DirichletBC

(test/tests/bcs/matched_value_bc/matched_value_bc_test.i)

[Mesh]
  [./square]
    type = GeneratedMeshGenerator
    nx = 2
    ny = 2
    dim = 2
  [../]
[]

# Solves a pair of coupled diffusion equations where u=v on the boundary

[Variables]
  active = 'u v'

  [./u]
    order = FIRST
    family = LAGRANGE
    initial_condition = 3
  [../]

  [./v]
    order = FIRST
    family = LAGRANGE
    initial_condition = 2
  [../]
[]

[Kernels]
  active = 'diff_u diff_v'

  [./diff_u]
    type = Diffusion
    variable = u
  [../]

  [./diff_v]
    type = Diffusion
    variable = v
  [../]
[]

[BCs]
  active = 'right_v left_u'

  [./right_v]
    type = DirichletBC
    variable = v
    boundary = 1
    value = 3
  [../]

  [./left_u]
    type = MatchedValueBC
    variable = u
    boundary = 3
    v = v
  [../]
[]

[Preconditioning]
  [./precond]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'

  nl_rel_tol = 1e-10
  l_tol = 1e-12
[]

[Outputs]
  file_base = out
  exodus = true
[]

(test/tests/bcs/misc_bcs/convective_flux_bc.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
  nz = 0
  zmin = 0
  zmax = 0
  elem_type = QUAD4
[]

[Variables]
  active = 'u'

  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  active = 'diff'

  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  active = 'left right'

  [./left]
    type = DirichletBC
    variable = u
    boundary = 3
    value = 0.0
  [../]

  [./right]
    type = ConvectiveFluxBC
    variable = u
    boundary = 1
    rate = 100
    initial = 10
    final = 20
    duration = 10
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'

  start_time = 0.0
  num_steps = 10
  dt = 1.0
[]

[Outputs]
  exodus = true
[]

(test/tests/multiapps/picard_multilevel/fullsolve_multilevel/sub_level2.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  xmin = 0
  xmax = 1
  ymin = 0
  ymax = 1
  nx = 10
  ny = 10
[]

[Variables]
  [w]
  []
[]

[AuxVariables]
  [v]
  []
[]

[Kernels]
  [time_derivative]
    type = TimeDerivative
    variable = w
  []
  [diffusion]
    type = Diffusion
    variable = w
  []
  [source]
    type = CoupledForce
    variable = w
    v = v
  []
[]

[BCs]
  [dirichlet]
    type = DirichletBC
    variable = w
    boundary = '0'
    value = 0
  []
[]

[Postprocessors]
  [avg_v]
    type = ElementAverageValue
    variable = v
    execute_on = 'initial linear'
  []
  [avg_w]
    type = ElementAverageValue
    variable = w
    execute_on = 'initial linear'
  []
[]

[Executioner]
  type = Transient

  petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart '
  petsc_options_value = 'hypre boomeramg 100'

  end_time = 0.1
  dt = 0.02
  # steady_state_detection = true
[]


[Outputs]
  exodus = true
  csv = true
  # print_linear_residuals = false
[]

(test/tests/mesh/splitting/grid_from_generated.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
  [Partitioner]
    type = GridPartitioner
    nx = 2
    ny = 2
    nz = 1
  []
[]

[Variables]
  [u]
  []
[]

[Kernels]
  [diff]
    type = Diffusion
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = 'left'
    value = 0
  []
  [right]
    type = DirichletBC
    variable = u
    boundary = 'right'
    value = 1
  []
[]

[Executioner]
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

[AuxVariables]
  [pid]
    family = MONOMIAL
    order = CONSTANT
  []
[]

[AuxKernels]
  [pid_aux]
    type = ProcessorIDAux
    variable = pid
    execute_on = 'INITIAL'
  []
[]

(test/tests/restart/start_time_override/start_time_override.i)

[Mesh]
  type = GeneratedMesh
  nx = 5
  ny = 5
  dim = 2
[]

[Problem]
  restart_file_base = transient_out_cp/LATEST
  skip_additional_restart_data = true
[]

[Variables]
  [u]
    order = FIRST
    family = LAGRANGE
  []
[]

[Kernels]
  [bodyforce]
    type = BodyForce
    variable = u
    value = 10.0
  []

  [ie]
    type = TimeDerivative
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 0
  []

  [right]
    type = DirichletBC
    variable = u
    boundary = 2
    value = 10
  []
[]

[Postprocessors]
  [u_norm]
    type = ElementL2Norm
    variable = u
  []
[]

[Executioner]
  type = Transient

  # Start time can be set explicitly here or be picked up from the restart file
  num_steps = 5
  dt = 0.1
[]

[Outputs]
  csv = true
[]

(modules/combined/test/tests/phase_field_fracture/crack2d_aniso_hist_false.i)

#This input uses PhaseField-Nonconserved Action to add phase field fracture bulk rate kernels
[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 40
    ny = 20
    ymax = 0.5
  []
  [./noncrack]
    type = BoundingBoxNodeSetGenerator
    new_boundary = noncrack
    bottom_left = '0.5 0 0'
    top_right = '1 0 0'
    input = gen
  [../]
[]

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Modules]
  [./TensorMechanics]
    [./Master]
      [./All]
        add_variables = true
        strain = SMALL
        additional_generate_output = 'strain_yy stress_yy'
        planar_formulation = PLANE_STRAIN
      [../]
    [../]
  [../]
  [./PhaseField]
    [./Nonconserved]
      [./c]
        free_energy = F
        kappa = kappa_op
        mobility = L
      [../]
    [../]
  [../]
[]

[Kernels]
  [./solid_x]
    type = PhaseFieldFractureMechanicsOffDiag
    variable = disp_x
    component = 0
    c = c
  [../]
  [./solid_y]
    type = PhaseFieldFractureMechanicsOffDiag
    variable = disp_y
    component = 1
    c = c
  [../]
[]

[BCs]
  [./ydisp]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = top
    function = 't'
  [../]
  [./yfix]
    type = DirichletBC
    variable = disp_y
    boundary = noncrack
    value = 0
  [../]
  [./xfix]
    type = DirichletBC
    variable = disp_x
    boundary = right
    value = 0
  [../]
[]

[Materials]
  [./pfbulkmat]
    type = GenericConstantMaterial
    prop_names = 'gc_prop l visco'
    prop_values = '1e-3 0.05 1e-6'
  [../]
  [./elasticity_tensor]
    type = ComputeElasticityTensor
    C_ijkl = '127.0 70.8 70.8 127.0 70.8 127.0 73.55 73.55 73.55'
    fill_method = symmetric9
    euler_angle_1 = 30
    euler_angle_2 = 0
    euler_angle_3 = 0
  [../]
  [./define_mobility]
    type = ParsedMaterial
    material_property_names = 'gc_prop visco'
    f_name = L
    function = '1.0/(gc_prop * visco)'
  [../]
  [./define_kappa]
    type = ParsedMaterial
    material_property_names = 'gc_prop l'
    f_name = kappa_op
    function = 'gc_prop * l'
  [../]
  [./damage_stress]
    type = ComputeLinearElasticPFFractureStress
    c = c
    E_name = 'elastic_energy'
    D_name = 'degradation'
    F_name = 'local_fracture_energy'
    decomposition_type = stress_spectral
  [../]
  [./degradation]
    type = DerivativeParsedMaterial
    f_name = degradation
    args = 'c'
    function = '(1.0-c)^2*(1.0 - eta) + eta'
    constant_names       = 'eta'
    constant_expressions = '1.0e-6'
    derivative_order = 2
  [../]
  [./local_fracture_energy]
    type = DerivativeParsedMaterial
    f_name = local_fracture_energy
    args = 'c'
    material_property_names = 'gc_prop l'
    function = 'c^2 * gc_prop / 2 / l'
    derivative_order = 2
  [../]
  [./fracture_driving_energy]
    type = DerivativeSumMaterial
    args = c
    sum_materials = 'elastic_energy local_fracture_energy'
    derivative_order = 2
    f_name = F
  [../]
[]

[Postprocessors]
  [./av_stress_yy]
    type = ElementAverageValue
    variable = stress_yy
  [../]
  [./av_strain_yy]
    type = SideAverageValue
    variable = disp_y
    boundary = top
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient

  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_factor_mat_solving_package'
  petsc_options_value = 'lu superlu_dist'

  nl_rel_tol = 1e-8
  l_tol = 1e-4
  l_max_its = 100
  nl_max_its = 10

  dt = 2e-6
  num_steps = 5
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/lid_driven.i)

[GlobalParams]
  gravity = '0 0 0'
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 1.0
    ymin = 0
    ymax = 1.0
    nx = 16
    ny = 16
    elem_type = QUAD9
  []
  [./corner_node]
    type = ExtraNodesetGenerator
    new_boundary = 'pinned_node'
    nodes = '0'
    input = gen
  [../]
[]

[Variables]
  [./vel_x]
    order = SECOND
    family = LAGRANGE
  [../]

  [./vel_y]
    order = SECOND
    family = LAGRANGE
  [../]

  [./T]
    order = SECOND
    family = LAGRANGE

    [./InitialCondition]
      type = ConstantIC
      value = 1.0
    [../]
  [../]

  [./p]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  # mass
  [./mass]
    type = INSMass
    variable = p
    u = vel_x
    v = vel_y
    pressure = p
  [../]

  # x-momentum, time
  [./x_momentum_time]
    type = INSMomentumTimeDerivative
    variable = vel_x
  [../]

  # x-momentum, space
  [./x_momentum_space]
    type = INSMomentumLaplaceForm
    variable = vel_x
    u = vel_x
    v = vel_y
    pressure = p
    component = 0
  [../]

  # y-momentum, time
  [./y_momentum_time]
    type = INSMomentumTimeDerivative
    variable = vel_y
  [../]

  # y-momentum, space
  [./y_momentum_space]
    type = INSMomentumLaplaceForm
    variable = vel_y
    u = vel_x
    v = vel_y
    pressure = p
    component = 1
  [../]

 # temperature
 [./temperature_time]
   type = INSTemperatureTimeDerivative
   variable = T
 [../]

 [./temperature_space]
   type = INSTemperature
   variable = T
   u = vel_x
   v = vel_y
 [../]
[]

[BCs]
  [./x_no_slip]
    type = DirichletBC
    variable = vel_x
    boundary = 'bottom right left'
    value = 0.0
  [../]

  [./lid]
    type = FunctionDirichletBC
    variable = vel_x
    boundary = 'top'
    function = 'lid_function'
  [../]

  [./y_no_slip]
    type = DirichletBC
    variable = vel_y
    boundary = 'bottom right top left'
    value = 0.0
  [../]

  [./T_hot]
    type = DirichletBC
    variable = T
    boundary = 'bottom'
    value = 1
  [../]

  [./T_cold]
    type = DirichletBC
    variable = T
    boundary = 'top'
    value = 0
  [../]

  [./pressure_pin]
    type = DirichletBC
    variable = p
    boundary = 'pinned_node'
    value = 0
  [../]
[]

[Materials]
  [./const]
    type = GenericConstantMaterial
    block = 0
    prop_names = 'rho mu cp k'
    prop_values = '1  1  1  .01'
  [../]
[]

[Functions]
  [./lid_function]
    # We pick a function that is exactly represented in the velocity
    # space so that the Dirichlet conditions are the same regardless
    # of the mesh spacing.
    type = ParsedFunction
    value = '4*x*(1-x)'
  [../]
[]

[Preconditioning]
  [./SMP]
    type = SMP
    full = true
    solve_type = 'NEWTON'
  [../]
[]

[Executioner]
  type = Transient
  # Run for 100+ timesteps to reach steady state.
  num_steps = 5
  dt = .5
  dtmin = .5
  petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -sub_pc_factor_levels'
  petsc_options_value = 'asm      2               ilu          4'
  line_search = 'none'
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-13
  nl_max_its = 6
  l_tol = 1e-6
  l_max_its = 500
[]

[Outputs]
  file_base = lid_driven_out
  exodus = true
  perf_graph = true
[]

(test/tests/kernels/scalar_constraint/scalar_constraint_bc.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  xmin = 0
  xmax = 1
  ymin = 0
  ymax = 1
  nx = 3
  ny = 3
  elem_type = QUAD4
[]

# NL

[Variables]
  [./u]
    family = LAGRANGE
    order = FIRST
  [../]

  [./alpha]
    family = SCALAR
    order = FIRST
    initial_condition = 1
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[ScalarKernels]
  [./alpha_ced]
    type = AlphaCED
    variable = alpha
    value = 10
  [../]
[]

[BCs]
  [./left]
    type = ScalarVarBC
    variable = u
    boundary = '3'
    alpha = alpha
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = '1'
    value = 0
  [../]
[]

[Preconditioning]
  active = 'pc'

  [./pc]
    type = SMP
    full = true

  solve_type = 'PJFNK'
  [../]

  [./FDP_PJFNK]
    type = FDP
    full = true

  solve_type = 'PJFNK'

    # These options **together** cause a zero pivot in this problem, even without SUPG terms.
    # But using either option alone appears to be OK.
    # petsc_options_iname = '-mat_fd_coloring_err -mat_fd_type'
    # petsc_options_value = '1.e-10               ds'

    petsc_options_iname = '-mat_fd_coloring_err'
    petsc_options_value = '1.e-10'
    # petsc_options_iname = '-mat_fd_type'
    # petsc_options_value = 'ds'
  [../]
[] # End preconditioning block

[Executioner]
  type = Steady
[]

[Outputs]
  exodus = true
  hide = alpha
[]

(modules/functional_expansion_tools/examples/3D_volumetric_Cartesian_different_submesh/main.i)

# Derived from the example '3D_volumetric_Cartesian' with the following differences:
#
#   1) The number of x and y divisions in the sub app is not the same as the master app
#   2) The subapp mesh is skewed in x and z
[Mesh]
  type = GeneratedMesh
  dim = 3

  xmin = 0.0
  xmax = 10.0
  nx = 15

  ymin = 1.0
  ymax = 11.0
  ny = 25

  zmin = 2.0
  zmax = 12.0
  nz = 35
[]

[Variables]
  [./m]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[AuxVariables]
  [./s_in]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  [./diff_m]
    type = HeatConduction
    variable = m
  [../]
  [./time_diff_m]
    type = HeatConductionTimeDerivative
    variable = m
  [../]
  [./s_in] # Add in the contribution from the SubApp
    type = CoupledForce
    variable = m
    v = s_in
  [../]
[]

[AuxKernels]
  [./reconstruct_s_in]
    type = FunctionSeriesToAux
    variable = s_in
    function = FX_Basis_Value_Main
  [../]
[]

[Materials]
  [./Unobtanium]
    type = GenericConstantMaterial
    prop_names =  'thermal_conductivity specific_heat density'
    prop_values = '1.0                  1.0           1.0' # W/(cm K), J/(g K), g/cm^3
  [../]
[]

[ICs]
  [./start_m]
    type = ConstantIC
    variable = m
    value = 1
  [../]
[]

[BCs]
  [./surround]
    type = DirichletBC
    variable = m
    value = 1
    boundary = 'top bottom left right front back'
  [../]
[]

[Functions]
  [./FX_Basis_Value_Main]
    type = FunctionSeries
    series_type = Cartesian
    orders = '3   4   5'
    physical_bounds = '0.0  10.0    1.0 11.0    2.0 12.0'
    x = Legendre
    y = Legendre
    z = Legendre
  [../]
[]

[UserObjects]
  [./FX_Value_UserObject_Main]
    type = FXVolumeUserObject
    function = FX_Basis_Value_Main
    variable = m
  [../]
[]

[Postprocessors]
  [./average_value]
    type = ElementAverageValue
    variable = m
  [../]
  [./peak_value]
    type = ElementExtremeValue
    value_type = max
    variable = m
  [../]
  [./picard_iterations]
    type = NumFixedPointIterations
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 10
  dt = 0.5
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
  fixed_point_max_its = 30
  nl_rel_tol = 1e-8
  nl_abs_tol = 1e-9
  fixed_point_rel_tol = 1e-8
  fixed_point_abs_tol = 1e-9
[]

[Outputs]
  exodus = true
[]

[MultiApps]
  [./FXTransferApp]
    type = TransientMultiApp
    input_files = sub.i
  [../]
[]

[Transfers]
  [./ValueToSub]
    type = MultiAppFXTransfer
    to_multi_app = FXTransferApp
    this_app_object_name = FX_Value_UserObject_Main
    multi_app_object_name = FX_Basis_Value_Sub
  [../]
  [./ValueToMe]
    type = MultiAppFXTransfer
    from_multi_app = FXTransferApp
    this_app_object_name = FX_Basis_Value_Main
    multi_app_object_name = FX_Value_UserObject_Sub
  [../]
[]

(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/heat_conduction/test/tests/gap_heat_transfer_mortar/gap_heat_transfer_mortar.i)

[Mesh]
  [file]
    type = FileMeshGenerator
    file = 2blk-gap.e
  []
  [secondary]
    type = LowerDBlockFromSidesetGenerator
    sidesets = '101'
    new_block_id = '10001'
    new_block_name = 'secondary_lower'
    input = file
  []
  [primary]
    type = LowerDBlockFromSidesetGenerator
    sidesets = '100'
    new_block_id = '10000'
    new_block_name = 'primary_lower'
    input = secondary
  []
[]

[Problem]
  kernel_coverage_check = false
  material_coverage_check = false
[]

[Variables]
  [./temp]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  [../]

  [./lm]
    order = FIRST
    family = LAGRANGE
    block = 'secondary_lower'
  [../]
[]

[Materials]
  [./left]
    type = HeatConductionMaterial
    block = 1
    thermal_conductivity = 1000
    specific_heat = 1
  [../]

  [./right]
    type = HeatConductionMaterial
    block = 2
    thermal_conductivity = 500
    specific_heat = 1
  [../]
[]

[Kernels]
  [./hc]
    type = HeatConduction
    variable = temp
    use_displaced_mesh = false
    block = '1 2'
  [../]
[]

[Constraints]
  [./ced]
    type = GapConductanceConstraint
    variable = lm
    secondary_variable = temp
    k = 100
    primary_boundary = 100
    primary_subdomain = 10000
    secondary_boundary = 101
    secondary_subdomain = 10001
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = temp
    boundary = 'left'
    value = 1
  [../]

  [./right]
    type = DirichletBC
    variable = temp
    boundary = 'right'
    value = 0
  [../]
[]

[Preconditioning]
  [./fmp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
  nl_rel_tol = 1e-11
[]

[Outputs]
  exodus = true
[]

(test/tests/executioners/nl_forced_its/2d_diffusion_test.i)

[Mesh]
  [./square]
    type = GeneratedMeshGenerator
    nx = 2
    ny = 2
    dim = 2
  [../]
[]

[Variables]
  active = 'u'

  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  active = 'diff'

  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  # BCs cannot be preset due to Jacobian test
  active = 'left right'

  [./left]
    type = DirichletBC
    variable = u
    preset = false
    boundary = 3
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    preset = false
    boundary = 1
    value = 1
  [../]
[]

[Executioner]
  type = Steady
  nl_forced_its = 2
  nl_abs_tol = 1e-10
  nl_rel_tol = 1e-50
  solve_type = 'NEWTON'
[]

(modules/tensor_mechanics/test/tests/lagrangian/updated/convergence/2D/neumann.i)

# Simple 2D plane strain test

[GlobalParams]
  displacements = 'disp_x disp_y'
  large_kinematics = true
[]

[Variables]
  [disp_x]
  []
  [disp_y]
  []
[]

[Mesh]
  [msh]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 4
    ny = 4
  []
[]

[Kernels]
  [sdx]
    type = UpdatedLagrangianStressDivergence
    variable = disp_x
    component = 0
    use_displaced_mesh = true
  []
  [sdy]
    type = UpdatedLagrangianStressDivergence
    variable = disp_y
    component = 1
    use_displaced_mesh = true
  []
[]

[Functions]
  [pullx]
    type = ParsedFunction
    value = '50000 * t'
  []
  [pully]
    type = ParsedFunction
    value = '-30000 * t'
  []
[]

[BCs]
  [leftx]
    type = DirichletBC
    preset = true
    boundary = left
    variable = disp_x
    value = 0.0
  []
  [lefty]
    type = DirichletBC
    preset = true
    boundary = left
    variable = disp_y
    value = 0.0
  []
  [pull_x]
    type = FunctionNeumannBC
    boundary = right
    variable = disp_x
    function = pullx
  []
  [pull_y]
    type = FunctionNeumannBC
    boundary = top
    variable = disp_y
    function = pully
  []
[]

[Materials]
  [elastic_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 100000.0
    poissons_ratio = 0.3
  []
  [compute_stress]
    type = ComputeLagrangianLinearElasticStress
  []
  [compute_strain]
    type = ComputeLagrangianStrain
  []
[]

[Preconditioning]
  [smp]
    type = SMP
    full = true
  []
[]

[Executioner]
  type = Transient

  solve_type = 'newton'
  line_search = none

  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'

  l_max_its = 2
  l_tol = 1e-14
  nl_max_its = 15
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-12

  start_time = 0.0
  dt = 0.2
  dtmin = 0.2
  end_time = 1.0
[]

[Postprocessors]
  [nonlin]
    type = NumNonlinearIterations
  []
[]

[Outputs]
  exodus = false
  csv = true
[]

(test/tests/outputs/misc/default_names.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'


  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
  [./oversample]
    type = Exodus
    refinements = 1
  [../]
[]

(tutorials/tutorial02_multiapps/step01_multiapps/04_sub3_multiple.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [v]
  []
[]

[Kernels]
  [diff]
    type = Diffusion
    variable = v
  []
  [td]
    type = TimeDerivative
    variable = v
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = v
    boundary = left
    value = 0
  []
  [right]
    type = DirichletBC
    variable = v
    boundary = right
    value = 3
  []
[]

[Executioner]
  type = Transient
  end_time = 2
  dt = 1

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(test/tests/bcs/periodic/trapezoid_non_periodic.i)

[Mesh]
  file = trapezoid.e
  uniform_refine = 1
[]

[Variables]
  [u]
    order = FIRST
    family = LAGRANGE
  []
[]

[AuxVariables]
  [periodic_dist]
    order = FIRST
    family = LAGRANGE
  []
[]

[Kernels]
  [diff]
    type = Diffusion
    variable = u
  []

  [forcing]
    type = GaussContForcing
    variable = u
    x_center = 2
    y_center = -1
    x_spread = 0.25
    y_spread = 0.5
  []

  [dot]
    type = TimeDerivative
    variable = u
  []
[]

[AuxKernels]
  [periodic_dist]
    type = PeriodicDistanceAux
    variable = periodic_dist
    point = '0.2 1.7 0.0'
  []
[]

[BCs]
  [right]
    type = DirichletBC
    variable = u
    value = 1
    boundary = 2
  []
  [left]
    type = DirichletBC
    variable = u
    value = 2
    boundary = 2
  []
[]

