
# only be a single crack, as manifested in the crack_flags variables.
[Mesh]
file = cracking_test.e
[]
[GlobalParams]
displacements = 'disp_x disp_y disp_z'
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx'
[../]
[]
[AuxVariables]
[./crack_flags1]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_flags2]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_flags3]
order = CONSTANT
family = MONOMIAL
[../]
[]
[AuxKernels]
[./crack_flags1]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_flags1
component = 0
[../]
[./crack_flags2]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_flags2
component = 1
[../]
[./crack_flags3]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_flags3
component = 2
[../]
[]
[BCs]
[./x_pin]
type = DirichletBC
variable = disp_x
boundary = '15 16'
value = 0.0
[../]
[./y_pin]
type = DirichletBC
variable = disp_y
boundary = '15 16'
value = 0.0
[../]
[./z_all]
type = DirichletBC
variable = disp_z
boundary = '11 12 13 14 15 16 17 18'
value = 0.0
[../]
[./x_lb]
type = FunctionDirichletBC
variable = disp_x
boundary = '11 12'
function = 'if(t<10,0,if(t>=100,1,1-cos((t-10)*pi/180)))'
[../]
[./y_lb]
type = FunctionDirichletBC
variable = disp_y
boundary = '11 12'
function = 'if(t<10,0,if(t>=100,1,sin((t-10)*pi/180)))'
[../]
[./x_lt]
type = FunctionDirichletBC
variable = disp_x
boundary = '13 14'
function = '2+(t-100)*0.01'
[../]
[./x_rt]
type = FunctionDirichletBC
variable = disp_x
boundary = '17 18'
function = '1+(t-100)*0.01'
[../]
[./top_pull]
type = FunctionDirichletBC
variable = disp_y
boundary = '13 14 17 18'
function = 'if(t<5,t*0.01,0.05-(t-5)*0.01)'
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 100.e9
poissons_ratio = 0.
[../]
[./cracking_stress]
type = ComputeSmearedCrackingStress
shear_retention_factor = 0.1
cracking_stress = 3.e9
softening_models = exponential_softening
[../]
[./exponential_softening]
type = ExponentialSoftening
[../]
[]
[Executioner]
type = Transient
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-5
nl_max_its = 100
nl_abs_tol = 1e-5
nl_rel_tol = 1e-12
start_time = 0
end_time = 110
dt = 1
[]
[Controls]
[./p1]
type = TimePeriod
start_time = 0.0
end_time = 10.0
disable_objects = 'BCs/x_lt BCs/x_rt'
enable_objects = 'BCs/top_pull'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p2]
type = TimePeriod
start_time = 10.0
end_time = 101.0
disable_objects = 'BCs/x_lt BCs/x_rt BCs/top_pull'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p3]
type = TimePeriod
start_time = 101.0
end_time = 110.0
enable_objects = 'BCs/x_lt BCs/x_rt'
disable_objects = 'BCs/top_pull'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[]
[Outputs]
exodus = true
[]
modules/solid_mechanics/test/tests/cracking/cracking_plane_stress.i
################################################################################
#
# 1x1x1 cube, single element
# simulate plane stress
# pull in +y direction on right surface to produce shear strain
#
#
#
# ____________
# /| /|
# / | 5 / | -X Left 1
# /__________ / | +X Right 4
# | | 3 | | +Y Top 5
# | 1 | | 4 | -Y Bottom 2
# | |_6_____|___| y +Z Front 6
# | / | / ^ -Z Back 3
# | / 2 | / |
# |/__________|/ |
# ----> x
# /
# /
# z
#
#
#
#################################################################################
[Mesh]
file = cube.e
displacements = 'disp_x disp_y disp_z'
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[./disp_z]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_xx_flags]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0.0026 0 -0.0026 0'
[../]
[./pressure]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0 0 0 0'
[../]