[Executioner]
  type = Transient
  dt = 0.5
  num_steps = 6
  solve_type = NEWTON
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/notched_plastic_block/biaxial_smooth.i)

# Uses a multi-smooted version of Mohr-Coulomb (via CappedMohrCoulombStressUpdate and ComputeMultipleInelasticStress) to simulate the following problem.
# A cubical block is notched around its equator.
# All of its outer surfaces have roller BCs, but the notched region is free to move as needed
# The block is initialised with a high hydrostatic tensile stress
# Without the notch, the BCs do not allow contraction of the block, and this stress configuration is admissible
# With the notch, however, the interior parts of the block are free to move in order to relieve stress, and this causes plastic failure
# The top surface is then pulled upwards (the bottom is fixed because of the roller BCs)
# This causes more failure
[Mesh]
  [generated_mesh]
    type = GeneratedMeshGenerator
    dim = 3
    nx = 9
    ny = 9
    nz = 9
    xmin = 0
    xmax = 0.1
    ymin = 0
    ymax = 0.1
    zmin = 0
    zmax = 0.1
  []
  [block_to_remove_xmin]
    type = SubdomainBoundingBoxGenerator
    bottom_left = '-0.01 -0.01 0.045'
    top_right = '0.01 0.11 0.055'
    location = INSIDE
    block_id = 1
    input = generated_mesh
  []
  [block_to_remove_xmax]
    type = SubdomainBoundingBoxGenerator
    bottom_left = '0.09 -0.01 0.045'
    top_right = '0.11 0.11 0.055'
    location = INSIDE
    block_id = 1
    input = block_to_remove_xmin
  []
  [block_to_remove_ymin]
    type = SubdomainBoundingBoxGenerator
    bottom_left = '-0.01 -0.01 0.045'
    top_right = '0.11 0.01 0.055'
    location = INSIDE
    block_id = 1
    input = block_to_remove_xmax
  []
  [block_to_remove_ymax]
    type = SubdomainBoundingBoxGenerator
    bottom_left = '-0.01 0.09 0.045'
    top_right = '0.11 0.11 0.055'
    location = INSIDE
    block_id = 1
    input = block_to_remove_ymin
  []
  [remove_block]
    type = BlockDeletionGenerator
    block = 1
    input = block_to_remove_ymax
  []
[]

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
[]

[Modules/TensorMechanics/Master]
  [./all]
    add_variables = true
    incremental = true
    generate_output = 'max_principal_stress mid_principal_stress min_principal_stress stress_zz'
    eigenstrain_names = ini_stress
  [../]
[]

[Postprocessors]
  [./uz]
    type = PointValue
    point = '0 0 0.1'
    use_displaced_mesh = false
    variable = disp_z
  [../]
  [./s_zz]
    type = ElementAverageValue
    use_displaced_mesh = false
    variable = stress_zz
  [../]
  [./num_res]
    type = NumResidualEvaluations
  [../]
  [./nr_its] # num_iters is the average number of NR iterations encountered per element in this timestep
    type = ElementAverageValue
    variable = num_iters
  [../]
  [./max_nr_its] # max_num_iters is the maximum number of NR iterations encountered in the element during the whole simulation
    type = ElementExtremeValue
    variable = max_num_iters
  [../]
  [./runtime]
    type = PerfGraphData
    data_type = TOTAL
    section_name = 'Root'
  [../]
[]

[BCs]
  # back=zmin, front=zmax, bottom=ymin, top=ymax, left=xmin, right=xmax
  [./xmin_xzero]
    type = DirichletBC
    variable = disp_x
    boundary = left
    value = 0.0
  [../]
  [./xmax_xzero]
    type = DirichletBC
    variable = disp_x
    boundary = right
    value = 0.0
  [../]
  [./ymin_yzero]
    type = DirichletBC
    variable = disp_y
    boundary = bottom
    value = 0.0
  [../]
  [./ymax_yzero]
    type = DirichletBC
    variable = disp_y
    boundary = top
    value = 0.0
  [../]
  [./zmin_zzero]
    type = DirichletBC
    variable = disp_z
    boundary = back
    value = '0'
  [../]
  [./zmax_disp]
    type = FunctionDirichletBC
    variable = disp_z
    boundary = front
    function = '1E-6*max(t,0)'
  [../]
[]

[AuxVariables]
  [./mc_int]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./num_iters]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./max_num_iters]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./yield_fcn]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[AuxKernels]
  [./mc_int_auxk]
    type = MaterialStdVectorAux
    index = 0
    property = plastic_internal_parameter
    variable = mc_int
  [../]
  [./num_iters_auxk]
    type = MaterialRealAux
    property = plastic_NR_iterations
    variable = num_iters
  [../]
  [./max_num_iters_auxk]
    type = MaterialRealAux
    property = max_plastic_NR_iterations
    variable = max_num_iters
  [../]
  [./yield_fcn_auxk]
    type = MaterialStdVectorAux
    index = 6
    property = plastic_yield_function
    variable = yield_fcn
  [../]
[]

[UserObjects]
  [./ts]
    type = TensorMechanicsHardeningConstant
    value = 1E16
  [../]
  [./mc_coh]
    type = TensorMechanicsHardeningConstant
    value = 5E6
  [../]
  [./mc_phi]
    type = TensorMechanicsHardeningConstant
    value = 35
    convert_to_radians = true
  [../]
  [./mc_psi]
    type = TensorMechanicsHardeningConstant
    value = 10
    convert_to_radians = true
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 16E9
    poissons_ratio = 0.25
  [../]
  [./mc]
    type = CappedMohrCoulombStressUpdate
    tensile_strength = ts
    compressive_strength = ts
    cohesion = mc_coh
    friction_angle = mc_phi
    dilation_angle = mc_psi
    smoothing_tol = 0.2E6
    yield_function_tol = 1E-5
  [../]
  [./stress]
    type = ComputeMultipleInelasticStress
    inelastic_models = mc
    perform_finite_strain_rotations = false
  [../]
  [./strain_from_initial_stress]
    type = ComputeEigenstrainFromInitialStress
    initial_stress = '6E6 0 0  0 6E6 0  0 0 6E6'
    eigenstrain_name = ini_stress
  [../]
[]

[Preconditioning]
  [./andy]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  start_time = -1
  end_time = 10
  dt = 1
  solve_type = NEWTON
  type = Transient

  l_tol = 1E-2
  nl_abs_tol = 1E-5
  nl_rel_tol = 1E-7
  l_max_its = 200
  nl_max_its = 400

  petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
  petsc_options_value = ' asm      2              lu            gmres     200'
[]


[Outputs]
  file_base = biaxial_smooth
  perf_graph = true
  exodus = false
  csv = true
[]

(modules/tensor_mechanics/test/tests/beam/static_orientation/euler_small_strain_orientation_xz.i)

# A unit load is applied at the end of a cantilever beam of length 4m.
# The properties of the cantilever beam are as follows:
# Young's modulus (E) = 2.60072400269
# Shear modulus (G) = 1.0e4
# Poissons ratio (nu) = -0.9998699638
# Shear coefficient (k) = 0.85
# Cross-section area (A) = 0.554256
# Iy = 0.0141889 = Iz
# Length = 4 m

# For this beam, the dimensionless parameter alpha = kAGL^2/EI = 2.04e6

# The small deformation analytical deflection of the beam is given by
# delta = PL^3/3EI * (1 + 3.0 / alpha) = PL^3/3EI = 578 m

# Using 10 elements to discretize the beam element, the FEM solution is 576.866 m.
# The ratio beam FEM solution and analytical solution is 0.998.

# The beam centerline is positioned on the global XZ plane at a 45deg. angle.
# Loading is along the global Y axis.

# References:
# Prathap and Bashyam (1982), International journal for numerical methods in engineering, vol. 18, 195-210.

[Mesh]
  type = FileMesh
  file = euler_small_strain_orientation_inclined_xz.e
  displacements = 'disp_x disp_y disp_z'
[]

[Modules/TensorMechanics/LineElementMaster]
  [./all]
    add_variables = true
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'

    # Geometry parameters
    area = 0.554256
    Ay = 0.0
    Az = 0.0
    Iy = 0.0141889
    Iz = 0.0141889
    y_orientation = '0 1.0 0.0'
  [../]
[]

[Materials]
  [./elasticity]
    type = ComputeElasticityBeam
    youngs_modulus = 2.60072400269
    poissons_ratio = -0.9998699638
    shear_coefficient = 0.85
    block = 0
  [../]
  [./stress]
    type = ComputeBeamResultants
    block = 0
  [../]
[]

[BCs]
  [./fixx1]
    type = DirichletBC
    variable = disp_x
    boundary = 0
    value = 0.0
  [../]
  [./fixy1]
    type = DirichletBC
    variable = disp_y
    boundary = 0
    value = 0.0
  [../]
  [./fixz1]
    type = DirichletBC
    variable = disp_z
    boundary = 0
    value = 0.0
  [../]
  [./fixr1]
    type = DirichletBC
    variable = rot_x
    boundary = 0
    value = 0.0
  [../]
  [./fixr2]
    type = DirichletBC
    variable = rot_y
    boundary = 0
    value = 0.0
  [../]
  [./fixr3]
    type = DirichletBC
    variable = rot_z
    boundary = 0
    value = 0.0
  [../]
[]

[NodalKernels]
  [./force_y2]
    type = ConstantRate
    variable = disp_y
    boundary = 1
    rate = 1.0e-4
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]
[Executioner]
  type = Transient
  solve_type = NEWTON
  line_search = 'none'
  nl_max_its = 15
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-10

  dt = 1
  dtmin = 1
  end_time = 2
[]

[Postprocessors]
  [./disp_y]
    type = PointValue
    point = '2.8284271 0.0 2.8284271'
    variable = disp_y
  [../]
[]

[Outputs]
  csv = true
  exodus = false
[]

(modules/contact/test/tests/hertz_spherical/hertz_contact.i)

# Hertz Contact: Sphere on sphere

# Spheres have the same radius, Young's modulus, and Poisson's ratio.

# Define E:
# 1/E = (1-nu1^2)/E1 + (1-nu2^2)/E2
#
# Effective radius R:
# 1/R = 1/R1 + 1/R2
#
# F is the applied compressive load.
#
# Area of contact a::
# a^3 = 3FR/4E
#
# Depth of indentation d:
# d = a^2/R
#
#
# Let R1 = R2 = 2.  Then R = 1.
#
# Let nu1 = nu2 = 0.25, E1 = E2 = 1.40625e7.  Then E = 7.5e6.
#
# Let F = 10000.  Then a = 0.1, d = 0.01.
#
[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
  volumetric_locking_correction = true
[]


[Mesh]#Comment
  file = hertz_contact.e
[] # Mesh

[Functions]
  [./pressure]
    type = PiecewiseLinear
    x = '0. 1. 2.'
    y = '0. 1. 1.'
    scale_factor = 795.77471545947674 # 10000/pi/2^2
  [../]
  [./disp_y]
    type = PiecewiseLinear
    x = '0.  1.    2.'
    y = '0. -0.01 -0.01'
  [../]
[] # Functions

[Variables]

  [./disp_x]
    order = FIRST
    family = LAGRANGE
  [../]

  [./disp_y]
    order = FIRST
    family = LAGRANGE
  [../]

  [./disp_z]
    order = FIRST
    family = LAGRANGE
  [../]

[] # Variables

[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
  [../]
  [./vonmises]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./hydrostatic]
    order = CONSTANT
    family = MONOMIAL
  [../]

[] # AuxVariables

[Modules/TensorMechanics/Master]
  [./all]
    add_variables = true
    strain = SMALL
  #  extra_vector_tags = 'ref'
  [../]
[]

[AuxKernels]

  [./stress_xx]
    type = RankTwoAux
    rank_two_tensor = stress
    index_i = 0
    index_j = 0
    variable = stress_xx
  [../]
  [./stress_yy]
    type = RankTwoAux
    rank_two_tensor = stress
    index_i = 1
    index_j = 1
    variable = stress_yy
  [../]
  [./stress_zz]
    type = RankTwoAux
    rank_two_tensor = stress
    index_i = 2
    index_j = 2
    variable = stress_zz
  [../]
  [./stress_xy]
    type = RankTwoAux
    rank_two_tensor = stress
    index_i = 0
    index_j = 1
    variable = stress_xy
  [../]
  [./stress_yz]
    type = RankTwoAux
    rank_two_tensor = stress
    index_i = 1
    index_j = 2
    variable = stress_yz
  [../]
  [./stress_zx]
    type = RankTwoAux
    rank_two_tensor = stress
    index_i = 2
    index_j = 0
    variable = stress_zx
  [../]

[] # AuxKernels

[BCs]

  [./base_x]
    type = DirichletBC
    variable = disp_x
    boundary = 1000
    value = 0.0
  [../]
  [./base_y]
    type = DirichletBC
    variable = disp_y
    boundary = 1000
    value = 0.0
  [../]
  [./base_z]
    type = DirichletBC
    variable = disp_z
    boundary = 1000
    value = 0.0
  [../]

  [./symm_x]
    type = DirichletBC
    variable = disp_x
    boundary = 1
    value = 0.0
  [../]
  [./symm_z]
    type = DirichletBC
    variable = disp_z
    boundary = 3
    value = 0.0
  [../]
  [./disp_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 2
    function = disp_y
  [../]

[] # BCs

[Contact]
  [./dummy_name]
    primary = 1000
    secondary = 100
    normalize_penalty = true
    tangential_tolerance = 1e-3
    penalty = 1e+10
  [../]
[]

[Materials]

  [./tensor]
    type = ComputeIsotropicElasticityTensor
    block = '1'
    youngs_modulus = 1.40625e7
    poissons_ratio = 0.25
  [../]
  [./stress]
    type = ComputeLinearElasticStress
    block = '1'
  [../]

  [./tensor_1000]
    type = ComputeIsotropicElasticityTensor
    block = '1000'
    youngs_modulus = 1e6
    poissons_ratio = 0.0
  [../]
  [./stress_1000]
    type = ComputeLinearElasticStress
    block = '1000'
  [../]

[] # Materials

[Preconditioning]
  [./SMP]
    type = SMP
    full = true
  []
[]

[Executioner]

  type = Transient

  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu     superlu_dist'
  line_search = 'none'


  nl_abs_tol = 1e-7
  l_max_its = 200
  start_time = 0.0
  dt = 0.5
  end_time = 2.0
[] # Executioner

[Postprocessors]
  [./maxdisp]
    type = NodalVariableValue
    nodeid = 122 # 123-1 where 123 is the exodus node number of the top-center node
    variable = disp_y
  [../]
[]

[Outputs]
  [./out]
    type = Exodus
  [../]
[] # Outputs

(modules/tensor_mechanics/test/tests/cohesive_zone_model/czm_traction_separation_base.i)

# base test to check the implemantation traction separation laws
# Loads are expressed using functions. See the czm_materials/3DC section in the
# test file  for examples.
[Mesh]
  [./msh]
    type = GeneratedMeshGenerator
    dim = 3
    nx = 2
    ny = 1
    nz = 1
  []
  [./subdomain_1]
    type = SubdomainBoundingBoxGenerator
    input = msh
    bottom_left = '0 0 0'
    block_id = 1
    top_right = '0.5 1 1'
  []
  [./subdomain_2]
    type = SubdomainBoundingBoxGenerator
    input = subdomain_1
    bottom_left = '0.5 0 0'
    block_id = 2
    top_right = '1 1 1'
  []
  [./breakmesh]
    input = subdomain_2
    type = BreakMeshByBlockGenerator
  [../]
  [add_side_sets]
    input = breakmesh
    type = SideSetsFromNormalsGenerator
    normals = '0 -1  0
               0  1  0
               -1 0  0
               1  0  0
               0  0 -1
               0  0  1'
    fixed_normal = true
    new_boundary = 'y0 y1 x0 x1 z0 z1'
  []
[]

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
[]

[Modules/TensorMechanics/Master]
  [./all]
    strain = SMALL
    add_variables = true
    generate_output = 'stress_xx stress_yy stress_zz stress_yz stress_xz stress_xy'
  [../]
[]

[Modules/TensorMechanics/CohesiveZoneMaster]
  [./czm1]
    strain = SMALL
    boundary = 'interface'
    generate_output = 'traction_x traction_y traction_z normal_traction tangent_traction jump_x jump_y jump_z normal_jump tangent_jump'
  [../]
[]

[BCs]
  [./left_x]
    type = DirichletBC
    variable = disp_x
    preset = false
    boundary = x0
    value = 0.0
  [../]
  [./left_y]
    type = DirichletBC
    variable = disp_y
    preset = false
    boundary = x0
    value = 0.0
  [../]
  [./left_z]
    type = DirichletBC
    variable = disp_z
    preset = false
    boundary = x0
    value = 0.0
  [../]
  [./right_x]
    type = FunctionDirichletBC
    variable = disp_x
    preset = false
    boundary = x1
  [../]
  [./right_y]
    type = FunctionDirichletBC
    variable = disp_y
    preset = false
    boundary = x1
  [../]
  [./right_z]
    type = FunctionDirichletBC
    variable = disp_z
    preset = false
    boundary = x1
  [../]
[]

[Materials]
  [./Elasticity_tensor]
    type = ComputeElasticityTensor
    block = '1 2'
    fill_method = symmetric_isotropic
    C_ijkl = '0.3 0.5e8'
  [../]
  [./stress]
    type = ComputeLinearElasticStress
    block = '1 2'
  [../]
  [./czm_mat]
    boundary = 'interface'
  [../]
[]

[Preconditioning]
  [./SMP]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient
  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'
  solve_type = NEWTON
  nl_abs_tol = 1e-8
  nl_rel_tol = 1e-6
  nl_max_its = 5
  l_tol = 1e-10
  l_max_its = 50
  start_time = 0.0
  dt = 0.2
  end_time = 3
  dtmin = 0.2
  line_search = none
[]

[Outputs]
  [./out]
    type = Exodus
  [../]
[]

(test/tests/nodalkernels/jac_test/bc_jacobian_test.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 4
  ny = 4
[]

[Variables]
  [./u_x]
  [../]
  [./u_y]
  [../]
[]

[Kernels]
  [./diff_x]
    type = CoefDiffusion
    variable = u_x
    coef = 0.1
  [../]
  [./diff_y]
    type = CoefDiffusion
    variable = u_y
    coef = 0.1
  [../]
[]

[NodalKernels]
  [./test_y]
    type = JacobianCheck
    variable = u_y
    boundary = top
  [../]
  [./test_x]
    type = JacobianCheck
    variable = u_x
    boundary = top
  [../]
[]

[BCs]
  [./left_x]
    type = DirichletBC
    variable = u_x
    preset = false
    boundary = left
    value = 0
  [../]
  [./right_x]
    type = DirichletBC
    variable = u_x
    preset = false
    boundary = right
    value = 1
  [../]
  [./left_y]
    type = DirichletBC
    variable = u_y
    preset = false
    boundary = left
    value = 0
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 1
  dt = 0.1
  solve_type = NEWTON
# petsc_options = '-snes_check_jacobian -snes_check_jacobian_view'
  nl_max_its = 1
  nl_abs_tol = 1e0
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/creep_tangent_operator/creep.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 2
  second_order = true
[]

[GlobalParams]
  displacements = 'disp_x disp_y'
  volumetric_locking_correction = false
[]

[Functions]
  [./pull]
    type = PiecewiseLinear
    x = '0 10'
    y = '0 1e-3'
  [../]
[]

[Modules/TensorMechanics/Master]
  [./all]
    strain = FINITE
    add_variables = true
    use_finite_deform_jacobian = true
    generate_output = 'hydrostatic_stress'
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 1e10
    poissons_ratio = 0.3
  [../]

  [./elastic_strain]
    type = ComputeMultipleInelasticStress
    # inelastic_models = ''
    tangent_operator = nonlinear
  [../]

  [./creep_ten]
    type = PowerLawCreepStressUpdate
    coefficient = 10e-24
    n_exponent = 4
    activation_energy = 0
    base_name = creep_ten
  [../]
  [./creep_ten2]
    type = PowerLawCreepStressUpdate
    coefficient = 10e-24
    n_exponent = 4
    activation_energy = 0
    base_name = creep_ten2
  [../]
  [./creep_one]
    type = PowerLawCreepStressUpdate
    coefficient = 1e-24
    n_exponent = 4
    activation_energy = 0
    base_name = creep_one
  [../]
  [./creep_nine]
    type = PowerLawCreepStressUpdate
    coefficient = 9e-24
    n_exponent = 4
    activation_energy = 0
    base_name = creep_nine
  [../]
  [./creep_zero]
    type = PowerLawCreepStressUpdate
    coefficient = 0e-24
    n_exponent = 4
    activation_energy = 0
    base_name = creep_zero
  [../]
[]

[BCs]
  [./no_disp_x]
    type = DirichletBC
    variable = disp_x
    boundary = left
    value = 0.0
  [../]

  [./no_disp_y]
    type = DirichletBC
    variable = disp_y
    boundary = bottom
    value = 0.0
  [../]

  [./pull_disp_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = top
    function = pull
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient

  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'
  line_search = 'none'
  nl_rel_tol = 1e-5

  num_steps = 5
  dt = 1e-1
[]

[Postprocessors]
  [./max_disp_x]
    type = ElementExtremeValue
    variable = disp_x
  [../]
  [./max_disp_y]
    type = ElementExtremeValue
    variable = disp_y
  [../]
  [./max_hydro]
    type = ElementAverageValue
    variable = hydrostatic_stress
  [../]
  [./dt]
    type = TimestepSize
  [../]
  [./num_lin]
    type = NumLinearIterations
    outputs = console
  [../]
  [./num_nonlin]
    type = NumNonlinearIterations
    outputs = console
  [../]
[]

[Outputs]
  csv = true
  perf_graph = true
[]

[Debug]
  show_var_residual_norms = true
[]

(test/tests/outputs/checkpoint/checkpoint_interval.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
  parallel_type = replicated
[]

[Variables]
  [u]
  []
[]

[Kernels]
  [diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  []
  [time]
    type = TimeDerivative
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  []
  [right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  []
[]

[Executioner]
  type = Transient
  num_steps = 11
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
  [out]
    type = Checkpoint
    interval = 3
    num_files = 2
  []
[]

(modules/porous_flow/test/tests/heat_conduction/no_fluid.i)

# 0phase heat conduction.
# apply a boundary condition of T=300 to a bar that
# is initially at T=200, and observe the expected
# error-function response
[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 10
  xmin = 0
  xmax = 100
[]

[GlobalParams]
  PorousFlowDictator = dictator
[]

[Variables]
  [temp]
    initial_condition = 200
  []
[]

[Kernels]
  [energy_dot]
    type = PorousFlowEnergyTimeDerivative
    variable = temp
  []
  [heat_conduction]
    type = PorousFlowHeatConduction
    variable = temp
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'temp'
    number_fluid_phases = 0
    number_fluid_components = 0
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
    temperature = temp
  []
  [thermal_conductivity]
    type = PorousFlowThermalConductivityIdeal
    dry_thermal_conductivity = '2.2 0 0  0 0 0  0 0 0'
  []
  [porosity]
    type = PorousFlowPorosityConst
    porosity = 0.1
  []
  [rock_heat]
    type = PorousFlowMatrixInternalEnergy
    specific_heat_capacity = 2.2
    density = 0.5
  []
[]

[BCs]
  [left]
    type = DirichletBC
    boundary = left
    value = 300
    variable = temp
  []
[]


[Preconditioning]
  [andy]
    type = SMP
    full = true
  []
[]

[Executioner]
  type = Transient
  solve_type = Newton
  dt = 1E1
  end_time = 1E2
[]

[Postprocessors]
  [t000]
    type = PointValue
    variable = temp
    point = '0 0 0'
    execute_on = 'initial timestep_end'
  []
  [t010]
    type = PointValue
    variable = temp
    point = '10 0 0'
    execute_on = 'initial timestep_end'
  []
  [t020]
    type = PointValue
    variable = temp
    point = '20 0 0'
    execute_on = 'initial timestep_end'
  []
  [t030]
    type = PointValue
    variable = temp
    point = '30 0 0'
    execute_on = 'initial timestep_end'
  []
  [t040]
    type = PointValue
    variable = temp
    point = '40 0 0'
    execute_on = 'initial timestep_end'
  []
  [t050]
    type = PointValue
    variable = temp
    point = '50 0 0'
    execute_on = 'initial timestep_end'
  []
  [t060]
    type = PointValue
    variable = temp
    point = '60 0 0'
    execute_on = 'initial timestep_end'
  []
  [t070]
    type = PointValue
    variable = temp
    point = '70 0 0'
    execute_on = 'initial timestep_end'
  []
  [t080]
    type = PointValue
    variable = temp
    point = '80 0 0'
    execute_on = 'initial timestep_end'
  []
  [t090]
    type = PointValue
    variable = temp
    point = '90 0 0'
    execute_on = 'initial timestep_end'
  []
  [t100]
    type = PointValue
    variable = temp
    point = '100 0 0'
    execute_on = 'initial timestep_end'
  []
[]

[Outputs]
  file_base = no_fluid
  [csv]
    type = CSV
  []
  exodus = false
[]

(test/tests/kernels/block_kernel/block_kernel_test.i)

[Mesh]
  file = rectangle.e
  uniform_refine = 1
[]

[Variables]
  [./u]
    order = FIRST
    family = LAGRANGE
    initial_condition = 1.0
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]

  [./body_force]
    type = BodyForce
    variable = u
    block = 1
    value = 10
    function = 'x+y'
  [../]

  [./time]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./right]
    type = DirichletBC
    variable = u
    boundary = 2
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'
  dt = 0.1
  num_steps = 10
[]

[Outputs]
  file_base = out
  exodus = true
[]

(modules/richards/test/tests/gravity_head_1/gh_fu_11.i)

# unsaturated = false
# gravity = true
# supg = false
# transient = true

[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 1
  xmin = -1
  xmax = 1
[]

[BCs]
  [./left]
    type = DirichletBC
    boundary = left
    value = 1
    variable = pressure
  [../]
[]


[GlobalParams]
  richardsVarNames_UO = PPNames
  density_UO = DensityConstBulk
  relperm_UO = RelPermPower
  SUPG_UO = SUPGnone
  sat_UO = Saturation
  seff_UO = SeffVG
[]

[UserObjects]
  [./PPNames]
    type = RichardsVarNames
    richards_vars = pressure
  [../]
  [./DensityConstBulk]
    type = RichardsDensityConstBulk
    dens0 = 1
    bulk_mod = 1.0E3
  [../]
  [./SeffVG]
    type = RichardsSeff1VG
    m = 0.8
    al = 1
  [../]
  [./RelPermPower]
    type = RichardsRelPermPower
    simm = 0.0
    n = 2
  [../]
  [./Saturation]
    type = RichardsSat
    s_res = 0.1
    sum_s_res = 0.1
  [../]
  [./SUPGnone]
    type = RichardsSUPGnone
  [../]
[]

[Variables]
  [./pressure]
    order = FIRST
    family = LAGRANGE
    [./InitialCondition]
      type = RandomIC
      block = 0
      min = 0
      max = 1
    [../]
  [../]
[]


[Kernels]
  active = 'richardsf richardst'
  [./richardst]
    type = RichardsMassChange
    variable = pressure
  [../]
  [./richardsf]
    type = RichardsFullyUpwindFlux
    variable = pressure
  [../]
[]

[Materials]
  [./rock]
    type = RichardsMaterial
    block = 0
    mat_porosity = 0.1
    mat_permeability = '1E-5 0 0  0 1E-5 0  0 0 1E-5'
    viscosity = 1E-3
    gravity = '-1 0 0'
    linear_shape_fcns = true
  [../]
[]


[Preconditioning]
  [./andy]
    type = SMP
    full = true
    petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
    petsc_options_value = 'bcgs bjacobi 1E-15 1E-10 10000'
  [../]
[]

[Executioner]
  type = Transient
  solve_type = Newton
  dt = 1E10
  end_time = 1E10
[]

[Outputs]
  execute_on = 'timestep_end'
  file_base = gh_fu_11
  exodus = true
[]

(test/tests/multiapps/full_solve_multiapp/sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 5
  dt = 0.01

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/j_integral/j_integral_3d_points.i)

#This tests the J-Integral evaluation capability.
#This is a 3d extrusion of a 2d plane strain model with 2 elements
#through the thickness, and calculates the J-Integrals using options
#to treat it as 3d.
#The analytic solution for J1 is 2.434.  This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.

[GlobalParams]
  order = FIRST
  family = LAGRANGE
  displacements = 'disp_x disp_y disp_z'
  volumetric_locking_correction = true
[]

[Mesh]
  file = crack3d.e
[]

[AuxVariables]
  [./SED]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[Functions]
  [./rampConstant]
    type = PiecewiseLinear
    x = '0. 1.'
    y = '0. 1.'
    scale_factor = -1e2
  [../]
[]

[DomainIntegral]
  integrals = JIntegral
  crack_front_points = '0 -10 .5
                        0 -10 0
                        0 -10 -.5'
  crack_direction_method = CrackDirectionVector
  crack_direction_vector = '1 0 0'
  radius_inner = '4.0 5.5'
  radius_outer = '5.5 7.0'
  output_q = false
  incremental = true
[]

[Modules/TensorMechanics/Master]
  [./master]
    strain = FINITE
    add_variables = true
    incremental = true
    generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
  [../]
[]

[AuxKernels]
  [./SED]
    type = MaterialRealAux
    variable = SED
    property = strain_energy_density
    execute_on = timestep_end
  [../]
[]

[BCs]
  [./crack_y]
    type = DirichletBC
    variable = disp_y
    boundary = 100
    value = 0.0
  [../]
  [./no_z]
    type = DirichletBC
    variable = disp_z
    boundary = 500
    value = 0.0
  [../]
  [./no_z2]
    type = DirichletBC
    variable = disp_z
    boundary = 510
    value = 0.0
  [../]

  [./no_x]
    type = DirichletBC
    variable = disp_x
    boundary = 700
    value = 0.0
  [../]

  [./Pressure]
    [./Side1]
      boundary = 400
      function = rampConstant
    [../]
  [../]

[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 207000
    poissons_ratio = 0.3
  [../]
  [./elastic_stress]
    type = ComputeFiniteStrainElasticStress
  [../]
[]


[Executioner]
  type = Transient

  petsc_options = '-snes_ksp_ew'
  petsc_options_iname = '-ksp_gmres_restart'
  petsc_options_value = '101'

  line_search = 'none'

  l_max_its = 50
  nl_max_its = 20
  nl_abs_tol = 1e-5
  l_tol = 1e-2

  start_time = 0.0
  dt = 1

  end_time = 1
  num_steps = 1
[]

[Outputs]
  file_base = j_integral_3d_points_out
  exodus = true
  csv = true
[]

(test/tests/misc/check_error/bad_bc_test.i)

[Mesh]
  [./square]
    type = GeneratedMeshGenerator
    nx = 2
    ny = 2
    dim = 2
  [../]
[]

[Variables]
  active = 'u'

  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  active = 'diff'

  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  active = 'left right'

  # Test for bad BC
  [./left]
    type = Foo
    variable = u
    boundary = 3
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 1
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'
[]

[Outputs]
  file_base = out
  exodus = true
[]

(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/modular_gap_heat_transfer_mortar_displaced_conduction.i)

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Mesh]
  [file]
    type = FileMeshGenerator
    file = 2blk-gap.e
  []
  [secondary]
    type = LowerDBlockFromSidesetGenerator
    sidesets = '101'
    new_block_id = 10001
    new_block_name = 'secondary_lower'
    input = file
  []
  [primary]
    type = LowerDBlockFromSidesetGenerator
    sidesets = '100'
    new_block_id = 10000
    new_block_name = 'primary_lower'
    input = secondary
  []
  allow_renumbering = false
[]

[Problem]
  kernel_coverage_check = false
  material_coverage_check = false
[]

[Variables]
  [temp]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
  [disp_x]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
  [disp_y]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
  [lm]
    order = FIRST
    family = LAGRANGE
    block = 'secondary_lower'
  []
[]

[Materials]
  [left]
    type = ADHeatConductionMaterial
    block = 1
    thermal_conductivity = 0.01
    specific_heat = 1
  []

  [right]
    type = ADHeatConductionMaterial
    block = 2
    thermal_conductivity = 0.005
    specific_heat = 1
  []
[]

[Kernels]
  [hc_displaced_block]
    type = ADHeatConduction
    variable = temp
    use_displaced_mesh = true
    block = '1'
  []
  [hc_undisplaced_block]
    type = ADHeatConduction
    variable = temp
    use_displaced_mesh = false
    block = '2'
  []
  [disp_x]
    type = Diffusion
    variable = disp_x
    block = '1 2'
  []
  [disp_y]
    type = Diffusion
    variable = disp_y
    block = '1 2'
  []
[]

[UserObjects]
  [conduction]
    type = GapFluxModelConduction
    temperature = temp
    boundary = 100
    gap_conductivity = 10.0
  []
[]

[Constraints]
  [ced]
    type = ModularGapConductanceConstraint
    variable = lm
    secondary_variable = temp
    use_displaced_mesh = true
    primary_boundary = 100
    primary_subdomain = 10000
    secondary_boundary = 101
    secondary_subdomain = 10001
    gap_flux_models = conduction
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = temp
    boundary = 'left'
    value = 100
  []

  [right]
    type = DirichletBC
    variable = temp
    boundary = 'right'
    value = 0
  []

  [left_disp_x]
    type = DirichletBC
    preset = false
    variable = disp_x
    boundary = 'left'
    value = .1
  []
  [right_disp_x]
    type = DirichletBC
    preset = false
    variable = disp_x
    boundary = 'right'
    value = 0
  []
  [bottom_disp_y]
    type = DirichletBC
    preset = false
    variable = disp_y
    boundary = 'bottom'
    value = 0
  []
[]

[Preconditioning]
  [fmp]
    type = SMP
    full = true
    solve_type = 'NEWTON'
  []
[]

[Executioner]
  type = Steady
  nl_rel_tol = 1e-11
  nl_abs_tol = 1.0e-10
[]


[VectorPostprocessors]
  [NodalTemperature]
    type = NodalValueSampler
    sort_by = id
    boundary = '100 101'
    variable = 'temp'
  []
[]

[Outputs]
  exodus = false
  csv = true
[]

(test/tests/auxkernels/parsed_aux/parsed_aux_test.i)

[Mesh]
  type = GeneratedMesh

  dim = 2

  xmin = 0
  xmax = 1

  ymin = 0
  ymax = 1

  nx = 10
  ny = 10
[]

[Variables]
  [u]
    order = FIRST
    family = LAGRANGE
  []

  [v]
    order = FIRST
    family = LAGRANGE
  []
[]

[AuxVariables]
  [parsed]
    order = FIRST
    family = LAGRANGE
  []
[]

[Kernels]
  [diff_u]
    type = Diffusion
    variable = u
  []

  [diff_v]
    type = Diffusion
    variable = v
  []
[]

[BCs]
  [left_u]
    type = DirichletBC
    variable = u
    boundary = 2
    value = 0
  []

  [right_u]
    type = DirichletBC
    variable = u
    boundary = 0
    value = 1
  []

  [left_v]
    type = DirichletBC
    variable = v
    boundary = 3
    value = 0
  []

  [right_v]
    type = DirichletBC
    variable = v
    boundary = 1
    value = 1
  []
[]

[Bounds]
  [u_bounds]
    type = ParsedAux
    variable = parsed
    args = 'u v'
    function = '(u-0.5)^3*v'
  []
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'
[]

[Outputs]
  file_base = out
  exodus = true
[]

(modules/tensor_mechanics/test/tests/weak_plane_shear/small_deform4.i)

# apply a pure tension, then some shear
# the BCs are designed to map out the yield function, showing
# the affect of 'cap' smoothing
[GlobalParams]
  displacements = 'x_disp y_disp z_disp'
[]

[Mesh]
  type = GeneratedMesh
  dim = 3
  xmin = -0.5
  xmax = 0.5
  ymin = -0.5
  ymax = 0.5
  zmin = -0.5
  zmax = 0.5
[]

[Modules/TensorMechanics/Master/all]
  strain = FINITE
  add_variables = true
  generate_output = 'stress_xz stress_zx stress_yz stress_zz'
[]

[BCs]
  [bottomx]
    type = DirichletBC
    variable = x_disp
    boundary = back
    value = 0.0
  []
  [bottomy]
    type = DirichletBC
    variable = y_disp
    boundary = back
    value = 0.0
  []
  [bottomz]
    type = DirichletBC
    variable = z_disp
    boundary = back
    value = 0.0
  []

  [topx]
    type = FunctionDirichletBC
    variable = x_disp
    boundary = front
    function = 'if(t<1E-6,0,3*(t-1E-6)*(t-1E-6)*1E6)'
  []
  [topy]
    type = FunctionDirichletBC
    variable = y_disp
    boundary = front
    function = 'if(t<1E-6,0,5*(t-1E-6)*(t-1E-6)*1E6)'
  []
  [topz]
    type = FunctionDirichletBC
    variable = z_disp
    boundary = front
    function = 'if(t<1E-6,t,1E-6)'
  []
[]

[AuxVariables]
  [yield_fcn]
    order = CONSTANT
    family = MONOMIAL
  []
  [iter]
    order = CONSTANT
    family = MONOMIAL
  []
[]

[AuxKernels]
  [yield_fcn_auxk]
    type = MaterialStdVectorAux
    property = plastic_yield_function
    index = 0
    variable = yield_fcn
  []
  [iter_auxk]
    type = MaterialRealAux
    property = plastic_NR_iterations
    variable = iter
  []
[]

[Postprocessors]
  [s_xz]
    type = PointValue
    point = '0 0 0'
    variable = stress_xz
  []
  [s_yz]
    type = PointValue
    point = '0 0 0'
    variable = stress_yz
  []
  [s_zz]
    type = PointValue
    point = '0 0 0'
    variable = stress_zz
  []
  [f]
    type = PointValue
    point = '0 0 0'
    variable = yield_fcn
  []
  [iter]
    type = PointValue
    point = '0 0 0'
    variable = iter
  []
[]

[UserObjects]
  [coh]
    type = TensorMechanicsHardeningConstant
    value = 1E3
  []
  [tanphi]
    type = TensorMechanicsHardeningConstant
    value = 1
  []
  [tanpsi]
    type = TensorMechanicsHardeningConstant
    value = 0.08748866
  []
  [wps]
    type = TensorMechanicsPlasticWeakPlaneShear
    cohesion = coh
    tan_friction_angle = tanphi
    tan_dilation_angle = tanpsi
    tip_scheme = cap
    smoother = 0
    cap_rate = 0.001
    cap_start = -1000.0
    yield_function_tolerance = 1E-3
    internal_constraint_tolerance = 1E-6
  []
[]

[Materials]
  [elasticity_tensor]
    type = ComputeElasticityTensor
    fill_method = symmetric_isotropic
    C_ijkl = '1E9 0.5E9'
  []
  [mc]
    type = ComputeMultiPlasticityStress
    ep_plastic_tolerance = 1E-4
    plastic_models = wps
    transverse_direction = '0 0 1'
    debug_fspb = crash
    debug_jac_at_stress = '1E4 2E4 3E4 2E4 -4E4 5E4 3E4 5E4 6E8'
    debug_jac_at_pm = 1
    debug_jac_at_intnl = 1
    debug_stress_change = 1E-3
    debug_pm_change = 1E-5
    debug_intnl_change = 1E-5
  []
[]

[Executioner]
  end_time = 2E-6
  dt = 1E-7
  type = Transient
[]

[Outputs]
  csv = true
[]

(modules/tensor_mechanics/test/tests/generalized_plane_strain/generalized_plane_strain_increment.i)

[GlobalParams]
  displacements = 'disp_x disp_y'
  scalar_out_of_plane_strain = scalar_strain_zz
  block = 0
[]

[Mesh]
  [./square]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 2
    ny = 2
  [../]
[]

[Variables]
  [./scalar_strain_zz]
    order = FIRST
    family = SCALAR
  [../]
[]

[AuxVariables]
  [./temp]
  [../]
  [./saved_x]
  [../]
  [./saved_y]
  [../]
[]

[Postprocessors]
  [./react_z]
    type = MaterialTensorIntegral
    rank_two_tensor = stress
    index_i = 2
    index_j = 2
  [../]
[]

[Modules/TensorMechanics/Master]
  [./all]
    strain = SMALL
    incremental = true
    add_variables = true
    generate_output = 'stress_xx stress_xy stress_yy stress_zz strain_xx strain_xy strain_yy strain_zz'
    planar_formulation = GENERALIZED_PLANE_STRAIN
    eigenstrain_names = eigenstrain
    scalar_out_of_plane_strain = scalar_strain_zz
    temperature = temp
    save_in = 'saved_x saved_y'
  [../]
[]

[AuxKernels]
  [./tempfuncaux]
    type = FunctionAux
    variable = temp
    function = tempfunc
    use_displaced_mesh = false
  [../]
[]

[Functions]
  [./tempfunc]
    type = ParsedFunction
    value = '(1-x)*t'
  [../]
[]

[BCs]
  [./bottomx]
    type = DirichletBC
    boundary = 0
    variable = disp_x
    value = 0.0
  [../]
  [./bottomy]
    type = DirichletBC
    boundary = 0
    variable = disp_y
    value = 0.0
  [../]
[]

[Materials]
  [./elastic_tensor]
    type = ComputeIsotropicElasticityTensor
    poissons_ratio = 0.3
    youngs_modulus = 1e6
  [../]
  [./thermal_strain]
    type = ComputeThermalExpansionEigenstrain
    temperature = temp
    thermal_expansion_coeff = 0.02
    stress_free_temperature = 0.5
    eigenstrain_name = eigenstrain
  [../]
  [./stress]
    type = ComputeStrainIncrementBasedStress
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient

  solve_type = PJFNK
  line_search = none

  # controls for linear iterations
  l_max_its = 100
  l_tol = 1e-4

  # controls for nonlinear iterations
  nl_max_its = 15
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-5

  # time control
  start_time = 0.0
  dt = 1.0
  dtmin = 1.0
  end_time = 2.0
[]

[Outputs]
  exodus = true
[]

(test/tests/geomsearch/3d_moving_penetration/pl_test4q.i)

[GlobalParams]
  order = SECOND
  family = LAGRANGE
[]

[Mesh]
  file = pl_test4q.e
  displacements = 'disp_x disp_y disp_z'
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
  [./disp_z]
  [../]
[]

[AuxVariables]
  [./distance]
  [../]
  [./tangential_distance]
  [../]
  [./normal_x]
  [../]
  [./normal_y]
  [../]
  [./normal_z]
  [../]
  [./closest_point_x]
  [../]
  [./closest_point_y]
  [../]
  [./closest_point_z]
  [../]
  [./element_id]
  [../]
  [./side]
  [../]
[]

[Kernels]
  [./diff_x]
    type = Diffusion
    variable = disp_x
  [../]
  [./diff_y]
    type = Diffusion
    variable = disp_y
  [../]
  [./diff_z]
    type = Diffusion
    variable = disp_z
  [../]
[]

[AuxKernels]
  [./penetrate]
    type = PenetrationAux
    variable = distance
    boundary = 11            #secondary
    paired_boundary = 12     #primary
  [../]

  [./penetrate2]
    type = PenetrationAux
    variable = distance
    boundary = 12            #secondary
    paired_boundary = 11     #primary
  [../]

  [./penetrate3]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 11
    paired_boundary = 12
    quantity = tangential_distance
  [../]

  [./penetrate4]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 12
    paired_boundary = 11
    quantity = tangential_distance
  [../]

  [./penetrate5]
    type = PenetrationAux
    variable = normal_x
    boundary = 11
    paired_boundary = 12
    quantity = normal_x
  [../]

  [./penetrate6]
    type = PenetrationAux
    variable = normal_x
    boundary = 12
    paired_boundary = 11
    quantity = normal_x
  [../]

  [./penetrate7]
    type = PenetrationAux
    variable = normal_y
    boundary = 11
    paired_boundary = 12
    quantity = normal_y
  [../]

  [./penetrate8]
    type = PenetrationAux
    variable = normal_y
    boundary = 12
    paired_boundary = 11
    quantity = normal_y
  [../]

  [./penetrate9]
    type = PenetrationAux
    variable = normal_z
    boundary = 11
    paired_boundary = 12
    quantity = normal_z
  [../]

  [./penetrate10]
    type = PenetrationAux
    variable = normal_z
    boundary = 12
    paired_boundary = 11
    quantity = normal_z
  [../]

  [./penetrate11]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 11
    paired_boundary = 12
    quantity = closest_point_x
  [../]

  [./penetrate12]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 12
    paired_boundary = 11
    quantity = closest_point_x
  [../]

  [./penetrate13]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 11
    paired_boundary = 12
    quantity = closest_point_y
  [../]

  [./penetrate14]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 12
    paired_boundary = 11
    quantity = closest_point_y
  [../]

  [./penetrate15]
    type = PenetrationAux
    variable = closest_point_z
    boundary = 11
    paired_boundary = 12
    quantity = closest_point_z
  [../]

  [./penetrate16]
    type = PenetrationAux
    variable = closest_point_z
    boundary = 12
    paired_boundary = 11
    quantity = closest_point_z
  [../]

  [./penetrate17]
    type = PenetrationAux
    variable = element_id
    boundary = 11
    paired_boundary = 12
    quantity = element_id
  [../]

  [./penetrate18]
    type = PenetrationAux
    variable = element_id
    boundary = 12
    paired_boundary = 11
    quantity = element_id
  [../]

  [./penetrate19]
    type = PenetrationAux
    variable = side
    boundary = 11
    paired_boundary = 12
    quantity = side
  [../]