[]
[SolidMechanics]
[./solid]
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
[../]
[]
[AuxKernels]
[./crack_xx_flags]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_xx_flags
component = 0
block = 1
[../]
[./stress_xx]
type = MaterialTensorAux
variable = stress_xx
tensor = stress
index = 0
[../]
[./stress_yy]
type = MaterialTensorAux
variable = stress_yy
tensor = stress
index = 1
[../]
[./stress_zz]
type = MaterialTensorAux
variable = stress_zz
tensor = stress
index = 2
[../]
[./stress_xy]
type = MaterialTensorAux
variable = stress_xy
tensor = stress
index = 3
[../]
[./stress_yz]
type = MaterialTensorAux
variable = stress_yz
tensor = stress
index = 4
[../]
[./stress_zx]
type = MaterialTensorAux
variable = stress_zx
tensor = stress
index = 5
[../]
[./strain_xx]
type = MaterialTensorAux
variable = strain_xx
tensor = total_strain
index = 0
[../]
[./strain_yy]
type = MaterialTensorAux
variable = strain_yy
tensor = total_strain
index = 1
[../]
[./strain_zz]
type = MaterialTensorAux
variable = strain_zz
tensor = total_strain
index = 2
[../]
[./strain_xy]
type = MaterialTensorAux
variable = strain_xy
tensor = total_strain
index = 3
[../]
[./strain_yz]
type = MaterialTensorAux
variable = strain_yz
tensor = total_strain
index = 4
[../]
[./strain_zx]
type = MaterialTensorAux
variable = strain_zx
tensor = total_strain
index = 5
[../]
[]
[BCs]
[./pull_y]
type = FunctionDirichletBC
variable = disp_y
boundary = 4
function = displ
[../]
[./pin_x]
type = DirichletBC
variable = disp_x
boundary = '1 4'
value = 0.0
[../]
[./pin_y]
type = DirichletBC
variable = disp_y
boundary = 1
value = 0.0
[../]
[./back]
type = DirichletBC
variable = disp_z
boundary = '3'
value = 0.0
[../]
[./front]
type = Pressure
variable = disp_z
component = 2
boundary = 6
function = pressure
factor = 1.0
[../]
[]
[Materials]
[./fred]
type = Elastic
block = 1
youngs_modulus = 200.0e3
poissons_ratio = 0.3
cracking_stress = 120
cracking_release = exponential
cracking_residual_stress = 0.1
cracking_beta = 0.1
compute_method = ShearRetention
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
[../]
[]
[Postprocessors]
[./elem_stress_xx]
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[../]
[./elem_strain_xx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./elem_stress_yy]
type = ElementalVariableValue
variable = stress_yy
elementid = 0
[../]
[./elem_strain_yy]
type = ElementalVariableValue
variable = strain_yy
elementid = 0
[../]
[./elem_stress_zz]
type = ElementalVariableValue
variable = stress_zz
elementid = 0
[../]
[./elem_strain_zz]
type = ElementalVariableValue
variable = strain_zz
elementid = 0
[../]
[./elem_stress_xy]
type = ElementalVariableValue
variable = stress_xy
elementid = 0
[../]
[./elem_strain_xy]
type = ElementalVariableValue
variable = strain_xy
elementid = 0
[../]
[./elem_stress_yz]
type = ElementalVariableValue
variable = stress_yz
elementid = 0
[../]
[./elem_strain_yz]
type = ElementalVariableValue
variable = strain_yz
elementid = 0
[../]
[./elem_stress_zx]
type = ElementalVariableValue
variable = stress_yz
elementid = 0
[../]
[./elem_strain_zx]
type = ElementalVariableValue
variable = strain_yz
elementid = 0
[../]
[./elem_crack_flags]
type = ElementalVariableValue
variable = crack_xx_flags
elementid = 0
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type -sub_pc_type'
petsc_options_value = '101 asm lu'
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-8
l_tol = 1e-5
start_time = 0.0
end_time = 0.4
dt = 0.04
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
[./console]
type = Console
output_linear = true
[../]
csv = true
[]
modules/solid_mechanics/test/tests/cracking/cracking_function.i
#
# Simple pull test for cracking.
#
#
[Mesh]
file = plate.e
displacements = 'disp_x disp_y'
# This test uses ElementalVariableValue postprocessors on specific
# elements, so element numbering needs to stay unchanged
allow_renumbering = false
[]
[Variables]
[./disp_x]
order = FIRST
family = LAGRANGE
[../]
[./disp_y]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yz]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zx]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_xx_flags]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_yy_flags]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0.001 0 -0.001 0'
[../]
[./pressure]
type = PiecewiseLinear
x = '0 0.4'
y = '1.0e5 1.0e5'
[../]
[./fstress]
type = ParsedFunction
value = 'if(x > 0.667, 1.1e6, 0) + if(x<=0.667, 1.2e6, 0)'
[../]
[]
[SolidMechanics]
[./solid]
disp_x = disp_x
disp_y = disp_y
[../]
[]
[AuxKernels]
[./crack_xx_flags]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_xx_flags
component = 0
block = 1
[../]
[./crack_yy_flags]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_yy_flags
component = 1
block = 1
[../]
[./stress_xx]
type = MaterialTensorAux
variable = stress_xx
tensor = stress
index = 0
[../]
[./stress_yy]
type = MaterialTensorAux
variable = stress_yy
tensor = stress
index = 1
[../]
[./stress_zz]
type = MaterialTensorAux
variable = stress_zz
tensor = stress
index = 2
[../]
[./stress_xy]
type = MaterialTensorAux
variable = stress_xy
tensor = stress
index = 3
[../]
[./stress_yz]
type = MaterialTensorAux
variable = stress_yz
tensor = stress
index = 4
[../]
[./stress_zx]
type = MaterialTensorAux
variable = stress_zx
tensor = stress
index = 5
[../]
[./strain_xx]
type = MaterialTensorAux
variable = strain_xx
tensor = total_strain
index = 0
[../]
[./strain_yy]
type = MaterialTensorAux
variable = strain_yy
tensor = total_strain
index = 1
[../]
[./strain_zz]
type = MaterialTensorAux
variable = strain_zz
tensor = total_strain
index = 2
[../]
[./strain_xy]
type = MaterialTensorAux
variable = strain_xy
tensor = total_strain
index = 3
[../]
[./strain_yz]
type = MaterialTensorAux
variable = strain_yz
tensor = total_strain
index = 4
[../]
[./strain_zx]
type = MaterialTensorAux
variable = strain_zx
tensor = total_strain
index = 5
[../]
[]
[BCs]
[./pull]
type = FunctionDirichletBC
variable = disp_x
boundary = '3 4'
function = displ
[../]
[./pin_x]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0
[../]
[./pin_y]
type = DirichletBC
variable = disp_y
boundary = '1 4'
value = 0.0
[../]
[]
[Materials]
[./SolidModel]
type = Elastic
block = 1
youngs_modulus = 200.0e7
poissons_ratio = 0.0 #.3
cracking_stress_function = fstress
cracking_stress = 1.2e6
cracking_residual_stress = 0.0
disp_x = disp_x
disp_y = disp_y
[../]
[]
[Postprocessors]
[./elem_stress_xx]
type = ElementalVariableValue
variable = stress_xx
elementid = 0
[../]
[./elem_strain_xx]
type = ElementalVariableValue
variable = strain_xx
elementid = 0
[../]
[./elem_crack_flags_x]
type = ElementalVariableValue
variable = crack_xx_flags
elementid = 0
[../]
[./elem_crack_flags_y]
type = ElementalVariableValue
variable = crack_yy_flags
elementid = 0
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101 '
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 0.2
dt = 0.0025
[]
[Outputs]
[./out]
type = Exodus
elemental_as_nodal = true
[../]
csv = true
[]
modules/tensor_mechanics/test/tests/cp_user_object/save_euler.i
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