  [./penetrate20]
    type = PenetrationAux
    variable = side
    boundary = 12
    paired_boundary = 11
    quantity = side
  [../]
[]

[BCs]
  [./b1x]
    type = DirichletBC
    variable = disp_x
    boundary = 1
    value = 0
  [../]

  [./b1y]
    type = DirichletBC
    variable = disp_y
    boundary = 1
    value = 0
  [../]

  [./b1z]
    type = DirichletBC
    variable = disp_z
    boundary = 1
    value = 0
  [../]

  [./b2x]
    type = DirichletBC
    variable = disp_x
    boundary = 2
    value = 0
  [../]

  [./b2y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 2
    function = disp_y
  [../]

  [./b2z]
    type = DirichletBC
    variable = disp_z
    boundary = 2
    value = 0
  [../]
[]

[Functions]
  [./disp_y]
    type = PiecewiseLinear
    x = '0.0 0.25 0.75 1.0'
    y = '0.0 2.0 -2.0  0.0'
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'
  petsc_options = '-snes_ksp_ew'

  nl_rel_tol = 1e-9
  l_max_its = 10

  start_time = 0.0
  dt = 0.025
  end_time = 1.0
  [./Quadrature]
    order = THIRD
  [../]
[]

[Outputs]
  file_base = pl_test4q_out
  exodus = true
[]

(test/tests/transfers/multiapp_projection_transfer/fromsub_master.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  xmin = 0
  ymin = 0
  xmax = 9
  ymax = 9
  nx = 9
  ny = 9
[]

[Variables]
  [u]
  []
[]

[AuxVariables]
  [v_nodal]
  []
  [v_elemental]
    order = CONSTANT
    family = MONOMIAL
  []
  [x_nodal]
  []
  [x_elemental]
    order = CONSTANT
    family = MONOMIAL
  []
[]

[Kernels]
  [diff]
    type = Diffusion
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  []
  [right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  []
[]

[Executioner]
  type = Transient
  num_steps = 1
  dt = 1
  solve_type = 'NEWTON'
[]

[Outputs]
  [out]
    type = Exodus
    elemental_as_nodal = true
  []
[]

[MultiApps]
  [sub]
    type = TransientMultiApp
    app_type = MooseTestApp
    positions = '1 1 0 5 5 0'
    input_files = fromsub_sub.i
  []
[]

[Transfers]
  [v_nodal_tr]
    type = MultiAppProjectionTransfer
    from_multi_app = sub
    source_variable = v
    variable = v_nodal
  []
  [v_elemental_tr]
    type = MultiAppProjectionTransfer
    from_multi_app = sub
    source_variable = v
    variable = v_elemental
  []
  [x_elemental_tr]
    type = MultiAppProjectionTransfer
    from_multi_app = sub
    source_variable = x
    variable = x_elemental
  []
  [x_nodal_tr]
    type = MultiAppProjectionTransfer
    from_multi_app = sub
    source_variable = x
    variable = x_nodal
  []
[]

(test/tests/multiapps/sub_cycling_failure/sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Problem]
  type = FailingProblem
  fail_step = 15
[]

[Executioner]
  type = Transient
  num_steps = 4
  dt = 0.01
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(test/tests/postprocessors/element_l2_norm/element_l2_norm.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 3
  ny = 3
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Postprocessors]
  [./L2_norm]
    type = ElementL2Norm
    variable = u
  [../]
[]

[Executioner]
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  csv = true
[]

(test/tests/controls/time_periods/aux_kernels/enable_disable.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Dampers]
  [./const_damp]
    type = ConstantDamper
    damping = 0.9
  [../]
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/beam/eigenstrain/eigenstrain_from_var.i)

# Test for eigenstrain from variables

# A constant axial eigenstrain of 0.01 is applied to a beam of length
# 4 m. The beam is fixed at one end. The eigenstrain causes a change in
# length of 0.04 m irrespective of the material properties of the beam.

[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 10
  xmin = 0.0
  xmax = 4.0
  displacements = 'disp_x disp_y disp_z'
[]

[Variables]
  [./disp_x]
    order = FIRST
    family = LAGRANGE
  [../]
  [./disp_y]
    order = FIRST
    family = LAGRANGE
  [../]
  [./disp_z]
    order = FIRST
    family = LAGRANGE
  [../]
  [./rot_x]
    order = FIRST
    family = LAGRANGE
  [../]
  [./rot_y]
    order = FIRST
    family = LAGRANGE
  [../]
  [./rot_z]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[AuxVariables]
  [./thermal_eig]
  [../]
  [./zero1]
  [../]
  [./zero2]
  [../]
[]

[AuxKernels]
  [./thermal_eig]
    type = ConstantAux
    value = 0.01
    variable = thermal_eig
  [../]
[]

[BCs]
  [./fixx1]
    type = DirichletBC
    variable = disp_x
    boundary = left
    value = 0.0
  [../]
  [./fixy1]
    type = DirichletBC
    variable = disp_y
    boundary = left
    value = 0.0
  [../]
  [./fixz1]
    type = DirichletBC
    variable = disp_z
    boundary = left
    value = 0.0
  [../]
  [./fixr1]
    type = DirichletBC
    variable = rot_x
    boundary = left
    value = 0.0
  [../]
  [./fixr2]
    type = DirichletBC
    variable = rot_y
    boundary = left
    value = 0.0
  [../]
  [./fixr3]
    type = DirichletBC
    variable = rot_z
    boundary = left
    value = 0.0
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]
[Executioner]
  type = Transient
  solve_type = NEWTON
  line_search = 'none'
  nl_max_its = 15
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-10

  dt = 1
  dtmin = 1
  end_time = 2
[]

[Kernels]
  [./solid_disp_x]
    type = StressDivergenceBeam
    block = '0'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'
    component = 0
    variable = disp_x
  [../]
  [./solid_disp_y]
    type = StressDivergenceBeam
    block = '0'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'
    component = 1
    variable = disp_y
  [../]
  [./solid_disp_z]
    type = StressDivergenceBeam
    block = '0'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'
    component = 2
    variable = disp_z
  [../]
  [./solid_rot_x]
    type = StressDivergenceBeam
    block = '0'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'
    component = 3
    variable = rot_x
  [../]
  [./solid_rot_y]
    type = StressDivergenceBeam
    block = '0'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'
    component = 4
    variable = rot_y
  [../]
  [./solid_rot_z]
    type = StressDivergenceBeam
    block = '0'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'
    component = 5
    variable = rot_z
  [../]
[]

[Materials]
  [./elasticity]
    type = ComputeElasticityBeam
    youngs_modulus = 1e6
    poissons_ratio = 0.3
    shear_coefficient = 1.0
    block = 0
  [../]
  [./strain]
    type = ComputeIncrementalBeamStrain
    block = '0'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y rot_z'
    area = 0.5
    Ay = 0.0
    Az = 0.0
    Iy = 0.01
    Iz = 0.01
    y_orientation = '0.0 1.0 0.0'
    eigenstrain_names = 'thermal'
  [../]
  [./stress]
    type = ComputeBeamResultants
    block = 0
  [../]
  [./thermal]
    type = ComputeEigenstrainBeamFromVariable
    displacement_eigenstrain_variables = 'thermal_eig zero1 zero2'
    eigenstrain_name = thermal
  [../]
[]

[Postprocessors]
  [./disp_x]
    type = PointValue
    point = '4.0 0.0 0.0'
    variable = disp_x
  [../]
  [./disp_y]
    type = PointValue
    point = '4.0 0.0 0.0'
    variable = disp_y
  [../]
[]

[Outputs]
  [./out]
    type = Exodus
    hide = 'thermal_eig zero1 zero2'
  [../]
[]

(test/tests/outputs/residual/output_residual_test.i)

[Mesh]
  file = sq-2blk.e
  uniform_refine = 3
[]

[Variables]
  # variable in the whole domain
  [./u]
    order = FIRST
    family = LAGRANGE

    [./InitialCondition]
      type = ConstantIC
      value = 0
    [../]
  [../]

  # subdomain restricted variable
  [./v]
    order = FIRST
    family = LAGRANGE
    block = '1'
  [../]
[]

[Functions]
  [./forcing_fn]
    type = ParsedFunction
    # dudt = 3*t^2*(x^2 + y^2)
    value = 3*t*t*((x*x)+(y*y))-(4*t*t*t)
  [../]

  [./exact_fn]
    type = ParsedFunction
    value = t*t*t*((x*x)+(y*y))
  [../]

  [./exact_fn_v]
    type = ParsedFunction
    value = t+1
  [../]
[]

[Kernels]
  [./ie_u]
    type = TimeDerivative
    variable = u
  [../]

  [./diff_u]
    type = Diffusion
    variable = u
  [../]

  [./ffn_u]
    type = BodyForce
    variable = u
    function = forcing_fn
  [../]


  [./ie_v]
    type = TimeDerivative
    variable = v
  [../]

  [./diff_v]
    type = Diffusion
    variable = v
  [../]

[]

[BCs]
  [./all_u]
    type = FunctionDirichletBC
    variable = u
    boundary = '1 2 3 4'
    function = exact_fn
  [../]

  [./bottom_v]
    type = DirichletBC
    variable = v
    boundary = 5
    value = 0
  [../]

  [./top_v]
    type = FunctionDirichletBC
    variable = v
    boundary = 6
    function = exact_fn_v
  [../]
[]

[Executioner]
  type = Transient
  scheme = 'implicit-euler'

  solve_type = 'PJFNK'

  start_time = 0.0
  num_steps = 5
  dt = 0.1
[]

[Outputs]
  execute_on = 'timestep_end'
  file_base = out
  exodus = true
[]

[Debug]
  show_var_residual = 'u v'
  show_var_residual_norms = true
[]

(test/tests/materials/discrete/reset_warning.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = MatDiffusionTest
    variable = u
    prop_name = 'prop'
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Materials]
  [./mat]
    type = GenericConstantMaterial
    prop_names = 'prop'
    prop_values = 1
    compute = false # testing that this produces warning because resetQpProperties is not re-defined
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/initial_stress/gravity_cosserat.i)

# Apply an initial stress that should be
# exactly that caused by gravity, and then
# do a transient step to check that nothing
# happens
# TODO: currently this has no div(moment_stress)
# contriution to the Kernels.  This is because
# there is no way in MOOSE of calculating
# moment stresses and applying initial stresses.
# This will become possible after issue #7243 is
# resolved.

[Mesh]
  type = GeneratedMesh
  dim = 3
  nx = 1
  ny = 1
  nz = 10
  xmin = -0.5
  xmax = 0.5
  ymin = -0.5
  ymax = 0.5
  zmin = -10
  zmax = 0
[]

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
  Cosserat_rotations = 'wc_x wc_y wc_z'
[]


[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
  [./disp_z]
  [../]
  [./wc_x]
  [../]
  [./wc_y]
  [../]
  [./wc_z]
  [../]
[]

[Kernels]
  [./cx_elastic]
    type = CosseratStressDivergenceTensors
    variable = disp_x
    component = 0
  [../]
  [./cy_elastic]
    type = CosseratStressDivergenceTensors
    variable = disp_y
    component = 1
  [../]
  [./cz_elastic]
    type = CosseratStressDivergenceTensors
    variable = disp_z
    component = 2
  [../]
  [./x_moment]
    type = MomentBalancing
    variable = wc_x
    component = 0
  [../]
  [./y_moment]
    type = MomentBalancing
    variable = wc_y
    component = 1
  [../]
  [./z_moment]
    type = MomentBalancing
    variable = wc_z
    component = 2
  [../]
  [./weight]
    type = BodyForce
    variable = disp_z
    value = -0.5 # this is density*gravity
  [../]
[]


[BCs]
  # back = zmin
  # front = zmax
  # bottom = ymin
  # top = ymax
  # left = xmin
  # right = xmax
  [./x]
    type = DirichletBC
    variable = disp_x
    boundary = 'left right'
    value = 0
  [../]
  [./y]
    type = DirichletBC
    variable = disp_y
    boundary = 'bottom top'
    value = 0
  [../]
  [./z]
    type = DirichletBC
    variable = disp_z
    boundary = 'back'
    value = 0
  [../]
[]

[AuxVariables]
  [./stress_xx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_xy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_xz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_zz]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[AuxKernels]
  [./stress_xx]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xx
    index_i = 0
    index_j = 0
  [../]
  [./stress_xy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xy
    index_i = 0
    index_j = 1
  [../]
  [./stress_xz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xz
    index_i = 0
    index_j = 2
  [../]
  [./stress_yy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yy
    index_i = 1
    index_j = 1
  [../]
  [./stress_yz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yz
    index_i = 1
    index_j = 2
  [../]
  [./stress_zz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zz
    index_i = 2
    index_j = 2
  [../]
[]


[Functions]
  [./weight]
    type = ParsedFunction
    value = '0.5*z' # initial stress that should result from the weight force
  [../]
  [./kxx]
    type = ParsedFunction
    value = '0.4*z' # some arbitrary xx and yy stress that should not affect the result
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeCosseratElasticityTensor
    B_ijkl = '1.1 0.6 0.6' # In Forest notation this is alpha=1.1 (this is unimportant), beta=gamma=0.6.
    fill_method_bending = 'general_isotropic'
    fill_method = symmetric_isotropic
    E_ijkl = '0.4 0.4' # young = 1, poisson = 0.25
  [../]
  [./strain]
    type = ComputeCosseratSmallStrain
    eigenstrain_names = ini_stress
  [../]
  [./ini_stress]
    type = ComputeEigenstrainFromInitialStress
    initial_stress = 'kxx 0 0  0 kxx 0  0 0 weight'
    eigenstrain_name = ini_stress
  [../]
  [./stress]
    type = ComputeCosseratLinearElasticStress
  [../]
[]


[Preconditioning]
  [./andy]
    type = SMP
    full = true
  [../]
[]


[Executioner]
  end_time = 1.0
  dt = 1.0
  solve_type = NEWTON
  type = Transient

  nl_abs_tol = 1E-8
  nl_rel_tol = 1E-12
  l_tol = 1E-3
  l_max_its = 200
  nl_max_its = 400

  petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
  petsc_options_value = ' asm      2              lu            gmres     200'
[]



[Outputs]
  file_base = gravity_cosserat
  exodus = true
[]

(modules/xfem/test/tests/mechanical_constraint/glued_penalty.i)

[GlobalParams]
  displacements = 'disp_x disp_y'
  volumetric_locking_correction = false
[]

[XFEM]
  geometric_cut_userobjects = 'line_seg_cut_uo'
  qrule = volfrac
  output_cut_plane = true
[]

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 11
  ny = 11
  xmin = 0.0
  xmax = 1.0
  ymin = 0.0
  ymax = 1.0
  elem_type = QUAD4
[]

[UserObjects]
  [./line_seg_cut_uo]
    type = LineSegmentCutUserObject
    cut_data = '1.0  0.5  0.0  0.5'
    time_start_cut = 0.0
    time_end_cut = 0.0
  [../]
[]

[Modules/TensorMechanics/Master]
  [./all]
    strain = FINITE
    planar_formulation = plane_strain
    add_variables = true
  [../]
[]

[Functions]
  [./pull]
    type = PiecewiseLinear
    x='0  50   100'
    y='0  0.02 0.1'
  [../]
[]

[BCs]
  [./bottomx]
    type = DirichletBC
    boundary = bottom
    variable = disp_x
    value = 0.0
  [../]
  [./bottomy]
    type = DirichletBC
    boundary = bottom
    variable = disp_y
    value = 0.0
  [../]
  [./topx]
    type = DirichletBC
    boundary = top
    variable = disp_x
    value = 0.0
  [../]
  [./topy]
    type = FunctionDirichletBC
    boundary = top
    variable = disp_y
    function = pull
  [../]
[]

[Constraints]
  [./disp_x]
    type = XFEMSingleVariableConstraint
    variable = disp_x
    use_penalty = true
    alpha = 1.0e8
    use_displaced_mesh = true
    geometric_cut_userobject = 'line_seg_cut_uo'
  [../]
  [./disp_y]
    type = XFEMSingleVariableConstraint
    variable = disp_y
    use_penalty = true
    alpha = 1.0e8
    use_displaced_mesh = true
    geometric_cut_userobject = 'line_seg_cut_uo'
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 1e6
    poissons_ratio = 0.3
    block = 0
  [../]

  [./_elastic_strain]
    type = ComputeFiniteStrainElasticStress
    block = 0
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'
  petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
  petsc_options_value = '201                hypre    boomeramg      8'

  line_search = 'none'

  [./Predictor]
    type = SimplePredictor
    scale = 1.0
  [../]

# controls for linear iterations
  l_max_its = 100
  l_tol = 1e-2

# controls for nonlinear iterations
  nl_max_its = 15
  nl_rel_tol = 1e-14
  nl_abs_tol = 1e-9

# time control
  start_time = 0.0
  dt = 1.0
  end_time = 2.0
  num_steps = 5000

  max_xfem_update = 1
[]

[Outputs]
  exodus = true
  execute_on = timestep_end
  [./console]
    type = Console
    output_linear = true
  [../]
[]

(test/tests/multiapps/cliargs_from_file/cliargs_master_inline.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 10
  dt = 1 # This will be constrained by the multiapp

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

[MultiApps]
  [./sub_app]
    positions = '0 0 0  0.5 0.5 0
                 0.6 0.6 0  0.7 0.7 0'
    cli_args_files = cliargs.txt
    type = TransientMultiApp
    input_files = 'cliargs_sub.i'
    app_type = MooseTestApp
  [../]
[]

(modules/combined/test/tests/beam_eigenstrain_transfer/subapp_err_2.i)

# SubApp with 2D model to test multi app vectorpostprocessor to aux var transfer

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 5
  xmin = 0.0
  xmax = 0.5
  ymin = 0.0
  ymax = 0.150080
[]

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[AuxVariables]
  [./temp]
  [../]
  [./axial_strain]
    order = FIRST
    family = MONOMIAL
  [../]
[]

[Functions]
  [./temperature_load]
    type = ParsedFunction
    value = t*(500.0)+300.0
  [../]
[]

[Modules]
  [./TensorMechanics]
    [./Master]
      [./all]
        strain = SMALL
        incremental = true
        add_variables = true
        eigenstrain_names = eigenstrain
      [../]
    [../]
  [../]
[]

[AuxKernels]
  [./tempfuncaux]
    type = FunctionAux
    variable = temp
    function = temperature_load
  [../]
  [./axial_strain]
    type = RankTwoAux
    variable = axial_strain
    rank_two_tensor = total_strain
    index_i = 1
    index_j = 1
    execute_on = timestep_end
  [../]
[]

[BCs]
  [./x_bot]
    type = DirichletBC
    variable = disp_x
    boundary = left
    value = 0.0
  [../]
  [./y_bot]
    type = DirichletBC
    variable = disp_y
    boundary = bottom
    value = 0.0
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 2.1e5
    poissons_ratio = 0.3
  [../]
  [./small_stress]
    type = ComputeFiniteStrainElasticStress
  [../]
  [./thermal_expansion_strain]
    type = ComputeThermalExpansionEigenstrain
    stress_free_temperature = 298
    thermal_expansion_coeff = 1.3e-5
    temperature = temp
    eigenstrain_name = eigenstrain
  [../]
[]

[Executioner]
  type = Transient

  #Preconditioned JFNK (default)
  solve_type = 'PJFNK'

  petsc_options = '-snes_ksp_ew'
  petsc_options_iname = '-ksp_gmres_restart'
  petsc_options_value = '101'

  line_search = 'none'

  l_max_its = 50
  nl_max_its = 50
  nl_rel_tol = 1e-8
  nl_abs_tol = 1e-8
  l_tol = 1e-9

  start_time = 0.0
  end_time = 0.075
  dt = 0.0125
  dtmin = 0.0001
[]

[Outputs]
  csv = true
  exodus = true
[]

[VectorPostprocessors]
  [./axial_str]
    type = LineValueSampler
    warn_discontinuous_face_values = false
    start_point = '0.5 0.0 0.0'
    end_point = '0.5 0.150080 0.0'
    variable = 'axial_strain temp'
    num_points = 21
    sort_by = 'y'
  [../]
[]

[Postprocessors]
  [./end_disp]
    type = PointValue
    variable = disp_y
    point = '0.5 0.150080 0.0'
  [../]
[]

(modules/tensor_mechanics/test/tests/crystal_plasticity/monolithic_material_based/cp_slip_rate_integ/crysp_substep.i)

[Mesh]
  type = GeneratedMesh
  dim = 3
  elem_type = HEX8
  displacements = 'disp_x disp_y disp_z'
[]

[Variables]
  [./disp_x]
    block = 0
  [../]
  [./disp_y]
    block = 0
  [../]
  [./disp_z]
    block = 0
  [../]
[]

[AuxVariables]
  [./stress_zz]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
  [./fp_zz]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
  [./e_zz]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
  [./gss1]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
[]

[Functions]
  [./tdisp]
    type = ParsedFunction
    value = 0.01*t
  [../]
[]

[Kernels]
  [./TensorMechanics]
    displacements = 'disp_x disp_y disp_z'
    use_displaced_mesh = true
  [../]
[]

[AuxKernels]
  [./stress_zz]
    type = RankTwoAux
    variable = stress_zz
    rank_two_tensor = stress
    index_j = 2
    index_i = 2
    execute_on = timestep_end
    block = 0
  [../]
  [./fp_zz]
    type = RankTwoAux
    variable = fp_zz
    rank_two_tensor = fp
    index_j = 2
    index_i = 2
    execute_on = timestep_end
    block = 0
  [../]
  [./e_zz]
    type = RankTwoAux
    variable = e_zz
    rank_two_tensor = lage
    index_j = 2
    index_i = 2
    execute_on = timestep_end
    block = 0
  [../]
  [./gss1]
    type = MaterialStdVectorAux
    variable = gss1
    property = gss
    index = 0
    execute_on = timestep_end
    block = 0
  [../]
[]

[BCs]
  [./symmy]
    type = DirichletBC
    variable = disp_y
    boundary = bottom
    value = 0
  [../]
  [./symmx]
    type = DirichletBC
    variable = disp_x
    boundary = left
    value = 0
  [../]
  [./symmz]
    type = DirichletBC
    variable = disp_z
    boundary = back
    value = 0
  [../]
  [./tdisp]
    type = FunctionDirichletBC
    variable = disp_z
    boundary = front
    function = tdisp
  [../]
[]

[Materials]
  [./crysp]
    type = FiniteStrainCPSlipRateRes
    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 0.01 5 8 0.001 0.01 9 12 0.001 0.01'
    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
    slip_incr_tol = 1
    maximum_substep_iteration = 8
  [../]
  [./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
  [../]
  [./strain]
    type = ComputeFiniteStrain
    block = 0
    displacements = 'disp_x disp_y disp_z'
  [../]
[]

[Postprocessors]
  [./stress_zz]
    type = ElementAverageValue
    variable = stress_zz
    block = 'ANY_BLOCK_ID 0'
  [../]
  [./fp_zz]
    type = ElementAverageValue
    variable = fp_zz
    block = 'ANY_BLOCK_ID 0'
  [../]
  [./e_zz]
    type = ElementAverageValue
    variable = e_zz
    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 = 0.2
  dtmax = 10.0
  dtmin = 0.05

  end_time = 1
[]

[Outputs]
  file_base = crysp_substep_out
  exodus = true
  print_linear_residuals = true
  perf_graph = true
[]

(modules/tensor_mechanics/test/tests/action/ad_converter_action_multi_eigenstrain.i)

# This tests the thermal expansion coefficient function using both
# options to specify that function: mean and instantaneous.  There
# two blocks, each containing a single element, and these use the
# two variants of the function.