displacements = 'disp_x disp_y'
nx = 2
ny = 2
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[]
[GlobalParams]
volumetric_locking_correction = true
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./e_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./fp_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./gss]
order = CONSTANT
family = MONOMIAL
[../]
[./euler1]
order = CONSTANT
family = MONOMIAL
[../]
[./euler2]
order = CONSTANT
family = MONOMIAL
[../]
[./euler3]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./tdisp]
type = ParsedFunction
value = 0.01*t
[../]
[]
[UserObjects]
[./prop_read]
type = ElementPropertyReadFile
prop_file_name = 'euler_ang_file.txt'
# Enter file data as prop#1, prop#2, .., prop#nprop
nprop = 3
read_type = element
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
variable = stress_yy
rank_two_tensor = stress
index_j = 1
index_i = 1
execute_on = timestep_end
[../]
[./e_yy]
type = RankTwoAux
variable = e_yy
rank_two_tensor = lage
index_j = 1
index_i = 1
execute_on = timestep_end
[../]
[./fp_yy]
type = RankTwoAux
variable = fp_yy
rank_two_tensor = fp
index_j = 1
index_i = 1
execute_on = timestep_end
[../]
[./gss]
type = MaterialStdVectorAux
variable = gss
property = state_var_gss
index = 0
execute_on = timestep_end
[../]
[./euler1]
type = MaterialRealVectorValueAux
variable = euler1
property = Euler_angles
component = 0
execute_on = timestep_end
[../]
[./euler2]
type = MaterialRealVectorValueAux
variable = euler2
property = Euler_angles
component = 1
execute_on = timestep_end
[../]
[./euler3]
type = MaterialRealVectorValueAux
variable = euler3
property = Euler_angles
component = 2
execute_on = timestep_end
[../]
[]
[BCs]
[./fix_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[./fix_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./tdisp]
type = FunctionDirichletBC
variable = disp_y
boundary = top
function = tdisp
[../]
[]
[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'
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
[../]
[]
[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'
[../]
[./strain]
type = ComputeFiniteStrain
displacements = 'disp_x disp_y'
[../]
[./elasticity_tensor]
type = ComputeElasticityTensorCP
C_ijkl = '1.684e5 1.214e5 1.214e5 1.684e5 1.214e5 1.684e5 0.754e5 0.754e5 0.754e5'
fill_method = symmetric9
read_prop_user_object = prop_read
[../]
[]
[Postprocessors]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
[../]
[./e_yy]
type = ElementAverageValue
variable = e_yy
[../]
[./fp_yy]
type = ElementAverageValue
variable = fp_yy
[../]
[./gss]
type = ElementAverageValue
variable = gss
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
dt = 0.01
solve_type = 'PJFNK'
petsc_options_iname = -pc_hypre_type
petsc_options_value = boomerang
nl_abs_tol = 1e-10
nl_rel_step_tol = 1e-10
dtmax = 10.0
nl_rel_tol = 1e-10
end_time = 1
dtmin = 0.01
num_steps = 10
nl_abs_step_tol = 1e-10
[]
[Outputs]
exodus = true
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y'
use_displaced_mesh = true
[../]
[]
modules/tensor_mechanics/test/tests/crystal_plasticity/crysp_save_euler.i
[Mesh]
type = GeneratedMesh
dim = 2
elem_type = QUAD4
displacements = 'disp_x disp_y'
nx = 2
ny = 2
[]
[Variables]
[./disp_x]
block = 0
[../]
[./disp_y]
block = 0
[../]
[]
[GlobalParams]
volumetric_locking_correction = true
[]
[AuxVariables]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./e_yy]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./fp_yy]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./rotout]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./gss1]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./euler1]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./euler2]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[./euler3]
order = CONSTANT
family = MONOMIAL
block = 0
[../]
[]
[Functions]
[./tdisp]
type = ParsedFunction
value = 0.01*t
[../]
[]
[UserObjects]
[./prop_read]
type = ElementPropertyReadFile
prop_file_name = 'euler_ang_file.txt'
# Enter file data as prop#1, prop#2, .., prop#nprop
nprop = 3
read_type = element
[../]
[]
[AuxKernels]
[./stress_yy]
type = RankTwoAux
variable = stress_yy
rank_two_tensor = stress
index_j = 1
index_i = 1
execute_on = timestep_end
block = 0
[../]
[./e_yy]
type = RankTwoAux
variable = e_yy
rank_two_tensor = lage
index_j = 1
index_i = 1
execute_on = timestep_end
block = 0
[../]
[./fp_yy]
type = RankTwoAux
variable = fp_yy
rank_two_tensor = fp
index_j = 1
index_i = 1
execute_on = timestep_end
block = 0
[../]
[./gss1]
type = MaterialStdVectorAux
variable = gss1
property = gss
index = 0
execute_on = timestep_end
block = 0
[../]
[./euler1]
type = MaterialRealVectorValueAux
variable = euler1
property = Euler_angles
component = 0
execute_on = timestep_end
block = 0
[../]
[./euler2]
type = MaterialRealVectorValueAux
variable = euler2
property = Euler_angles
component = 1
execute_on = timestep_end
block = 0
[../]
[./euler3]
type = MaterialRealVectorValueAux
variable = euler3
property = Euler_angles
component = 2
execute_on = timestep_end
block = 0
[../]
[]
[BCs]
[./fix_x]
type = DirichletBC
variable = disp_x
boundary = 'left'
value = 0
[../]
[./fix_y]
type = DirichletBC
variable = disp_y
boundary = 'bottom'
value = 0
[../]
[./tdisp]
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 60.8 5 8 60.8 9 12 60.8'
tan_mod_type = exact
[../]
[./strain]
type = ComputeFiniteStrain
block = 0
displacements = 'disp_x disp_y'
[../]
[./elasticity_tensor]
type = ComputeElasticityTensorCP
block = 0
C_ijkl = '1.684e5 1.214e5 1.214e5 1.684e5 1.214e5 1.684e5 0.754e5 0.754e5 0.754e5'
fill_method = symmetric9
read_prop_user_object = prop_read
[../]
[]
[Postprocessors]
[./stress_yy]
type = ElementAverageValue
variable = stress_yy
block = 'ANY_BLOCK_ID 0'
[../]
[./e_yy]
type = ElementAverageValue
variable = e_yy
block = 'ANY_BLOCK_ID 0'
[../]
[./fp_yy]
type = ElementAverageValue
variable = fp_yy
block = 'ANY_BLOCK_ID 0'
[../]
[./gss1]
type = ElementAverageValue
variable = gss1
block = 'ANY_BLOCK_ID 0'
[../]
[]
[Preconditioning]
[./smp]
type = SMP
full = true
[../]
[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-pc_type'
petsc_options_value = 'lu'
nl_rel_tol = 1e-10
nl_abs_tol = 1e-10
dt = 0.01
dtmax = 10.0
dtmin = 0.01
num_steps = 10
[]
[Outputs]
file_base = crysp_save_euler_out
exodus = true
[]
[Kernels]
[./TensorMechanics]
displacements = 'disp_x disp_y'
use_displaced_mesh = true
[../]
[]
test/tests/materials/types/test.i
[Mesh]
type = GeneratedMesh
dim = 2
xmin = 0
xmax = 1
ymin = 0
ymax = 1
nx = 2
ny = 2
[]
[Variables]
[./u]
order = FIRST
family = LAGRANGE
[../]
[]
[AuxVariables]
[./real]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec0]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec1]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec0_qp0]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvec0_qp1]
order = CONSTANT
family = MONOMIAL
[../]
[./realvec0]
order = CONSTANT
family = MONOMIAL
[../]
[./realvec1]
order = CONSTANT
family = MONOMIAL
[../]
[./realvec2]
order = CONSTANT
family = MONOMIAL
[../]
[./densemat00]