# In this test, the instantaneous CTE function has a constant value,
# while the mean CTE function is an analytic function designed to
# give the same response.  If \bar{alpha}(T) is the mean CTE function,
# and \alpha(T) is the instantaneous CTE function,

# \bar{\alpha}(T) = 1/(T-Tref) \intA^{T}_{Tsf} \alpha(T) dT

# where Tref is the reference temperature used to define the mean CTE
# function, and Tsf is the stress-free temperature.

# This version of the test uses finite deformation theory.
# The two models produce very similar results.  There are slight
# differences due to the large deformation treatment.

[Mesh]
  file = 'blocks.e'
[]

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
[]

[AuxVariables]
  [./temp]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Problem]
  solve = false
[]

[Modules/TensorMechanics/Master]
  [./block1]
    block = 1
    strain = FINITE
    add_variables = true
    automatic_eigenstrain_names = true
    generate_output = 'strain_xx strain_yy strain_zz'
    use_automatic_differentiation = true
  [../]
  [./block2]
    block = 2
    strain = FINITE
    add_variables = true
    automatic_eigenstrain_names = true
    generate_output = 'strain_xx strain_yy strain_zz'
    use_automatic_differentiation = true
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = disp_x
    boundary = 3
    value = 0.0
  [../]

  [./bottom]
    type = DirichletBC
    variable = disp_y
    boundary = 2
    value = 0.0
  [../]

  [./back]
    type = DirichletBC
    variable = disp_z
    boundary = 1
    value = 0.0
  [../]
[]

[AuxKernels]
  [./temp]
    type = FunctionAux
    variable = temp
    block = '1 2'
    function = temp_func
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ADComputeIsotropicElasticityTensor
    youngs_modulus = 1e6
    poissons_ratio = 0.3
  [../]
  [./small_stress]
    type = ADComputeFiniteStrainElasticStress
  [../]
  [./thermal_expansion_strain1]
    type = ComputeMeanThermalExpansionFunctionEigenstrain
    block = 1
    thermal_expansion_function = cte_func_mean
    thermal_expansion_function_reference_temperature = 0.5
    stress_free_temperature = 0.0
    temperature = temp
    eigenstrain_name = reg_eigenstrain1
  [../]
  [./converter1]
    type = RankTwoTensorMaterialADConverter
    block = 1
    reg_props_in = 'reg_eigenstrain1'
    ad_props_out = 'eigenstrain1'

  [../]
  [./thermal_expansion_strain2]
    type = ADComputeInstantaneousThermalExpansionFunctionEigenstrain
    block = 2
    thermal_expansion_function = cte_func_inst
    stress_free_temperature = 0.0
    temperature = temp
    eigenstrain_name = eigenstrain2
  [../]
[]

[Functions]
  [./cte_func_mean]
    type = ParsedFunction
    vars = 'tsf tref scale' #stress free temp, reference temp, scale factor
    vals = '0.0 0.5  1e-4'
    value = 'scale * (t - tsf) / (t - tref)'
  [../]
  [./cte_func_inst]
    type = PiecewiseLinear
    xy_data = '0 1.0
               2 1.0'
    scale_factor = 1e-4
  [../]

  [./temp_func]
    type = PiecewiseLinear
    xy_data = '0 1
               1 2'
  [../]
[]

[Postprocessors]
  [./disp_1]
    type = NodalExtremeValue
    variable = disp_x
    boundary = 101
  [../]

  [./disp_2]
    type = NodalExtremeValue
    variable = disp_x
    boundary = 102
  [../]
[]

[Executioner]
  type = Transient

  solve_type = PJFNK
  l_max_its = 100
  l_tol = 1e-4
  nl_abs_tol = 1e-8
  nl_rel_tol = 1e-12

  start_time = 0.0
  end_time = 1.0
  dt = 0.1
[]

[Outputs]
  csv = true
[]

(modules/tensor_mechanics/test/tests/ad_elastic/rspherical_incremental_small_elastic-noad.i)

[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 5
[]

[Problem]
  coord_type = RSPHERICAL
[]

[GlobalParams]
  displacements = 'disp_r'
[]

[Variables]
  # scale with one over Young's modulus
  [./disp_r]
    scaling = 1e-10
  [../]
[]

[Kernels]
  [./stress_r]
    type = StressDivergenceRSphericalTensors
    component = 0
    variable = disp_r
  [../]
[]

[BCs]
  [./center]
    type = DirichletBC
    variable = disp_r
    boundary = left
    value = 0
  [../]
  [./rdisp]
    type = DirichletBC
    variable = disp_r
    boundary = right
    value = 0.1
  [../]
[]

[Materials]
  [./elasticity]
    type = ComputeIsotropicElasticityTensor
    poissons_ratio = 0.3
    youngs_modulus = 1e10
  [../]
  [./strain]
    type = ComputeRSphericalIncrementalStrain
  [../]
  [./stress]
    type = ComputeFiniteStrainElasticStress
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient
  dt = 0.05
  solve_type = 'NEWTON'

  petsc_options_iname = -pc_hypre_type
  petsc_options_value = boomeramg

  dtmin = 0.05
  num_steps = 1
  nl_max_its = 200
[]

[Outputs]
  exodus = true
  file_base = rspherical_incremental_small_elastic_out
[]

(test/tests/vectorpostprocessors/point_value_sampler_history/point_value_sampler_history.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  [../]
  [./time]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[VectorPostprocessors]
  [./point_sample]
    type = PointValueSampler
    variable = 'u'
    points = '0.1 0.1 0'
    sort_by = x

    contains_complete_history = true
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 10
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  csv = true
[]

(modules/porous_flow/test/tests/heat_advection/heat_advection_1d_KT.i)

# 1phase, heat advecting with a moving fluid
# Using the Kuzmin-Turek stabilization scheme
[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 50
  xmin = 0
  xmax = 1
[]

[GlobalParams]
  PorousFlowDictator = dictator
  gravity = '0 0 0'
[]

[Variables]
  [temp]
    initial_condition = 200
  []
  [pp]
  []
[]

[ICs]
  [pp]
    type = FunctionIC
    variable = pp
    function = '1-x'
  []
[]

[BCs]
  [pp0]
    type = DirichletBC
    variable = pp
    boundary = left
    value = 1
  []
  [pp1]
    type = DirichletBC
    variable = pp
    boundary = right
    value = 0
  []
  [spit_heat]
    type = DirichletBC
    variable = temp
    boundary = left
    value = 300
  []
  [suck_heat]
    type = DirichletBC
    variable = temp
    boundary = right
    value = 200
  []
[]

[Kernels]
  [mass_dot]
    type = PorousFlowMassTimeDerivative
    fluid_component = 0
    variable = pp
  []
  [fluid_advection]
    type = PorousFlowFluxLimitedTVDAdvection
    variable = pp
    advective_flux_calculator = fluid_advective_flux
  []
  [energy_dot]
    type = PorousFlowEnergyTimeDerivative
    variable = temp
  []
  [heat_advection]
    type = PorousFlowFluxLimitedTVDAdvection
    variable = temp
    advective_flux_calculator = heat_advective_flux
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'temp pp'
    number_fluid_phases = 1
    number_fluid_components = 1
  []
  [pc]
    type = PorousFlowCapillaryPressureVG
    m = 0.6
    alpha = 1.3
  []
  [fluid_advective_flux]
    type = PorousFlowAdvectiveFluxCalculatorSaturated
    flux_limiter_type = superbee
  []
  [heat_advective_flux]
    type = PorousFlowAdvectiveFluxCalculatorSaturatedHeat
    flux_limiter_type = superbee
  []
[]

[Modules]
  [FluidProperties]
    [simple_fluid]
      type = SimpleFluidProperties
      bulk_modulus = 100
      density0 = 1000
      viscosity = 4.4
      thermal_expansion = 0
      cv = 2
    []
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
    temperature = temp
  []
  [porosity]
    type = PorousFlowPorosityConst
    porosity = 0.2
  []
  [rock_heat]
    type = PorousFlowMatrixInternalEnergy
    specific_heat_capacity = 1.0
    density = 125
  []
  [simple_fluid]
    type = PorousFlowSingleComponentFluid
    fp = simple_fluid
    phase = 0
  []
  [permeability]
    type = PorousFlowPermeabilityConst
    permeability = '1.1 0 0 0 2 0 0 0 3'
  []
  [relperm]
    type = PorousFlowRelativePermeabilityCorey
    n = 2
    phase = 0
  []
  [massfrac]
    type = PorousFlowMassFraction
  []
  [PS]
    type = PorousFlow1PhaseP
    porepressure = pp
    capillary_pressure = pc
  []
[]

[Preconditioning]
  [andy]
    type = SMP
    full = true
    petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
    petsc_options_value = 'gmres bjacobi 1E-15 1E-10 10000'
  []
[]

[Executioner]
  type = Transient
  solve_type = Newton
  dt = 0.01
  end_time = 0.6
[]

[VectorPostprocessors]
  [T]
    type = LineValueSampler
    start_point = '0 0 0'
    end_point = '1 0 0'
    num_points = 51
    sort_by = x
    variable = temp
  []
[]

[Outputs]
  file_base = heat_advection_1d_KT
  [csv]
    type = CSV
    sync_times = '0.1 0.6'
    sync_only = true
  []
[]

(test/tests/userobjects/Terminator/terminator_pass.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 30
  ny = 6
  xmin = -15.0
  xmax = 15.0
  ymin = -3.0
  ymax = 3.0
  elem_type = QUAD4
[]

[Variables]
  [c]
    order = FIRST
    family = LAGRANGE
    initial_condition = 1
  []
[]

[Postprocessors]
  [dt]
    type = TimestepSize
  []
[]

[UserObjects]
  [arnold]
    type = Terminator
    expression = 'dt > 20'
    fail_mode = HARD
    error_level = INFO
    message = 'Arnold says this should end'
    execute_on = TIMESTEP_END
  []
[]

[Kernels]
  [cres]
    type = Diffusion
    variable = c
  []

  [time]
    type = TimeDerivative
    variable = c
  []
[]

[BCs]
  [c]
    type = DirichletBC
    variable = c
    boundary = left
    value = 0
  []
[]

[Executioner]
  type = Transient
  [TimeStepper]
    type = IterationAdaptiveDT
    dt = 4
  []
  nl_abs_step_tol = 1e-10
[]

[Outputs]
  csv = true
  print_linear_residuals = false
[]

(test/tests/ics/check_error/two_ics_on_same_boundary.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[ICs]
  [./left]
    type = ConstantIC
    variable = u
    boundary = left
    value = 0.5
  [../]
  [./left2]
    type = ConstantIC
    variable = u
    boundary = left
    value = 2
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Steady
[]

[Outputs]
[]

(modules/contact/test/tests/mechanical_constraint/glued_kinematic.i)

[Mesh]
  file = blocks_2d_nogap.e
[]

[GlobalParams]
  volumetric_locking_correction = false
  displacements = 'disp_x disp_y'
[]

[AuxVariables]
  [./penetration]
  [../]
  [./inc_slip_x]
  [../]
  [./inc_slip_y]
  [../]
  [./accum_slip_x]
  [../]
  [./accum_slip_y]
  [../]
[]

[Functions]
  [./vertical_movement]
    type = ParsedFunction
    value = -t
  [../]
[]

[Modules/TensorMechanics/Master]
  [./all]
    add_variables = true
    strain = FINITE
  [../]
[]

[AuxKernels]
  [./zeroslip_x]
    type = ConstantAux
    variable = inc_slip_x
    boundary = 3
    execute_on = timestep_begin
    value = 0.0
  [../]
  [./zeroslip_y]
    type = ConstantAux
    variable = inc_slip_y
    boundary = 3
    execute_on = timestep_begin
    value = 0.0
  [../]
  [./accum_slip_x]
    type = AccumulateAux
    variable = accum_slip_x
    accumulate_from_variable = inc_slip_x
    execute_on = timestep_end
  [../]
  [./accum_slip_y]
    type = AccumulateAux
    variable = accum_slip_y
    accumulate_from_variable = inc_slip_y
    execute_on = timestep_end
  [../]
  [./penetration]
    type = PenetrationAux
    variable = penetration
    boundary = 3
    paired_boundary = 2
  [../]
[]

[BCs]
  [./left_x]
    type = DirichletBC
    variable = disp_x
    boundary = 1
    value = 0.0
  [../]
  [./left_y]
    type = DirichletBC
    variable = disp_y
    boundary = 1
    value = 0.0
  [../]
  [./right_x]
    type = DirichletBC
    variable = disp_x
    boundary = 4
    #Initial gap is 0.01
    value = -0.01
  [../]
  [./right_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 4
    function = vertical_movement
  [../]
[]

[Materials]
  [./left]
    type = ComputeIsotropicElasticityTensor
    block = '1'
    youngs_modulus = 1e7
    poissons_ratio = 0.3
  [../]
  [./right]
    type = ComputeIsotropicElasticityTensor
    block = '2'
    youngs_modulus = 1e6
    poissons_ratio = 0.3
  [../]
  [./stress]
    type = ComputeFiniteStrainElasticStress
    block = '1 2'
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'

  line_search = 'none'

  l_max_its = 100
  nl_max_its = 1000
  dt = 0.01
  end_time = 0.10
  num_steps = 1000
  l_tol = 1e-6
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-8
  dtmin = 0.01

  [./Predictor]
    type = SimplePredictor
    scale = 1.0
  [../]
[]

[Outputs]
  [./out]
    type = Exodus
    elemental_as_nodal = true
  [../]
  [./console]
    type = Console
    max_rows = 5
  [../]
[]

[Contact]
  [./leftright]
    primary = 2
    secondary = 3
    model = glued
    penalty = 1e+6
  [../]
[]

(test/tests/meshgenerators/gmsh_bcs/gmsh_bcs.i)

[Mesh]
  [./fmg]
    type = FileMeshGenerator
    file = plate_hole.msh
  []
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = 12
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = 10
    value = 1
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  execute_on = 'timestep_end'
  exodus = true
[]

(test/tests/restart/restart_diffusion/restart_diffusion_test_transient.i)

[Mesh]
  file = steady_out.e
[]

[Variables]
  [./u]
    order = FIRST
    family = LAGRANGE
    initial_from_file_var = u
    initial_from_file_timestep = 2
  [../]
[]

[Kernels]
  active = 'bodyforce ie'

  [./bodyforce]
    type = BodyForce
    variable = u
    value = 10.0
  [../]

  [./ie]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = 3
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 1
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'

  start_time = 0.0
  num_steps = 10
  dt = .1
[]

[Outputs]
  file_base = out
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_element/ins/lid_driven/lid_driven_chorin.i)

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 1.0
    ymin = 0
    ymax = 1.0
    nx = 40
    ny = 40
    elem_type = QUAD4
  []
  [./corner_node]
    type = ExtraNodesetGenerator
    new_boundary = 99
    nodes = '0'
    input = gen
  [../]
[]

[Variables]
  # x-velocity
  [./u]
    order = FIRST
    family = LAGRANGE

    [./InitialCondition]
      type = ConstantIC
      value = 0.0
    [../]
  [../]

  # y-velocity
  [./v]
    order = FIRST
    family = LAGRANGE

    [./InitialCondition]
      type = ConstantIC
      value = 0.0
    [../]
  [../]

  # x-star velocity
  [./u_star]
    order = FIRST
    family = LAGRANGE

    [./InitialCondition]
      type = ConstantIC
      value = 0.0
    [../]
  [../]

  # y-star velocity
  [./v_star]
    order = FIRST
    family = LAGRANGE

    [./InitialCondition]
      type = ConstantIC
      value = 0.0
    [../]
  [../]

  # Pressure
  [./p]
    order = FIRST
    family = LAGRANGE

    [./InitialCondition]
      type = ConstantIC
      value = 0
    [../]
  [../]
[]



[Kernels]
  [./x_chorin_predictor]
    type = INSChorinPredictor
    variable = u_star
    u = u
    v = v
    u_star = u_star
    v_star = v_star
    component = 0
    predictor_type = 'new'
  [../]

  [./y_chorin_predictor]
    type = INSChorinPredictor
    variable = v_star
    u = u
    v = v
    u_star = u_star
    v_star = v_star
    component = 1
    predictor_type = 'new'
  [../]

  [./x_chorin_corrector]
    type = INSChorinCorrector
    variable = u
    u_star = u_star
    v_star = v_star
    pressure = p
    component = 0
  [../]

  [./y_chorin_corrector]
    type = INSChorinCorrector
    variable = v
    u_star = u_star
    v_star = v_star
    pressure = p
    component = 1
  [../]

  [./chorin_pressure_poisson]
    type = INSChorinPressurePoisson
    variable = p
    u_star = u_star
    v_star = v_star
  [../]
[]

[BCs]
  [./u_no_slip]
    type = DirichletBC
    variable = u
    preset = false
    boundary = 'bottom right left'
    value = 0.0
  [../]

  [./u_lid]
    type = DirichletBC
    variable = u
    preset = false
    boundary = 'top'
    value = 100.0
  [../]

  [./v_no_slip]
    type = DirichletBC
    variable = v
    preset = false
    boundary = 'bottom right top left'
    value = 0.0
  [../]

  # Make u_star satsify all the same variables as the real velocity.
  [./u_star_no_slip]
    type = DirichletBC
    variable = u_star
    preset = false
    boundary = 'bottom right left'
    value = 0.0
  [../]

  [./u_star_lid]
    type = DirichletBC
    variable = u_star
    preset = false
    boundary = 'top'
    value = 100.0
  [../]

  [./v_star_no_slip]
    type = DirichletBC
    variable = v_star
    preset = false
    boundary = 'bottom right top left'
    value = 0.0
  [../]

  # With solid walls everywhere, we specify dp/dn=0, i.e the
  # "natural BC" for pressure.  Technically the problem still
  # solves without pinning the pressure somewhere, but the pressure
  # bounces around a lot during the solve, possibly because of
  # the addition of arbitrary constants.
  [./pressure_pin]
    type = DirichletBC
    variable = p
    preset = false
    boundary = '99'
    value = 0
  [../]
[]

[Materials]
  [./const]
    type = GenericConstantMaterial
    block = 0
    # rho = 1000    # kg/m^3
    # mu = 0.798e-3 # Pa-s at 30C
    # cp = 4.179e3  # J/kg-K at 30C
    # k = 0.58      # W/m-K at ?C

    # Dummy parameters
    prop_names = 'rho mu cp k'
    prop_values = '1  1  1  1'
  [../]
[]

[Preconditioning]
#active = 'FDP_Newton'
#active = 'SMP_PJFNK'
active = 'SMP_Newton'

[./FDP_Newton]
type = FDP
full = true

solve_type = 'NEWTON'

#petsc_options_iname = '-mat_fd_coloring_err'
#petsc_options_value = '1.e-10'
[../]

# For some reason, nonlinear convergence with JFNK is poor, but it
# seems to be OK for SMP_Newton.  This may indicate a a scaling issue
# in the JFNK case....
[./SMP_PJFNK]
  type = SMP
  full = true

  #Preconditioned JFNK (default)
  solve_type = 'PJFNK'


[../]

[./SMP_Newton]
  type = SMP
  full = true

  solve_type = 'NEWTON'

[../]
[]


[Executioner]
  type = Transient
  # Note: the explicit case with lid velocity = 100 and a 40x40 was unstable
  # for dt=1.e-4, even though the restriction should be dt < dx/|u| = 1/4000 = 2.5e-4
  #
  dt = 1.e-3
  dtmin = 1.e-6
  petsc_options_iname = '-ksp_gmres_restart '
  petsc_options_value = '300                '

  line_search = 'none'

  nl_rel_tol = 1e-12
  nl_max_its = 6
  l_max_its = 300
  start_time = 0.0
  num_steps = 5

  automatic_scaling = true
  verbose = true
  compute_scaling_once = false
[]

[Debug]
  show_var_residual_norms = true
[]

[Outputs]
  file_base = lid_driven_chorin_out
  exodus = true
[]

(test/tests/transfers/multiapp_conservative_transfer/master_nearest_point.i)

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    xmax = 1
    ymax = 1
    nx = 10
    ny = 10
  []
  [block1]
    input = gen
    type = SubdomainBoundingBoxGenerator
    block_id = 1
    bottom_left = '0.5 0 0'
    top_right = '1 1 0'
  []
[]

[Variables]
  [power_density]
  []
[]

[Functions]
  [pwr_func]
    type = ParsedFunction
    value = '1e3*x*(1-x)+5e2'
  []
[]

[Kernels]
  [diff]
    type = Diffusion
    variable = power_density
  []

  [coupledforce]
    type = BodyForce
    variable = power_density
    function = pwr_func
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = power_density
    boundary = left
    value = 0
  []
  [right]
    type = DirichletBC
    variable = power_density
    boundary = right
    value = 1e3
  []
[]

[AuxVariables]
  [from_sub]
  []
[]

[VectorPostprocessors]
  [from_nearest_point]
    type = NearestPointIntegralVariablePostprocessor
    variable = power_density
    points = '0 0.5 0 1 0.5 0'
  []

  [to_nearest_point]
    type = NearestPointIntegralVariablePostprocessor
    variable = from_sub
    points = '0 0.5 0 1 0.5 0'
    execute_on = 'transfer'
  []
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[MultiApps]
  [sub]
    type = FullSolveMultiApp
    input_files = sub_nearest_point.i
    positions = '0 0 0 0.5 0 0'
    execute_on = timestep_end
  []
[]

[Transfers]
  [to_sub]
    type = MultiAppMeshFunctionTransfer
    source_variable = power_density
    variable = from_master
    to_multi_app = sub
    execute_on = timestep_end

    # The following inputs specify what postprocessors should be conserved
    # 1 NearestPointIntegralVariablePostprocessor is specified on the master
    # side with N points, where N is the number of subapps
    # 1 pp is specified on the subapp side
    from_postprocessors_to_be_preserved = 'from_nearest_point'
    to_postprocessors_to_be_preserved = 'from_master_pp'
  []

  [from_sub]
    type = MultiAppMeshFunctionTransfer
    source_variable = sink
    variable = from_sub
    from_multi_app = sub
    execute_on = timestep_end

    # The following inputs specify what postprocessors should be conserved
    # 1 NearestPointIntegralVariablePostprocessor is specified on the master
    # with N points, where N is the number of subapps
    # 1 pp is specified on the subapp side
    to_postprocessors_to_be_preserved = 'to_nearest_point'
    from_postprocessors_to_be_preserved = 'sink'
  []
[]

[Outputs]
  csv = true
  exodus = true
[]

(modules/thermal_hydraulics/test/tests/misc/count_iterations/count_iterations.i)

# This tests the "Debug/count_iterations" parameter, which creates
# post-processors for numbers of linear and nonlinear iterations. A dummy
# diffusion solve is performed, and the numbers of iterations are stored in a
# CSV file.