order = CONSTANT
family = MONOMIAL
[../]
[./densemat01]
order = CONSTANT
family = MONOMIAL
[../]
[./tensor00]
order = CONSTANT
family = MONOMIAL
[../]
[./tensor11]
order = CONSTANT
family = MONOMIAL
[../]
[./tensor22]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad00]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad01]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad02]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad10]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad11]
order = CONSTANT
family = MONOMIAL
[../]
[./stdvecgrad12]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Kernels]
[./diff]
type = Diffusion
variable = u
[../]
[]
[AuxKernels]
[./real0]
type = MaterialRealAux
variable = real
property = real_prop
execute_on = timestep_end
[../]
[./stdvec0]
type = MaterialStdVectorAux
variable = stdvec0
property = stdvec_prop
index = 0
execute_on = timestep_end
[../]
[./stdvec1]
type = MaterialStdVectorAux
variable = stdvec1
property = stdvec_prop
index = 1
execute_on = timestep_end
[../]
[./stdvec0_qp0]
type = MaterialStdVectorAux
variable = stdvec0_qp0
property = stdvec_prop_qp
index = 0
selected_qp = 0
execute_on = timestep_end
[../]
[./stdvec0_qp1]
type = MaterialStdVectorAux
variable = stdvec0_qp1
property = stdvec_prop_qp
index = 0
selected_qp = 1
execute_on = timestep_end
[../]
[./densemat00]
type = MaterialRealDenseMatrixAux
variable = densemat00
property = matrix_prop
row = 0
column = 0
execute_on = timestep_end
[../]
[./densemat01]
type = MaterialRealDenseMatrixAux
variable = densemat01
property = matrix_prop
row = 0
column = 1
execute_on = timestep_end
[../]
[./realvec0]
type = MaterialRealVectorValueAux
variable = realvec0
property = realvec_prop
component = 0
execute_on = timestep_end
[../]
[./realvec1]
type = MaterialRealVectorValueAux
variable = realvec1
property = realvec_prop
component = 1
execute_on = timestep_end
[../]
[./realvec2]
type = MaterialRealVectorValueAux
variable = realvec2
property = realvec_prop
component = 2
execute_on = timestep_end
[../]
[./realtensor00]
type = MaterialRealTensorValueAux
variable = tensor00
property = tensor_prop
row = 0
column = 0
execute_on = timestep_end
[../]
[./realtensor11]
type = MaterialRealTensorValueAux
variable = tensor11
property = tensor_prop
row = 1
column = 1
execute_on = timestep_end
[../]
[./realtensor22]
type = MaterialRealTensorValueAux
variable = tensor22
property = tensor_prop
row = 2
column = 2
execute_on = timestep_end
[../]
[./stdvecgrad00]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad00
property = stdvec_grad_prop
[../]
[./stdvecgrad01]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad01
property = stdvec_grad_prop
component = 1
[../]
[./stdvecgrad02]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad02
property = stdvec_grad_prop
component = 2
[../]
[./stdvecgrad10]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad10
index = 1
property = stdvec_grad_prop
[../]
[./stdvecgrad11]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad11
index = 1
component = 1
property = stdvec_grad_prop
[../]
[./stdvecgrad12]
type = MaterialStdVectorRealGradientAux
variable = stdvecgrad12
index = 1
component = 2
property = stdvec_grad_prop
[../]
[]
[BCs]
[./left]
type = DirichletBC
variable = u
boundary = 3
value = 0
[../]
[./right]
type = DirichletBC
variable = u
boundary = 1
value = 1
[../]
[]
[Materials]
[./mat]
type = TypesMaterial
block = 0
[../]
[]
[Executioner]
type = Steady
solve_type = PJFNK
[]
[Outputs]
file_base = test_out
exodus = true
[]
modules/tensor_mechanics/test/tests/smeared_cracking/cracking_function.i
#
# Simple pull test for cracking. This tests the option to prescribe the
# cracking strength using an AuxVariable. In this case, an elemental
# AuxVariable is used, and a function is used to prescribe its value.
# One of the elements is weaker than the others, so the crack localizes
# in that element.
#
[Mesh]
file = plate.e
[]
[GlobalParams]
displacements = 'disp_x disp_y'
[]
[AuxVariables]
[./cracking_stress_fn]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_flags2]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./displ]
type = PiecewiseLinear
x = '0 0.1 0.2 0.3 0.4'
y = '0 0.001 0 -0.001 0'
[../]
[./fstress]
type = ParsedFunction
value = 'if(x > 0.667, 1.1e6, 1.2e6)'
[../]
[]
[Modules/TensorMechanics/Master]
[./all]
strain = FINITE
add_variables = true
generate_output = 'stress_xx stress_yy stress_zz stress_xy stress_yz stress_zx strain_xx strain_yy strain_xy strain_yz'
[../]
[]
[AuxKernels]
[./cracking_stress_fn]
type = FunctionAux
variable = cracking_stress_fn
function = fstress
execute_on = initial
[../]
[./crack_flags2]
type = MaterialRealVectorValueAux
property = crack_flags
variable = crack_flags2
component = 2
[../]
[]
[BCs]
[./pull]
type = FunctionDirichletBC
variable = disp_x
boundary = '3 4'
function = displ
[../]
[./pin_x]
type = DirichletBC
variable = disp_x
boundary = '1 2'
value = 0
[../]
[./pin_y]
type = DirichletBC
variable = disp_y
boundary = '1 4'
value = 0.0
[../]
[]
[Materials]
[./elasticity_tensor]
type = ComputeIsotropicElasticityTensor
youngs_modulus = 200.0e7
poissons_ratio = 0.0
[../]
[./elastic_stress]
type = ComputeSmearedCrackingStress
cracking_stress = cracking_stress_fn
softening_models = abrupt_softening
[../]
[./abrupt_softening]
type = AbruptSoftening
residual_stress = 0.0
[../]
[]
[Postprocessors]
[./elem_stress_xx]
type = ElementalVariableValue
variable = stress_xx
elementid = 2
[../]
[./elem_strain_xx]
type = ElementalVariableValue
variable = strain_xx
elementid = 2
[../]
[./elem_crack_flags_x]
type = ElementalVariableValue
variable = crack_flags2
elementid = 2
[../]
[]
[Executioner]
type = Transient
solve_type = PJFNK
petsc_options_iname = '-ksp_gmres_restart'
petsc_options_value = '101 '
line_search = 'none'
l_max_its = 100
nl_max_its = 100
nl_rel_tol = 1e-8
nl_abs_tol = 1e-6
l_tol = 1e-5
start_time = 0.0
end_time = 0.2
dt = 0.0025
[]
[Outputs]
exodus = true
csv = true
[]
modules/solid_mechanics/test/tests/cracking/cracking_xyz.i
#
# Test to exercise the exponential stress release
#
# First x, then y, then z directions crack
#
[GlobalParams]
order = FIRST
family = LAGRANGE
[]
[Mesh]
file = cracking_test.e
displacements = 'disp_x disp_y disp_z'
[]
[Variables]
[./disp_x]
[../]
[./disp_y]
[../]
[./disp_z]
[../]
[]
[AuxVariables]
[./crack_1]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_2]
order = CONSTANT
family = MONOMIAL
[../]
[./crack_3]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./strain_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xx]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_xy]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_yz]
order = CONSTANT
family = MONOMIAL
[../]
[./stress_zx]
order = CONSTANT
family = MONOMIAL
[../]
[]
[Functions]
[./displx]