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [u]
  []
[]

[Kernels]
  [time_derivative]
    type = TimeDerivative
    variable = u
  []
  [diff]
    type = Diffusion
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  []
  [right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  []
[]

[Problem]
  type = FEProblem
  coord_type = RZ
  rz_coord_axis = X
[]

[Executioner]
  type = Transient
  scheme = implicit-euler

  [TimeStepper]
    type = ConstantDT
    dt = 0.01
  []

  start_time = 0.0
  num_steps = 2
  abort_on_solve_fail = true

  solve_type = 'NEWTON'
  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'
[]

[Outputs]
  csv = true
[]

[Debug]
  count_iterations = true
[]

(modules/contact/test/tests/mortar_tm/2drz/ad_frictionless_first/small.i)

E_block = 1e7
E_plank = 1e7
elem = QUAD4
order = FIRST
name = 'small'

[Problem]
  coord_type = RZ
[]

[Mesh]
  patch_size = 80
  patch_update_strategy = auto
  [plank]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0
    xmax = 0.6
    ymin = -10
    ymax = 10
    nx = 2
    ny = 67
    elem_type = ${elem}
    boundary_name_prefix = plank
  []
  [plank_id]
    type = SubdomainIDGenerator
    input = plank
    subdomain_id = 1
  []

  [block]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0.61
    xmax = 1.21
    ymin = 9.2
    ymax = 10.0
    nx = 3
    ny = 4
    elem_type = ${elem}
    boundary_name_prefix = block
    boundary_id_offset = 10
  []
  [block_id]
    type = SubdomainIDGenerator
    input = block
    subdomain_id = 2
  []

  [combined]
    type = MeshCollectionGenerator
    inputs = 'plank_id block_id'
  []
  [block_rename]
    type = RenameBlockGenerator
    input = combined
    old_block = '1 2'
    new_block = 'plank block'
  []
[]

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Variables]
  [disp_x]
    order = ${order}
    block = 'plank block'
    scaling = '${fparse 2.0 / (E_plank + E_block)}'
  []
  [disp_y]
    order = ${order}
    block = 'plank block'
    scaling = '${fparse 2.0 / (E_plank + E_block)}'
  []
[]

[Modules/TensorMechanics/Master]
  [block]
    use_automatic_differentiation = true
    generate_output = 'stress_xx stress_yy stress_zz vonmises_stress hydrostatic_stress strain_xx '
                      'strain_yy strain_zz'
    block = 'block'
  []
  [plank]
    use_automatic_differentiation = true
    generate_output = 'stress_xx stress_yy stress_zz vonmises_stress hydrostatic_stress strain_xx '
                      'strain_yy strain_zz'
    block = 'plank'
    eigenstrain_names = 'swell'
  []
[]

[Contact]
  [frictionless]
    primary = plank_right
    secondary = block_left
    formulation = mortar
    c_normal = 1e0
  []
[]

[BCs]
  [left_x]
    type = DirichletBC
    variable = disp_x
    boundary = plank_left
    value = 0.0
  []
  [left_y]
    type = DirichletBC
    variable = disp_y
    boundary = plank_bottom
    value = 0.0
  []
  [right_x]
    type = DirichletBC
    variable = disp_x
    boundary = block_right
    value = 0
  []
  [right_y]
    type = ADFunctionDirichletBC
    variable = disp_y
    boundary = block_right
    function = '-t'
  []
[]

[Materials]
  [plank]
    type = ADComputeIsotropicElasticityTensor
    block = 'plank'
    poissons_ratio = 0.3
    youngs_modulus = ${E_plank}
  []
  [block]
    type = ADComputeIsotropicElasticityTensor
    block = 'block'
    poissons_ratio = 0.3
    youngs_modulus = ${E_block}
  []
  [stress]
    type = ADComputeLinearElasticStress
    block = 'plank block'
  []
  [swell]
    type = ADComputeEigenstrain
    block = 'plank'
    eigenstrain_name = swell
    eigen_base = '1 0 0 0 0 0 0 0 0'
    prefactor = swell_mat
  []
  [swell_mat]
    type = ADGenericFunctionMaterial
    prop_names = 'swell_mat'
    prop_values = '7e-2*(1-cos(4*t))'
    block = 'plank'
  []
[]

[Executioner]
  type = Transient
  solve_type = 'NEWTON'
  petsc_options = '-snes_converged_reason -ksp_converged_reason'
  petsc_options_iname = '-pc_type -mat_mffd_err -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = 'lu       1e-5          NONZERO               1e-15'
  end_time = 10
  dt = 0.1
  dtmin = 0.1
  timestep_tolerance = 1e-6
  line_search = 'contact'
[]

[Postprocessors]
  [nl_its]
    type = NumNonlinearIterations
  []
  [total_nl_its]
    type = CumulativeValuePostprocessor
    postprocessor = nl_its
  []
  [l_its]
    type = NumLinearIterations
  []
  [total_l_its]
    type = CumulativeValuePostprocessor
    postprocessor = l_its
  []
  [contact]
    type = ContactDOFSetSize
    variable = frictionless_normal_lm
    subdomain = frictionless_secondary_subdomain
  []
  [avg_hydro]
    type = ElementAverageValue
    variable = hydrostatic_stress
    block = 'block'
  []
  [max_hydro]
    type = ElementExtremeValue
    variable = hydrostatic_stress
    block = 'block'
  []
  [min_hydro]
    type = ElementExtremeValue
    variable = hydrostatic_stress
    block = 'block'
    value_type = min
  []
  [avg_vonmises]
    type = ElementAverageValue
    variable = vonmises_stress
    block = 'block'
  []
  [max_vonmises]
    type = ElementExtremeValue
    variable = vonmises_stress
    block = 'block'
  []
  [min_vonmises]
    type = ElementExtremeValue
    variable = vonmises_stress
    block = 'block'
    value_type = min
  []
[]

[Outputs]
  exodus = true
  file_base = ${name}
  [comp]
    type = CSV
    show = 'contact'
  []
  [out]
    type = CSV
    file_base = '${name}_out'
  []
[]

[Debug]
  show_var_residual_norms = true
[]

(modules/porous_flow/test/tests/mass_conservation/mass13.i)

# The sample is an annulus in RZ coordinates.
# Roller BCs are applied to the rmin, top and bottom boundaries
# A constant displacement is applied to the outer boundary: disp_r = -0.01 * t * (r - rmin)/(rmax - rmin).
# There is no fluid flow.
# Fluid mass conservation is checked.
#
# The flag volumetric_locking_correction = true is set for the strain calculator,
# which ensures that the volumetric strain is uniform throughout the element
#
# Theoretically,
# volumetric_strain = volume / volume0 - 1 = ((rmax - 0.01*t)^2 - rmin^2) / (rmax^2 - rmin^2) - 1
# However, with ComputeAxisymmetricRZSmallStrain, strain_rr = -0.01 * t / (rmax - rmin)
# and strain_tt = disp_r / r = -0.01 * t * (1 - rmin / r_qp) / (rmax - rmin), where r_qp is the radius of the quadpoint
# With volumetric_locking_correction = true, r_qp = (rmax - rmin) / 2.
# The volumetric strain is
# epv = -0.01 * t * (2 - rmin / r_qp) / (rmax - rmin)
# and volume = volume0 * (1 + epv)
#
# Fluid conservation reads
# volume0 * rho0 * exp(P0/bulk) = volume * rho0 * exp(P/bulk), so
# P - P0 = bulk * log(volume0 / volume) = 0.5 * log(1 / (1 + epv))

# With rmax = 2 and rmin = 1
# fluid_mass = volume0 * rho0 * exp(P0/bulk) = pi*3 * 1 * exp(0.1/0.5) = 11.51145


[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 1
  ny = 1
  xmin = 1
  xmax = 2
  ymin = -0.5
  ymax = 0.5
[]

[Problem]
  coord_type = RZ
[]

[GlobalParams]
  displacements = 'disp_r disp_z'
  PorousFlowDictator = dictator
  block = 0
  biot_coefficient = 0.3
[]

[Variables]
  [disp_r]
  []
  [disp_z]
  []
  [porepressure]
    initial_condition = 0.1
  []
[]

[BCs]
  [plane_strain]
    type = DirichletBC
    variable = disp_z
    value = 0
    boundary = 'bottom top'
  []
  [rmin_fixed]
    type = DirichletBC
    variable = disp_r
    value = 0
    boundary = left
  []
  [contract]
    type = FunctionDirichletBC
    variable = disp_r
    function = -0.01*t
    boundary = right
  []
[]

[Kernels]
  [grad_stress_r]
    type = StressDivergenceRZTensors
    variable = disp_r
    component = 0
  []
  [grad_stress_z]
    type = StressDivergenceRZTensors
    variable = disp_z
    component = 1
  []
  [poro_r]
    type = PorousFlowEffectiveStressCoupling
    variable = disp_r
    component = 0
  []
  [poro_z]
    type = PorousFlowEffectiveStressCoupling
    variable = disp_z
    component = 1
  []
  [poro_vol_exp]
    type = PorousFlowMassVolumetricExpansion
    variable = porepressure
    fluid_component = 0
  []
  [mass0]
    type = PorousFlowMassTimeDerivative
    fluid_component = 0
    variable = porepressure
  []
[]

[AuxVariables]
  [stress_rr]
    order = CONSTANT
    family = MONOMIAL
  []
  [stress_rz]
    order = CONSTANT
    family = MONOMIAL
  []
  [stress_zz]
    order = CONSTANT
    family = MONOMIAL
  []
  [stress_tt]
    order = CONSTANT
    family = MONOMIAL
  []
  [strain_rr]
    order = CONSTANT
    family = MONOMIAL
  []
  [strain_zz]
    order = CONSTANT
    family = MONOMIAL
  []
  [strain_tt]
    order = CONSTANT
    family = MONOMIAL
  []
  [vol_strain]
    order = CONSTANT
    family = MONOMIAL
  []
[]

[AuxKernels]
  [stress_rr]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_rr
    index_i = 0
    index_j = 0
  []
  [stress_rz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_rz
    index_i = 0
    index_j = 1
  []
  [stress_zz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zz
    index_i = 1
    index_j = 1
  []
  [stress_tt]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_tt
    index_i = 2
    index_j = 2
  []
  [strain_rr]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = strain_rr
    index_i = 0
    index_j = 0
  []
  [strain_zz]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = strain_zz
    index_i = 1
    index_j = 1
  []
  [strain_tt]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = strain_tt
    index_i = 2
    index_j = 2
  []
  [vol_strain]
    type = MaterialRealAux
    property = PorousFlow_total_volumetric_strain_qp
    variable = vol_strain
  []
[]

[Modules]
  [FluidProperties]
    [simple_fluid]
      type = SimpleFluidProperties
      bulk_modulus = 0.5
      density0 = 1
      thermal_expansion = 0
      viscosity = 1
    []
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
  []
  [elasticity_tensor]
    type = ComputeElasticityTensor
    C_ijkl = '1 1.5'
    # bulk modulus is lambda + 2*mu/3 = 1 + 2*1.5/3 = 2
    fill_method = symmetric_isotropic
  []
  [strain]
    type = ComputeAxisymmetricRZSmallStrain
    volumetric_locking_correction = true # the strain will be the same at every qp of the element
  []
  [stress]
    type = ComputeLinearElasticStress
  []
  [vol_strain]
    type = PorousFlowVolumetricStrain
  []
  [eff_fluid_pressure]
    type = PorousFlowEffectiveFluidPressure
  []
  [ppss]
    type = PorousFlow1PhaseP
    porepressure = porepressure
    capillary_pressure = pc
  []
  [massfrac]
    type = PorousFlowMassFraction
  []
  [simple_fluid]
    type = PorousFlowSingleComponentFluid
    fp = simple_fluid
    phase = 0
  []
  [porosity]
    type = PorousFlowPorosityConst
    porosity = 0.1
  []
  [permeability]
    type = PorousFlowPermeabilityConst
    permeability = '0.5 0 0   0 0.5 0   0 0 0.5'
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'porepressure disp_r disp_z'
    number_fluid_phases = 1
    number_fluid_components = 1
  []
  [pc]
    type = PorousFlowCapillaryPressureVG
    m = 0.5
    alpha = 1
  []
[]

[Postprocessors]
  [p0]
    type = PointValue
    outputs = 'console csv'
    execute_on = 'initial timestep_end'
    point = '1.0 0 0'
    variable = porepressure
  []
  [vol_strain]
    type = PointValue
    outputs = 'console csv'
    execute_on = 'initial timestep_end'
    point = '1 0 0'
    variable = vol_strain
  []
  [strain_rr]
    type = PointValue
    outputs = 'console csv'
    execute_on = 'initial timestep_end'
    point = '1 0 0'
    variable = strain_rr
  []
  [strain_zz]
    type = PointValue
    outputs = 'console csv'
    execute_on = 'initial timestep_end'
    point = '1 0 0'
    variable = strain_zz
  []
  [strain_tt]
    type = PointValue
    outputs = 'console csv'
    execute_on = 'initial timestep_end'
    point = '1 0 0'
    variable = strain_tt
  []
  [rdisp]
    type = PointValue
    outputs = csv
    point = '2 0 0'
    use_displaced_mesh = false
    variable = disp_r
  []
  [stress_rr]
    type = PointValue
    outputs = csv
    point = '1 0 0'
    variable = stress_rr
  []
  [stress_zz]
    type = PointValue
    outputs = csv
    point = '1 0 0'
    variable = stress_zz
  []
  [stress_tt]
    type = PointValue
    outputs = csv
    point = '1 0 0'
    variable = stress_tt
  []
  [fluid_mass]
    type = PorousFlowFluidMass
    fluid_component = 0
    execute_on = 'initial timestep_end'
    outputs = 'console csv'
  []
[]

[Preconditioning]
  [andy]
    type = SMP
    full = true
    petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
    petsc_options_value = 'bcgs bjacobi 1E-14 1E-8 10000'
  []
[]

[Executioner]
  type = Transient
  solve_type = Newton
  start_time = 0
  end_time = 10
  dt = 2
[]

[Outputs]
  execute_on = 'initial timestep_end'
  [csv]
    type = CSV
  []
[]

(test/tests/materials/has_material/has_boundary_prop.i)

[Mesh]
  type = FileMesh
  file = rectangle.e
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  active = 'u_diff'
  [./u_diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 1
  [../]
  [./right]
    type = MatTestNeumannBC
    variable = u
    boundary = 2
    mat_prop = 'right_bc'
    has_check = true
  [../]
[]

[Materials]
  [./right_bc]
    type = GenericConstantMaterial
    boundary = 2
    prop_names = 'right_bc'
    prop_values = '2.0'
  [../]
  [./other]
    type = GenericConstantMaterial
    boundary = 1
    prop_names = 'other_value'
    prop_values = '1.0'
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
[]

[Outputs]
  execute_on = 'timestep_end'
  exodus = true
[]

(test/tests/multiapps/initial_intactive/master.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 10
  dt = 0.2

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

[MultiApps]
  [./sub]
    positions = '0 0 0'
    type = TransientMultiApp
    input_files = 'sub.i'
    app_type = MooseTestApp
    enable = false # Start with a multiapp that's disabled up front
    sub_cycling = true
  [../]
[]

[Controls]
  [./multiapp_enable]
    type = TimePeriod
    disable_objects = 'MultiApps::sub'
    start_time = 0
    end_time = 1.3
    execute_on = 'timestep_begin'
    reverse_on_false = true
  [../]
[]

(test/tests/vectorpostprocessors/time_data/time_data.i)

###############################################################
# The following tests that the CSV output object can include an
# additional .csv file that contains the time and timestep
# data from VectorPostprocessor object.
###############################################################


[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
  [./v]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./diff_v]
    type = Diffusion
    variable = v
  [../]
  [./time]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
  [./left_v]
    type = DirichletBC
    variable = v
    boundary = left
    value = 1
  [../]
  [./right_v]
    type = DirichletBC
    variable = v
    boundary = right
    value = 0
  [../]
[]

[VectorPostprocessors]
  [./line_sample]
    type = LineValueSampler
    variable = 'u v'
    start_point = '0 0.5 0'
    end_point = '1 0.5 0'
    num_points = 11
    sort_by = id
    execute_on = 'initial timestep_end'
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 20
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  execute_on = 'initial timestep_end'
  [./out]
    type = CSV
    time_data = true
    interval = 2
  [../]
[]

(test/tests/parser/cli_multiapp_all/dt_from_master_sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 10
  dt = 1 # This will be constrained by the master solve

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  execute_on = 'timestep_end'
  exodus = true
[]

(modules/peridynamics/test/tests/simple_tests/2D_regularD_variableH_OSPD.i)

# Test for ordinary state-based peridynamic formulation
# for regular grid from generated mesh with varying bond constants
# partial Jacobian
# Jacobian from bond-based formulation is used for preconditioning

# Square plate with Dirichlet boundary conditions applied
# at the left, top and bottom edges

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Mesh]
  type = PeridynamicsMesh
  horizon_number = 3

  [./gmg]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 4
    ny = 4
  [../]
  [./gpd]
    type = MeshGeneratorPD
    input = gmg
    retain_fe_mesh = false
  [../]
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
[]

[BCs]
  [./left_x]
    type = DirichletBC
    variable = disp_x
    boundary = 1003
    value = 0.0
  [../]
  [./top_y]
    type = DirichletBC
    variable = disp_y
    boundary = 1002
    value = 0.0
  [../]
  [./bottom_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 1000
    function = '-0.001*t'
  [../]
[]

[Modules/Peridynamics/Mechanics/Master]
  [./all]
    formulation = ORDINARY_STATE
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 2e5
    poissons_ratio = 0.0
  [../]

  [./force_density]
    type = ComputeSmallStrainVariableHorizonMaterialOSPD
  [../]
[]

[Preconditioning]
  [./SMP]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient
  solve_type = PJFNK
  line_search = none
  start_time = 0
  end_time = 1
[]

[Outputs]
  file_base = 2D_regularD_variableH_OSPD
  exodus = true
[]

(modules/porous_flow/test/tests/poro_elasticity/pp_generation_fullysat_action.i)

# Same as pp_generation.i, but using an Action
#
# A sample is constrained on all sides and its boundaries are
# also impermeable.  Fluid is pumped into the sample via a
# volumetric source (ie kg/second per cubic meter), and the
# rise in porepressure is observed.
#
# Source = s  (units = kg/m^3/second)
#
# Expect:
# fluid_mass = mass0 + s*t
# stress = 0 (remember this is effective stress)
# Porepressure = fluid_bulk*log(fluid_mass_density/density_P0), where fluid_mass_density = fluid_mass/porosity
# porosity = biot+(phi0-biot)*exp(pp(biot-1)/solid_bulk)
#
# Parameters:
# Biot coefficient = 0.3
# Phi0 = 0.1
# Solid Bulk modulus = 2
# fluid_bulk = 13
# density_P0 = 1

[Mesh]
  type = GeneratedMesh
  dim = 3
  nx = 1
  ny = 1
  nz = 1
  xmin = -0.5
  xmax = 0.5
  ymin = -0.5
  ymax = 0.5
  zmin = -0.5
  zmax = 0.5
[]

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
  PorousFlowDictator = dictator
  block = 0
[]

[Variables]
  [disp_x]
  []
  [disp_y]
  []
  [disp_z]
  []
  [porepressure]
  []
[]
[Modules]
  [FluidProperties]
    [the_simple_fluid]
      type = SimpleFluidProperties
      thermal_expansion = 0.0
      bulk_modulus = 13.0
      viscosity = 1.0
      density0 = 1.0
    []
  []
[]

[PorousFlowFullySaturated]
  coupling_type = HydroMechanical
  displacements = 'disp_x disp_y disp_z'
  porepressure = porepressure
  biot_coefficient = 0.3
  gravity = '0 0 0'
  fp = the_simple_fluid
  stabilization = none # not needed: there is no flow
  save_component_rate_in = nodal_kg_per_s
[]

[BCs]
  [confinex]
    type = DirichletBC
    variable = disp_x
    value = 0
    boundary = 'left right'
  []
  [confiney]
    type = DirichletBC
    variable = disp_y
    value = 0
    boundary = 'bottom top'
  []
  [confinez]
    type = DirichletBC
    variable = disp_z
    value = 0
    boundary = 'back front'
  []
[]


[Kernels]
  [source]
    type = BodyForce
    function = 0.1
    variable = porepressure
  []
[]

[AuxVariables]
  [nodal_kg_per_s]
  []
  [porosity]
    order = CONSTANT
    family = MONOMIAL
  []
[]

[AuxKernels]
  [porosity]
    type = PorousFlowPropertyAux
    variable = porosity
    property = porosity
  []
[]

[Materials]
  [elasticity_tensor]
    type = ComputeElasticityTensor
    C_ijkl = '1 1.5'
    # bulk modulus is lambda + 2*mu/3 = 1 + 2*1.5/3 = 2
    fill_method = symmetric_isotropic
  []
  [strain]
    type = ComputeSmallStrain
  []
  [stress]
    type = ComputeLinearElasticStress
  []
  [porosity]
    type = PorousFlowPorosity
    fluid = true
    mechanical = true
    porosity_zero = 0.1
    biot_coefficient = 0.3
    solid_bulk = 2
  []
  [permeability]
    type = PorousFlowPermeabilityConst
    permeability = '1 0 0   0 1 0   0 0 1' # unimportant
  []
[]

[Functions]
  [porosity_analytic]
    type = ParsedFunction
    value = 'biot+(phi0-biot)*exp(pp*(biot-1)/bulk)'
    vars = 'biot phi0 pp bulk'
    vals = '0.3 0.1 p0 2'
  []
[]

[Postprocessors]
  [nodal_kg_per_s]
    type = PointValue
    point = ' 0 0 0'
    variable = nodal_kg_per_s
    outputs = csv
  []
  [fluid_mass]
    type = PorousFlowFluidMass
    fluid_component = 0
    execute_on = 'initial timestep_end'
  []
  [porosity]
    type = PointValue
    outputs = 'console csv'
    point = '0 0 0'
    variable = porosity
  []
  [p0]
    type = PointValue
    outputs = csv
    point = '0 0 0'
    variable = porepressure
  []
  [porosity_analytic]
    type = FunctionValuePostprocessor
    function = porosity_analytic
  []
  [zdisp]
    type = PointValue
    outputs = csv
    point = '0 0 0.5'
    variable = disp_z
  []
  [stress_xx]
    type = PointValue
    outputs = csv
    point = '0 0 0'
    variable = stress_xx
  []
  [stress_yy]
    type = PointValue
    outputs = csv
    point = '0 0 0'
    variable = stress_yy
  []
  [stress_zz]
    type = PointValue
    outputs = csv
    point = '0 0 0'
    variable = stress_zz
  []

[]


[Preconditioning]
  [andy]
    type = SMP
    full = true
    petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it'
    petsc_options_value = 'bcgs bjacobi 1E-14 1E-10 10000'
  []
[]

[Executioner]
  type = Transient
  solve_type = Newton
  start_time = 0
  end_time = 10
  dt = 1
[]

[Outputs]
  execute_on = 'timestep_end'
  file_base = pp_generation_fullysat_action
  csv = true
[]

(test/tests/misc/check_error/interface_kernel_with_aux_var.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 2
[]

[Variables]
  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[AuxVariables]
  [./v]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./rea]
    type = Reaction
    variable = u
  [../]
[]

[InterfaceKernels]
  [./nope]
    type = InterfaceDiffusion
    variable = v
    neighbor_var = u
    boundary = 'left'
    D = 4
    D_neighbor = 2
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = 2
    value = 1
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'NEWTON'
[]

[Outputs]
  file_base = out
  exodus = true
[]

(modules/tensor_mechanics/test/tests/dynamics/time_integration/hht_test.i)

# Test for  HHT time integration

# The test is for an 1D bar element of  unit length fixed on one end
# with a ramped pressure boundary condition applied to the other end.
# alpha, beta and gamma are HHT time integration parameters
# The equation of motion in terms of matrices is:
#
# M*accel + alpha*(K*disp - K*disp_old) + K*disp = P(t+alpha dt)*Area
#
# Here M is the mass matrix, K is the stiffness matrix, P is the applied pressure
#
# This equation is equivalent to:
#
# density*accel + alpha*(Div stress - Div stress_old) +Div Stress= P(t+alpha dt)
#
# The first term on the left is evaluated using the Inertial force kernel
# The next two terms on the left involving alpha are evaluated using the
# DynamicStressDivergenceTensors Kernel
# The residual due to Pressure is evaluated using Pressure boundary condition
#
# The system will come to steady state slowly after the pressure becomes constant.
# Alpha equal to zero will result in Newmark integration.

[Mesh]
  type = GeneratedMesh
  dim = 3
  nx = 1
  ny = 1
  nz = 1
  xmin = 0.0
  xmax = 0.1
  ymin = 0.0
  ymax = 1.0
  zmin = 0.0
  zmax = 0.1
[]


[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
  [./disp_z]
  [../]
[]

[AuxVariables]
  [./vel_x]
  [../]
  [./accel_x]
  [../]
  [./vel_y]
  [../]
  [./accel_y]
  [../]
  [./vel_z]
  [../]
  [./accel_z]
  [../]
  [./stress_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strain_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]

[]

[Kernels]
  [./DynamicTensorMechanics]
    displacements = 'disp_x disp_y disp_z'
    hht_alpha = 0.11
  [../]
  [./inertia_x]
    type = InertialForce
    variable = disp_x
    velocity = vel_x
    acceleration = accel_x
    beta = 0.25
    gamma = 0.5
  [../]
  [./inertia_y]
    type = InertialForce
    variable = disp_y
    velocity = vel_y
    acceleration = accel_y
    beta = 0.25
    gamma = 0.5
  [../]
  [./inertia_z]
    type = InertialForce
    variable = disp_z
    velocity = vel_z
    acceleration = accel_z
    beta = 0.25
    gamma = 0.5
  [../]

[]

[AuxKernels]
  [./accel_x]
    type = NewmarkAccelAux
    variable = accel_x
    displacement = disp_x
    velocity = vel_x
    beta = 0.25
    execute_on = timestep_end
  [../]
  [./vel_x]
    type = NewmarkVelAux
    variable = vel_x
    acceleration = accel_x
    gamma = 0.5
    execute_on = timestep_end
  [../]
  [./accel_y]
    type = NewmarkAccelAux
    variable = accel_y
    displacement = disp_y
    velocity = vel_y
    beta = 0.25
    execute_on = timestep_end
  [../]
  [./vel_y]
    type = NewmarkVelAux
    variable = vel_y
    acceleration = accel_y
    gamma = 0.5
    execute_on = timestep_end
  [../]
  [./accel_z]
    type = NewmarkAccelAux
    variable = accel_z
    displacement = disp_z
    velocity = vel_z
    beta = 0.25
    execute_on = timestep_end
  [../]
  [./vel_z]
    type = NewmarkVelAux
    variable = vel_z
    acceleration = accel_z
    gamma = 0.5
    execute_on = timestep_end
  [../]
  [./stress_yy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yy
    index_i = 0
    index_j = 1
  [../]
  [./strain_yy]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = strain_yy
    index_i = 0
    index_j = 1
  [../]

[]


[BCs]
  [./top_y]
    type = DirichletBC
    variable = disp_y
    boundary = top
    value=0.0
  [../]
  [./top_x]
    type = DirichletBC
    variable = disp_x
    boundary = top
    value=0.0
  [../]
  [./top_z]
    type = DirichletBC
    variable = disp_z
    boundary = top
    value=0.0
  [../]
  [./bottom_x]
    type = DirichletBC
    variable = disp_x
    boundary = bottom
    value=0.0
  [../]
  [./bottom_z]
    type = DirichletBC
    variable = disp_z
    boundary = bottom
    value=0.0
  [../]
  [./Pressure]
    [./Side1]
      boundary = bottom
      function = pressure
      factor = 1
      hht_alpha = 0.11
      displacements = 'disp_x disp_y disp_z'
    [../]
  [../]
[]

[Materials]
  [./Elasticity_tensor]
    type = ComputeElasticityTensor
    block = 0
    fill_method = symmetric_isotropic
    C_ijkl = '210e9 0'
  [../]

  [./strain]
    type = ComputeSmallStrain
    block = 0
    displacements = 'disp_x disp_y disp_z'
  [../]

  [./stress]
    type = ComputeLinearElasticStress
    block = 0
  [../]
  [./density]
    type = GenericConstantMaterial
    block = 0
    prop_names = 'density'
    prop_values = '7750'
  [../]

[]

[Executioner]
  type = Transient
  start_time = 0
  end_time = 2
  dt = 0.1
[]


[Functions]
  [./pressure]
    type = PiecewiseLinear
    x = '0.0 0.1 0.2 1.0 2.0 5.0'
    y = '0.0 0.1 0.2 1.0 1.0 1.0'
    scale_factor = 1e9
  [../]
[]

[Postprocessors]
  [./_dt]
    type = TimestepSize
  [../]
  [./disp]
    type = NodalExtremeValue
    variable = disp_y
    boundary = bottom
  [../]
  [./vel]
    type = NodalExtremeValue
    variable = vel_y
    boundary = bottom
  [../]
  [./accel]
    type = NodalExtremeValue
    variable = accel_y
    boundary = bottom
  [../]
  [./stress_yy]
    type = ElementAverageValue
    variable = stress_yy
  [../]
  [./strain_yy]
    type = ElementAverageValue
    variable = strain_yy
  [../]
[]

[Outputs]
  exodus = true
  perf_graph = true
[]

(test/tests/multiapps/picard_catch_up/sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 2
[]

[Variables]
  [./v]
  [../]
[]

[AuxVariables]
  [./u]
  [../]
[]

[Kernels]
  [./diff_v]
    type = Diffusion
    variable = v
  [../]
  [./force_v]
    type = CoupledForce
    variable = v
    v = u
  [../]
  [./nan]
    type = NanAtCountKernel
    variable = v
    count = 32
  [../]
[]

[BCs]
  [./left_v]
    type = DirichletBC
    variable = v
    preset = false
    boundary = left
    value = 1
  [../]
  [./right_v]
    type = FunctionDirichletBC
    variable = v
    preset = false
    boundary = right
    function = 't + 1'
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 2
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
  nl_abs_tol = 1e-10
  snesmf_reuse_base = false
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/rom_stress_update/2drz_json.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 2
[]

[Problem]
  coord_type = RZ
[]

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[AuxVariables]
  [./temperature]
    initial_condition = 900.0
  [../]
[]

[Modules/TensorMechanics/Master]
  [./all]
    strain = FINITE
    add_variables = true
    generate_output = vonmises_stress
  [../]
[]

[BCs]
  [./symmy]
    type = DirichletBC
    variable = disp_y
    boundary = bottom
    value = 0
  [../]
  [./symmx]
    type = DirichletBC
    variable = disp_x
    boundary = left
    value = 0
  [../]
  [./pressure_x]
    type = Pressure
    variable = disp_x
    boundary = right
    function = t
    factor = 3.1675e5
  [../]
  [./pressure_y]
    type = Pressure
    variable = disp_y
    boundary = top
    function = t
    factor = 6.336e5
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 3.30e11
    poissons_ratio = 0.3
  [../]
  [./stress]
    type = ComputeMultipleInelasticStress
    inelastic_models = rom_stress_prediction
  [../]
  [./rom_stress_prediction]
    type = LAROMANCEStressUpdate
    temperature = temperature
    initial_cell_dislocation_density = 6.0e12
    initial_wall_dislocation_density = 4.4e11
    model = laromance/test/SS316H.json
    outputs = all
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'NEWTON'

  nl_abs_tol = 1e-12
  automatic_scaling = true
  compute_scaling_once = false

  num_steps = 5
  dt = 2
[]

[Postprocessors]
  [./effective_strain_avg]
    type = ElementAverageValue
    variable = effective_creep_strain
  [../]
  [./temperature]
    type = ElementAverageValue
    variable = temperature
  [../]
  [./cell_dislocations]
    type = ElementAverageValue
    variable = cell_dislocations
  [../]
  [./wall_disloactions]
    type = ElementAverageValue
    variable = wall_dislocations
  [../]
  [./vonmises_stress]
    type = ElementAverageValue
    variable = vonmises_stress
  [../]
[]

[Outputs]
  csv = true
[]

(test/tests/parser/multiple_inputs/diffusion1a.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  []
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
[]

[Outputs]
  exodus = true
[]

(modules/contact/test/tests/sliding_block/in_and_out/frictionless_kinematic.i)

#  This is a benchmark test that checks constraint based frictionless
#  contact using the kinematic method.  In this test a sinusoidal
#  displacement is applied in the horizontal direction to simulate
#  a small block come in and out of contact as it slides down a larger block.
#
#  The sinusoid is of the form 0.4sin(4t)+0.2. The gold file is run
#  on one processor and the benchmark
#  case is run on a minimum of 4 processors to ensure no parallel variability
#  in the contact pressure and penetration results.  Further documentation can
#  found in moose/modules/contact/doc/sliding_block/
#

[Mesh]
  file = sliding_elastic_blocks_2d.e
  patch_size = 80
[]

[GlobalParams]
  volumetric_locking_correction = false
  displacements = 'disp_x disp_y'
[]

[AuxVariables]
  [./penetration]
  [../]
  [./inc_slip_x]
  [../]
  [./inc_slip_y]
  [../]
  [./accum_slip_x]
  [../]
  [./accum_slip_y]
  [../]
[]

[Functions]
  [./vertical_movement]
    type = ParsedFunction
    value = -t
  [../]
  [./horizontal_movement]
    type = ParsedFunction
    value = -0.04*sin(4*t)+0.02
  [../]
[]

[Modules/TensorMechanics/Master]
  [./all]
    add_variables = true
    strain = FINITE
  [../]
[]

[AuxKernels]
  [./zeroslip_x]
    type = ConstantAux
    variable = inc_slip_x
    boundary = 3
    execute_on = timestep_begin
    value = 0.0
  [../]
  [./zeroslip_y]
    type = ConstantAux
    variable = inc_slip_y
    boundary = 3
    execute_on = timestep_begin
    value = 0.0
  [../]
  [./accum_slip_x]
    type = AccumulateAux
    variable = accum_slip_x
    accumulate_from_variable = inc_slip_x
    execute_on = timestep_end
  [../]
  [./accum_slip_y]
    type = AccumulateAux
    variable = accum_slip_y
    accumulate_from_variable = inc_slip_y
    execute_on = timestep_end
  [../]
  [./penetration]
    type = PenetrationAux
    variable = penetration
    boundary = 3
    paired_boundary = 2
  [../]
[]

[Postprocessors]
  [./nonlinear_its]
    type = NumNonlinearIterations
    execute_on = timestep_end
  [../]
  [./penetration]
    type = NodalVariableValue
    variable = penetration
    nodeid = 222
  [../]
  [./contact_pressure]
    type = NodalVariableValue
    variable = contact_pressure
    nodeid = 222
  [../]
[]

[BCs]
  [./left_x]
    type = DirichletBC
    variable = disp_x
    boundary = 1
    value = 0.0
  [../]
  [./left_y]
    type = DirichletBC
    variable = disp_y
    boundary = 1
    value = 0.0
  [../]
  [./right_x]
    type = FunctionDirichletBC
    variable = disp_x
    boundary = 4
    function = horizontal_movement
  [../]
  [./right_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 4
    function = vertical_movement
  [../]
[]

[Materials]
  [./left]
    type = ComputeIsotropicElasticityTensor
    block = '1 2'
    youngs_modulus = 1e6
    poissons_ratio = 0.3
    constant_on = SUBDOMAIN
  [../]
  [./stress]
    type = ComputeFiniteStrainElasticStress
    block = '1 2'
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'

  petsc_options = '-snes_ksp_ew'
  petsc_options_iname = '-pc_type -sub_pc_type -pc_asm_overlap -ksp_gmres_restart'
  petsc_options_value = 'asm     lu    20    101'

  line_search = 'none'

  l_max_its = 100
  nl_max_its = 1000
  dt = 0.1
  end_time = 15
  num_steps = 1000
  l_tol = 1e-6
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-6
  dtmin = 0.01

  [./Predictor]
    type = SimplePredictor
    scale = 1.0
  [../]
[]

[Outputs]
  interval = 10
  [./out]
    type = Exodus
    elemental_as_nodal = true
  [../]
  [./console]
    type = Console
    max_rows = 5
  [../]
[]

[Contact]
  [./leftright]
    secondary = 3
    primary = 2
    model = frictionless
    penalty = 1e+6
    normal_smoothing_distance = 0.1
  [../]
[]

(modules/navier_stokes/test/tests/auxkernels/peclet-number-functor-aux/fe-thermal.i)

rho = 1
mu = 1
k = 1
cp = 1

[GlobalParams]
  gravity = '0 0 0'
  pspg = true
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 10
    ny = 10
  []
  [corner_node]
    type = ExtraNodesetGenerator
    new_boundary = 'pinned_node'
    nodes = '0'
    input = gen
  []
[]

[AuxVariables]
  [Pe]
    family = MONOMIAL
    order = FIRST
  []
[]

[AuxKernels]
  [Pe]
    type = PecletNumberFunctorAux
    variable = Pe
    speed = speed
    thermal_diffusivity = 'thermal_diffusivity'
  []
[]

[Variables]
  [vel_x][]
  [vel_y][]
  [p][]
  [T][]
[]

[Kernels]
  # mass
  [mass]
    type = INSMass
    variable = p
    u = vel_x
    v = vel_y
    pressure = p
  []
  # x-momentum, space
  [x_momentum_space]
    type = INSMomentumLaplaceForm
    variable = vel_x
    u = vel_x
    v = vel_y
    pressure = p
    component = 0
  []
  # y-momentum, space
  [y_momentum_space]
    type = INSMomentumLaplaceForm
    variable = vel_y
    u = vel_x
    v = vel_y
    pressure = p
    component = 1
  []
  [temperature_space]
    type = INSTemperature
    variable = T
    u = vel_x
    v = vel_y
  []
[]

[BCs]
  [x_no_slip]
    type = DirichletBC
    variable = vel_x
    boundary = 'bottom right left'
    value = 0.0
  []
  [lid]
    type = FunctionDirichletBC
    variable = vel_x
    boundary = 'top'
    function = 'lid_function'
  []
  [y_no_slip]
    type = DirichletBC
    variable = vel_y
    boundary = 'bottom right top left'
    value = 0.0
  []
  [pressure_pin]
    type = DirichletBC
    variable = p
    boundary = 'pinned_node'
    value = 0
  []
  [T_hot]
    type = DirichletBC
    variable = T
    boundary = 'bottom'
    value = 1
  []
  [T_cold]
    type = DirichletBC
    variable = T
    boundary = 'top'
    value = 0
  []
[]

[Materials]
  [const]
    type = GenericConstantMaterial
    block = 0
    prop_names = 'rho mu k cp'
    prop_values = '${rho} ${mu} ${k} ${cp}'
  []
  [speed]
    type = ADVectorMagnitudeFunctorMaterial
    x_functor = vel_x
    y_functor = vel_y
    vector_magnitude_name = speed
  []
  [thermal_diffusivity]
    type = ThermalDiffusivityFunctorMaterial
    k = ${k}
    rho = ${rho}
    cp = ${cp}
  []
[]

[Functions]
  [lid_function]
    # We pick a function that is exactly represented in the velocity
    # space so that the Dirichlet conditions are the same regardless
    # of the mesh spacing.
    type = ParsedFunction
    value = '4*x*(1-x)'
  []
[]

[Preconditioning]
  [SMP]
    type = SMP
    full = true
    solve_type = 'NEWTON'
  []
[]

[Executioner]
  type = Steady
  petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type'
  petsc_options_value = 'asm      2               lu'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/lagrangian/total/homogenization/large-tests/1d-strain.i)

# 2D test with just strain control

[GlobalParams]
  displacements = 'disp_x'
  large_kinematics = true
  constraint_types = 'strain'
  ndim = 1
  macro_gradient = hvar
[]

[Mesh]
  [base]
    type = FileMeshGenerator
    file = '1d.exo'
  []
  [sets]
    input = base
    type = SideSetsFromPointsGenerator
    new_boundary = 'left right'
    points = '-1 0 0
               7 0 0'
  []
[]

[Variables]
  [disp_x]
  []
  [hvar]
    family = SCALAR
    order = FIRST
  []
[]

[AuxVariables]
  [s11]
    family = MONOMIAL
    order = CONSTANT
  []
  [s21]
    family = MONOMIAL
    order = CONSTANT
  []
  [s31]
    family = MONOMIAL
    order = CONSTANT
  []
  [s12]
    family = MONOMIAL
    order = CONSTANT
  []
  [s22]
    family = MONOMIAL
    order = CONSTANT
  []
  [s32]
    family = MONOMIAL
    order = CONSTANT
  []
  [s13]
    family = MONOMIAL
    order = CONSTANT
  []
  [s23]
    family = MONOMIAL
    order = CONSTANT
  []
  [s33]
    family = MONOMIAL
    order = CONSTANT
  []

  [F11]
    family = MONOMIAL
    order = CONSTANT
  []
  [F21]
    family = MONOMIAL
    order = CONSTANT
  []
  [F31]
    family = MONOMIAL
    order = CONSTANT
  []
  [F12]
    family = MONOMIAL
    order = CONSTANT
  []
  [F22]
    family = MONOMIAL
    order = CONSTANT
  []
  [F32]
    family = MONOMIAL
    order = CONSTANT
  []
  [F13]
    family = MONOMIAL
    order = CONSTANT
  []
  [F23]
    family = MONOMIAL
    order = CONSTANT
  []
  [F33]
    family = MONOMIAL
    order = CONSTANT
  []
[]

[AuxKernels]
  [s11]
    type = RankTwoAux
    variable = s11
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 0
  []
  [s21]
    type = RankTwoAux
    variable = s21
    rank_two_tensor = pk1_stress
    index_i = 1
    index_j = 0
  []
  [s31]
    type = RankTwoAux
    variable = s31
    rank_two_tensor = pk1_stress
    index_i = 2
    index_j = 0
  []
  [s12]
    type = RankTwoAux
    variable = s12
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 1
  []
  [s22]
    type = RankTwoAux
    variable = s22
    rank_two_tensor = pk1_stress
    index_i = 1
    index_j = 1
  []
  [s32]
    type = RankTwoAux
    variable = s32
    rank_two_tensor = pk1_stress
    index_i = 2
    index_j = 1
  []
  [s13]
    type = RankTwoAux
    variable = s13
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 2
  []
  [s23]
    type = RankTwoAux
    variable = s23
    rank_two_tensor = pk1_stress
    index_i = 1
    index_j = 2
  []
  [s33]
    type = RankTwoAux
    variable = s33
    rank_two_tensor = pk1_stress
    index_i = 2
    index_j = 2
  []

  [F11]
    type = RankTwoAux
    variable = F11
    rank_two_tensor = deformation_gradient
    index_i = 0
    index_j = 0
  []
  [F21]
    type = RankTwoAux
    variable = F21
    rank_two_tensor = deformation_gradient
    index_i = 1
    index_j = 0
  []
  [F31]
    type = RankTwoAux
    variable = F31
    rank_two_tensor = deformation_gradient
    index_i = 2
    index_j = 0
  []
  [F12]
    type = RankTwoAux
    variable = F12
    rank_two_tensor = deformation_gradient
    index_i = 0
    index_j = 1
  []
  [F22]
    type = RankTwoAux
    variable = F22
    rank_two_tensor = deformation_gradient
    index_i = 1
    index_j = 1
  []
  [F32]
    type = RankTwoAux
    variable = F32
    rank_two_tensor = deformation_gradient
    index_i = 2
    index_j = 1
  []
  [F13]
    type = RankTwoAux
    variable = F13
    rank_two_tensor = deformation_gradient
    index_i = 0
    index_j = 2
  []
  [F23]
    type = RankTwoAux
    variable = F23
    rank_two_tensor = deformation_gradient
    index_i = 1
    index_j = 2
  []
  [F33]
    type = RankTwoAux
    variable = F33
    rank_two_tensor = deformation_gradient
    index_i = 2
    index_j = 2
  []
[]

[UserObjects]
  [integrator]
    type = HomogenizationConstraintIntegral
    targets = 'strain11'
    execute_on = 'initial linear'
  []
[]

[Kernels]
  [sdx]
    type = HomogenizedTotalLagrangianStressDivergence
    variable = disp_x
    component = 0
  []
[]

[ScalarKernels]
  [enforce]
    type = HomogenizationConstraintScalarKernel
    variable = hvar
    integrator = integrator
  []
[]

[Functions]
  [strain11]
    type = ParsedFunction
    value = '4.0e-1*t'
  []
[]

[BCs]
  [Periodic]
    [all]
      variable = disp_x
      auto_direction = 'x'
    []
  []

  [centerfix_x]
    type = DirichletBC
    boundary = "fixme"
    variable = disp_x
    value = 0
  []
[]

[Materials]
  [elastic_tensor_1]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 100000.0
    poissons_ratio = 0.3
    block = '1'
  []
  [elastic_tensor_2]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 120000.0
    poissons_ratio = 0.21
    block = '2'
  []
  [elastic_tensor_3]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 80000.0
    poissons_ratio = 0.4
    block = '3'
  []
  [elastic_tensor_4]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 76000.0
    poissons_ratio = 0.11
    block = '4'
  []
  [compute_stress]
    type = ComputeLagrangianLinearElasticStress
  []
  [compute_strain]
    type = ComputeLagrangianStrain
    homogenization_gradient_names = 'homogenization_gradient'
  []
  [compute_homogenization_gradient]
    type = ComputeHomogenizedLagrangianStrain
  []
[]