type = PiecewiseLinear
# x = '0 1'
# y = '0 .0035'
x = '0 1'
y = '0 0.00175'
[../]
[./velocity_y]
type = ParsedFunction
value = 'if(t < 2, 0.00175, 0)'
[../]
[./velocity_z]
type = ParsedFunction
value = 0.00175
[../]
[]
[SolidMechanics]
[./solid]
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
[../]
[]
[AuxKernels]
[./crack_1]
type = MaterialRealVectorValueAux
variable = crack_1
property = crack_flags
component = 0
[../]
[./crack_2]
type = MaterialRealVectorValueAux
variable = crack_2
property = crack_flags
component = 1
[../]
[./crack_3]
type = MaterialRealVectorValueAux
variable = crack_3
property = crack_flags
component = 2
[../]
[./strain_xx]
type = MaterialTensorAux
variable = strain_xx
tensor = total_strain
index = 0
[../]
[./strain_yy]
type = MaterialTensorAux
variable = strain_yy
tensor = total_strain
index = 1
[../]
[./strain_zz]
type = MaterialTensorAux
variable = strain_zz
tensor = total_strain
index = 2
[../]
[./stress_xx]
type = MaterialTensorAux
variable = stress_xx
tensor = stress
index = 0
[../]
[./stress_yy]
type = MaterialTensorAux
variable = stress_yy
tensor = stress
index = 1
[../]
[./stress_zz]
type = MaterialTensorAux
variable = stress_zz
tensor = stress
index = 2
[../]
[./stress_xy]
type = MaterialTensorAux
variable = stress_xy
tensor = stress
index = 3
[../]
[./stress_yz]
type = MaterialTensorAux
variable = stress_yz
tensor = stress
index = 4
[../]
[./stress_zx]
type = MaterialTensorAux
variable = stress_zx
tensor = stress
index = 5
[../]
[]
[BCs]
[./fix_x]
type = DirichletBC
variable = disp_x
boundary = 1
value = 0.0
[../]
[./move_x]
type = FunctionDirichletBC
variable = disp_x
boundary = 4
function = displx
[../]
[./fix_y]
type = DirichletBC
variable = disp_y
boundary = 2
value = 0.0
[../]
[./move_y]
type = PresetVelocity
variable = disp_y
boundary = 5
function = velocity_y
# time_periods = 'p2 p3'
[../]
[./fix_z]
type = DirichletBC
variable = disp_z
boundary = 3
value = 0.0
[../]
[./move_z]
type = PresetVelocity
variable = disp_z
boundary = 6
function = velocity_z
# time_periods = 'p3'
[../]
[]
[Materials]
[./fred]
type = Elastic
block = 1
youngs_modulus = 186.5e9
poissons_ratio = .316
cracking_stress = 119.3e6
cracking_release = exponential
disp_x = disp_x
disp_y = disp_y
disp_z = disp_z
formulation = linear
[../]
[]
#[Preconditioning]
# [./SMP]
# type = SMP
# full = true
# []
#[]
[Executioner]
type = Transient
#Preconditioned JFNK (default)
solve_type = 'PJFNK'
petsc_options_iname = '-ksp_gmres_restart -pc_type'
petsc_options_value = '101 lu'
line_search = 'none'
l_max_its = 100
l_tol = 1e-6
nl_max_its = 100
nl_abs_tol = 4e-8
#nl_rel_tol = 1e-3
nl_rel_tol = 1e-6
start_time = 0.0
end_time = 3.0
# dt = 0.005
dt = 0.01
[]
[Controls]
[./p1]
type = TimePeriod
start_time = 0.0
end_time = 1.0
disable_objects = 'BCs/move_y BCs/move_z'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p2]
type = TimePeriod
start_time = 1.0
end_time = 2.0
disable_objects = 'BCs/move_z'
enable_objects = 'BCs/move_y'
reverse_on_false = false
execute_on = 'initial timestep_begin'
[../]
[./p3]
type = TimePeriod
start_time = 2.0
end_time = 3.0
enable_objects = 'BCs/move_y BCs/move_z'
reverse_on_false = false
execute_on = 'initial timestep_begin'
set_sync_times = true
[../]
[]
[Outputs]
exodus = true
[]