[Preconditioning]
  [smp]
    type = SMP
    full = true
  []
[]

[Postprocessors]
  [s11]
    type = ElementAverageValue
    variable = s11
    execute_on = 'initial timestep_end'
  []
  [s21]
    type = ElementAverageValue
    variable = s21
    execute_on = 'initial timestep_end'
  []
  [s31]
    type = ElementAverageValue
    variable = s31
    execute_on = 'initial timestep_end'
  []
  [s12]
    type = ElementAverageValue
    variable = s12
    execute_on = 'initial timestep_end'
  []
  [s22]
    type = ElementAverageValue
    variable = s22
    execute_on = 'initial timestep_end'
  []
  [s32]
    type = ElementAverageValue
    variable = s32
    execute_on = 'initial timestep_end'
  []
  [s13]
    type = ElementAverageValue
    variable = s13
    execute_on = 'initial timestep_end'
  []
  [s23]
    type = ElementAverageValue
    variable = s23
    execute_on = 'initial timestep_end'
  []
  [s33]
    type = ElementAverageValue
    variable = s33
    execute_on = 'initial timestep_end'
  []

  [F11]
    type = ElementAverageValue
    variable = F11
    execute_on = 'initial timestep_end'
  []
  [F21]
    type = ElementAverageValue
    variable = F21
    execute_on = 'initial timestep_end'
  []
  [F31]
    type = ElementAverageValue
    variable = F31
    execute_on = 'initial timestep_end'
  []
  [F12]
    type = ElementAverageValue
    variable = F12
    execute_on = 'initial timestep_end'
  []
  [F22]
    type = ElementAverageValue
    variable = F22
    execute_on = 'initial timestep_end'
  []
  [F32]
    type = ElementAverageValue
    variable = F32
    execute_on = 'initial timestep_end'
  []
  [F13]
    type = ElementAverageValue
    variable = F13
    execute_on = 'initial timestep_end'
  []
  [F23]
    type = ElementAverageValue
    variable = F23
    execute_on = 'initial timestep_end'
  []
  [F33]
    type = ElementAverageValue
    variable = F33
    execute_on = 'initial timestep_end'
  []
[]

[Executioner]
  type = Transient

  solve_type = 'newton'
  line_search = none

  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'

  l_max_its = 2
  l_tol = 1e-14
  nl_max_its = 10
  nl_rel_tol = 1e-8
  nl_abs_tol = 1e-10

  start_time = 0.0
  dt = 0.2
  dtmin = 0.2
  end_time = 1.0
[]

[Outputs]
  exodus = false
  csv = true
[]

(modules/contact/test/tests/mortar_tm/2d/frictionless_second/finite_rr.i)

E_block = 1e7
E_plank = 1e7
elem = QUAD9
order = SECOND
name = 'finite_rr'

[Mesh]
  patch_size = 80
  patch_update_strategy = auto
  [plank]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = -0.3
    xmax = 0.3
    ymin = -10
    ymax = 10
    nx = 2
    ny = 67
    elem_type = ${elem}
    boundary_name_prefix = plank
  []
  [plank_id]
    type = SubdomainIDGenerator
    input = plank
    subdomain_id = 1
  []

  [block]
    type = GeneratedMeshGenerator
    dim = 2
    xmin = 0.31
    xmax = 0.91
    ymin = 7.7
    ymax = 8.5
    nx = 3
    ny = 4
    elem_type = ${elem}
    boundary_name_prefix = block
    boundary_id_offset = 10
  []
  [block_id]
    type = SubdomainIDGenerator
    input = block
    subdomain_id = 2
  []

  [combined]
    type = MeshCollectionGenerator
    inputs = 'plank_id block_id'
  []
  [block_rename]
    type = RenameBlockGenerator
    input = combined
    old_block = '1 2'
    new_block = 'plank block'
  []
[]

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Problem]
  type = ReferenceResidualProblem
  extra_tag_vectors = 'ref'
  reference_vector = 'ref'
[]

[Variables]
  [disp_x]
    order = ${order}
    block = 'plank block'
    scaling = '${fparse 2.0 / (E_plank + E_block)}'
  []
  [disp_y]
    order = ${order}
    block = 'plank block'
    scaling = '${fparse 2.0 / (E_plank + E_block)}'
  []
[]

[Modules/TensorMechanics/Master]
  [action]
    strain = FINITE
    generate_output = 'stress_xx stress_yy stress_zz vonmises_stress hydrostatic_stress strain_xx '
                      'strain_yy strain_zz'
    block = 'plank block'
    extra_vector_tags = 'ref'
  []
[]

[Contact]
  [frictionless]
    primary = plank_right
    secondary = block_left
    formulation = mortar
    c_normal = 1e0
  []
[]

[BCs]
  [left_x]
    type = DirichletBC
    variable = disp_x
    preset = false
    boundary = plank_left
    value = 0.0
  []
  [left_y]
    type = DirichletBC
    variable = disp_y
    preset = false
    boundary = plank_bottom
    value = 0.0
  []
  [right_x]
    type = FunctionDirichletBC
    variable = disp_x
    preset = false
    boundary = block_right
    function = '-0.04*sin(4*(t+1.5))+0.02'
  []
  [right_y]
    type = FunctionDirichletBC
    variable = disp_y
    preset = false
    boundary = block_right
    function = '-t'
  []
[]

[Materials]
  [plank]
    type = ComputeIsotropicElasticityTensor
    block = 'plank'
    poissons_ratio = 0.3
    youngs_modulus = ${E_plank}
  []
  [block]
    type = ComputeIsotropicElasticityTensor
    block = 'block'
    poissons_ratio = 0.3
    youngs_modulus = ${E_block}
  []
  [stress]
    type = ComputeFiniteStrainElasticStress
    block = 'plank block'
  []
[]

[Preconditioning]
  [smp]
    type = SMP
    full = true
  []
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'
  petsc_options = '-snes_converged_reason -ksp_converged_reason'
  petsc_options_iname = '-pc_type -mat_mffd_err -pc_factor_shift_type -pc_factor_shift_amount'
  petsc_options_value = 'lu       1e-5          NONZERO               1e-15'
  end_time = 5.0
  dt = 0.1
  dtmin = 0.1
  timestep_tolerance = 1e-6
  line_search = 'contact'
  nl_abs_tol = 1e-7
[]

[Postprocessors]
  [nl_its]
    type = NumNonlinearIterations
  []
  [total_nl_its]
    type = CumulativeValuePostprocessor
    postprocessor = nl_its
  []
  [l_its]
    type = NumLinearIterations
  []
  [total_l_its]
    type = CumulativeValuePostprocessor
    postprocessor = l_its
  []
  [contact]
    type = ContactDOFSetSize
    variable = frictionless_normal_lm
    subdomain = frictionless_secondary_subdomain
  []
  [avg_hydro]
    type = ElementAverageValue
    variable = hydrostatic_stress
    block = 'block'
  []
  [max_hydro]
    type = ElementExtremeValue
    variable = hydrostatic_stress
    block = 'block'
  []
  [min_hydro]
    type = ElementExtremeValue
    variable = hydrostatic_stress
    block = 'block'
    value_type = min
  []
  [avg_vonmises]
    type = ElementAverageValue
    variable = vonmises_stress
    block = 'block'
  []
  [max_vonmises]
    type = ElementExtremeValue
    variable = vonmises_stress
    block = 'block'
  []
  [min_vonmises]
    type = ElementExtremeValue
    variable = vonmises_stress
    block = 'block'
    value_type = min
  []
[]

[Outputs]
  exodus = true
  file_base = ${name}
  [comp]
    type = CSV
    show = 'contact'
  []
  [out]
    type = CSV
    file_base = '${name}_out'
  []
[]

[Debug]
  show_var_residual_norms = true
[]

(test/tests/transfers/multiapp_nearest_node_transfer/two_way_many_apps_sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
  xmax = 0.2
  ymax = 0.2
[]

[Variables]
  [./u]
  [../]
[]

[AuxVariables]
  [./from_master]
  [../]
  [./elemental_from_master]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 1
  dt = 1

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(test/tests/transfers/multiapp_postprocessor_transfer/sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = CoefDiffusion
    variable = u
    coef = 0.01
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 2
  [../]
[]

[Postprocessors]
  [./from_master]
    type = Receiver
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 1
  dt = 1

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'

  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
[]

(test/tests/geomsearch/2d_moving_penetration/pl_test4qnns.i)

[GlobalParams]
  order = SECOND
  family = LAGRANGE
[]

[Mesh]
  file = pl_test4q.e
  displacements = 'disp_x disp_y'
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
[]

[AuxVariables]
  [./distance]
  [../]
  [./tangential_distance]
  [../]
  [./normal_x]
  [../]
  [./normal_y]
  [../]
  [./closest_point_x]
  [../]
  [./closest_point_y]
  [../]
  [./element_id]
  [../]
  [./side]
  [../]
[]

[Kernels]
  [./diff_x]
    type = Diffusion
    variable = disp_x
  [../]
  [./diff_y]
    type = Diffusion
    variable = disp_y
  [../]
[]

[AuxKernels]
  [./penetrate]
    type = PenetrationAux
    variable = distance
    boundary = 11            #secondary
    paired_boundary = 12     #primary
  [../]

  [./penetrate2]
    type = PenetrationAux
    variable = distance
    boundary = 12            #secondary
    paired_boundary = 11     #primary
    normal_smoothing_method = nodal_normal_based
  [../]

  [./penetrate3]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 11
    paired_boundary = 12
    quantity = tangential_distance
  [../]

  [./penetrate4]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 12
    paired_boundary = 11
    quantity = tangential_distance
  [../]

  [./penetrate5]
    type = PenetrationAux
    variable = normal_x
    boundary = 11
    paired_boundary = 12
    quantity = normal_x
  [../]

  [./penetrate6]
    type = PenetrationAux
    variable = normal_x
    boundary = 12
    paired_boundary = 11
    quantity = normal_x
  [../]

  [./penetrate7]
    type = PenetrationAux
    variable = normal_y
    boundary = 11
    paired_boundary = 12
    quantity = normal_y
  [../]

  [./penetrate8]
    type = PenetrationAux
    variable = normal_y
    boundary = 12
    paired_boundary = 11
    quantity = normal_y
  [../]

  [./penetrate9]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 11
    paired_boundary = 12
    quantity = closest_point_x
  [../]

  [./penetrate10]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 12
    paired_boundary = 11
    quantity = closest_point_x
  [../]

  [./penetrate11]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 11
    paired_boundary = 12
    quantity = closest_point_y
  [../]

  [./penetrate12]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 12
    paired_boundary = 11
    quantity = closest_point_y
  [../]

  [./penetrate13]
    type = PenetrationAux
    variable = element_id
    boundary = 11
    paired_boundary = 12
    quantity = element_id
  [../]

  [./penetrate14]
    type = PenetrationAux
    variable = element_id
    boundary = 12
    paired_boundary = 11
    quantity = element_id
  [../]

  [./penetrate15]
    type = PenetrationAux
    variable = side
    boundary = 11
    paired_boundary = 12
    quantity = side
  [../]

  [./penetrate16]
    type = PenetrationAux
    variable = side
    boundary = 12
    paired_boundary = 11
    quantity = side
  [../]
[]

[BCs]
  [./b1x]
    type = DirichletBC
    variable = disp_x
    boundary = 1
    value = 0
  [../]

  [./b1y]
    type = DirichletBC
    variable = disp_y
    boundary = 1
    value = 0
  [../]

  [./b2x]
    type = DirichletBC
    variable = disp_x
    boundary = 2
    value = 0
  [../]

  [./b2y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 2
    function = disp_y
  [../]
[]

[Functions]
  [./disp_y]
    type = PiecewiseLinear
    x = '0.0 0.25 0.75 1.0'
    y = '0.0 2.0 -2.0  0.0'
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'
  petsc_options = '-snes_ksp_ew'

  nl_rel_tol = 1.e-9
  l_max_its = 10

  start_time = 0.0
  dt = 0.02
  end_time = 1.0
  [./Quadrature]
    order = THIRD
  [../]
[]

[Outputs]
  file_base = pl_test4qnns_out
  exodus = true
[]

[NodalNormals]
  boundary = 11
  corner_boundary = 20
[]

(test/tests/time_steppers/constant_dt/constant_dt.i)

###########################################################
# This is a simple test with a time-dependent problem
# demonstrating the use of the TimeStepper system.
#
# @Requirement F1.20
###########################################################


[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  [../]
  [./time]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 10
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'

  # Pluggable TimeStepper System
  [./TimeStepper]
    type = ConstantDT
    dt = 0.2
  [../]
[]

[Outputs]
  exodus = true
[]

(test/tests/tag/eigen_tag.i)

[Mesh/gmg]
  type = GeneratedMeshGenerator
  dim = 2
  nx = 5
  ny = 5
[]

[Variables/u]
[]

[AuxVariables]
  [vec_tag_diff]
    order = FIRST
    family = LAGRANGE
  []
  [vec_tag_rhs]
    order = FIRST
    family = LAGRANGE
  []
  [mat_tag_diff]
    order = FIRST
    family = LAGRANGE
  []
  [mat_tag_rhs]
    order = FIRST
    family = LAGRANGE
  []
[]

[Kernels]
  [diff]
    type = Diffusion
    variable = u
    extra_vector_tags = 'tag_diff'
    extra_matrix_tags = 'tag_diff'
  []
  [rhs]
    type = CoefReaction
    variable = u
    extra_vector_tags = 'eigen tag_rhs'
    extra_matrix_tags = 'tag_rhs'
  []
[]

[AuxKernels]
  [vec_tag_diff]
    type = TagVectorAux
    variable = vec_tag_diff
    v = u
    vector_tag = tag_diff
  []
  [vec_tag_rhs]
    type = TagVectorAux
    variable = vec_tag_rhs
    v = u
    vector_tag = tag_rhs
  []

  [mat_tag_diff]
    type = TagVectorAux
    variable = mat_tag_diff
    v = u
    vector_tag = tag_diff
  []
  [mat_tag_rhs]
    type = TagVectorAux
    variable = mat_tag_diff
    v = u
    vector_tag = tag_rhs
  []
[]

[BCs/homogeneous]
  type = DirichletBC
  boundary = 'top right bottom left'
  variable = u
  value = 0
[]

[Problem]
  extra_tag_vectors = 'tag_diff tag_rhs'
  extra_tag_matrices = 'tag_diff tag_rhs'
[]


[Executioner]
  type = Eigenvalue
  solve_type = NEWTON
  eigen_problem_type = GEN_NON_HERMITIAN
[]

[Outputs]
  exodus = true
[]

(test/tests/geomsearch/2d_moving_penetration/pl_test4tt.i)

[GlobalParams]
  order = FIRST
  family = LAGRANGE
[]

[Mesh]
  file = pl_test4.e
  displacements = 'disp_x disp_y'
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
[]

[AuxVariables]
  [./distance]
  [../]
  [./tangential_distance]
  [../]
  [./normal_x]
  [../]
  [./normal_y]
  [../]
  [./closest_point_x]
  [../]
  [./closest_point_y]
  [../]
  [./element_id]
  [../]
  [./side]
  [../]
[]

[Kernels]
  [./diff_x]
    type = Diffusion
    variable = disp_x
  [../]
  [./diff_y]
    type = Diffusion
    variable = disp_y
  [../]
[]

[AuxKernels]
  [./penetrate]
    type = PenetrationAux
    variable = distance
    boundary = 11            #secondary
    paired_boundary = 12     #primary
    tangential_tolerance = 0.1
  [../]

  [./penetrate2]
    type = PenetrationAux
    variable = distance
    boundary = 12            #secondary
    paired_boundary = 11     #primary
    tangential_tolerance = 0.1
  [../]

  [./penetrate3]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 11
    paired_boundary = 12
    quantity = tangential_distance
  [../]

  [./penetrate4]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 12
    paired_boundary = 11
    quantity = tangential_distance
  [../]

  [./penetrate5]
    type = PenetrationAux
    variable = normal_x
    boundary = 11
    paired_boundary = 12
    quantity = normal_x
  [../]

  [./penetrate6]
    type = PenetrationAux
    variable = normal_x
    boundary = 12
    paired_boundary = 11
    quantity = normal_x
  [../]

  [./penetrate7]
    type = PenetrationAux
    variable = normal_y
    boundary = 11
    paired_boundary = 12
    quantity = normal_y
  [../]

  [./penetrate8]
    type = PenetrationAux
    variable = normal_y
    boundary = 12
    paired_boundary = 11
    quantity = normal_y
  [../]

  [./penetrate9]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 11
    paired_boundary = 12
    quantity = closest_point_x
  [../]

  [./penetrate10]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 12
    paired_boundary = 11
    quantity = closest_point_x
  [../]

  [./penetrate11]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 11
    paired_boundary = 12
    quantity = closest_point_y
  [../]

  [./penetrate12]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 12
    paired_boundary = 11
    quantity = closest_point_y
  [../]

  [./penetrate13]
    type = PenetrationAux
    variable = element_id
    boundary = 11
    paired_boundary = 12
    quantity = element_id
  [../]

  [./penetrate14]
    type = PenetrationAux
    variable = element_id
    boundary = 12
    paired_boundary = 11
    quantity = element_id
  [../]

  [./penetrate15]
    type = PenetrationAux
    variable = side
    boundary = 11
    paired_boundary = 12
    quantity = side
  [../]

  [./penetrate16]
    type = PenetrationAux
    variable = side
    boundary = 12
    paired_boundary = 11
    quantity = side
  [../]
[]

[BCs]
  [./b1x]
    type = DirichletBC
    variable = disp_x
    boundary = 1
    value = 0
  [../]

  [./b1y]
    type = DirichletBC
    variable = disp_y
    boundary = 1
    value = 0
  [../]

  [./b2x]
    type = DirichletBC
    variable = disp_x
    boundary = 2
    value = 0
  [../]

  [./b2y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 2
    function = disp_y
  [../]
[]

[Functions]
  [./disp_y]
    type = PiecewiseLinear
    x = '0.0 0.25 0.75 1.0'
    y = '0.0 2.0 -2.0  0.0'
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'
  petsc_options = '-snes_ksp_ew'

  nl_rel_tol = 1e-10
  l_max_its = 10

  start_time = 0.0
  dt = 0.0125
  end_time = 1.0
[]

[Outputs]
  file_base = pl_test4tt_out
  exodus = true
[]

(modules/tensor_mechanics/test/tests/capped_weak_plane/small_deform_cosserat4.i)

# Plastic deformation.  Layered Cosserat with parameters:
# Young = 10.0
# Poisson = 0.25
# layer_thickness = 10
# joint_normal_stiffness = 2.5
# joint_shear_stiffness = 2.0
# These give the following nonzero components of the elasticity tensor:
# E_0000 = E_1111 = 1.156756756757E+01
# E_0011 = E_1100 = 3.855855855856E+00
# E_2222 = E_pp = 8.108108108108E+00
# E_0022 = E_1122 = E_2200 = E_2211 = 2.702702702703E+00
# G = E_0101 = E_0110 = E_1001 = E_1010 = 4
# Gt = E_qq = E_0202 = E_0220 = E_2002 = E_1212 = E_1221 = E_2112 = 3.333333333333E+00
# E_2020 = E_2121 = 3.666666666667E+00
# They give the following nonzero components of the bending rigidity tensor:
# D = 8.888888888889E+02
# B_0101 = B_1010 = 8.080808080808E+00
# B_0110 = B_1001 = -2.020202020202E+00
#
# Applying the following deformation to the zmax surface of a unit cube:
# disp_x = 32*t/Gt
# disp_y = 24*t/Gt
# disp_z = 10*t/E_2222
# but leaving wc_x and wc_y unfixed
# yields the following strains:
# strain_xz = 32*t/Gt - wc_y = 9.6*t - wc_y
# strain_zx = wc_y
# strain_yz = 24*t/Gt + wc_x = 7.2*t + wc_x
# strain_zy = - wc_x
# strain_zz = 10*t/E_2222 = 1.23333333*t
# and all other components, and the curvature, are zero (assuming
# wc is uniform over the cube).
#
# When wc=0, the nonzero components of stress are therefore:
# stress_xx = stress_yy = 3.33333*t
# stress_xz = stress_zx = 32*t
# stress_yz = stress_zy = 24*t
# stress_zz = 10*t
# The moment stress is zero.
# So q = 40*t and p = 10*t
#
# Use tan(friction_angle) = 0.5 and tan(dilation_angle) = E_qq/Epp/2, and cohesion=20,
# the system should return to p=0, q=20, ie stress_zz=0, stress_xz=16,
# stress_yz=12 on the first time step (t=1)
# and
# stress_xx = stress_yy = 0
# and
# stress_zx = 32, and stress_zy = 24.
# This has resulted in a non-symmetric stress tensor, and there is
# zero moment stress, so the system is not in equilibrium.  A
# nonzero wc must therefore be generated.
#
# The obvious choice of wc is such that stress_zx = 16 and
# stress_zy = 12, because then the final returned stress will
# be symmetric.  This gives
# wc_y = - 48
# wc_x = 36
# At t=1, the nonzero components of stress are
# stress_xx = stress_yy = 3.33333
# stress_xz = 32, stress_zx = 16
# stress_yz = 24, stress_zy = 12
# stress_zz = 10*t
# The moment stress is zero.
#
# The returned stress is
# stress_xx = stress_yy = 0
# stress_xz = stress_zx = 16
# stress_yz = stress_zy = 12
# stress_zz = 0
# The total strains are given above.
# Since q returned from 40 to 20, plastic_strain_xz = 9.6/2 = 4.8
# and plastic_strain_yz = 7.2/2 = 3.6.
# Since p returned to zero, all of the total strain_zz is
# plastic, ie plastic_strain_zz = 1.23333
[Mesh]
  type = GeneratedMesh
  dim = 3
  nx = 1
  ny = 1
  nz = 1
  xmin = -0.5
  xmax = 0.5
  ymin = -0.5
  ymax = 0.5
  zmin = -0.5
  zmax = 0.5
[]

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
  Cosserat_rotations = 'wc_x wc_y wc_z'
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
  [./disp_z]
  [../]
  [./wc_x]
  [../]
  [./wc_y]
  [../]
[]

[Kernels]
  [./cx_elastic]
    type = CosseratStressDivergenceTensors
    variable = disp_x
    component = 0
  [../]
  [./cy_elastic]
    type = CosseratStressDivergenceTensors
    variable = disp_y
    component = 1
  [../]
  [./cz_elastic]
    type = CosseratStressDivergenceTensors
    variable = disp_z
    component = 2
  [../]
  [./x_couple]
    type = StressDivergenceTensors
    variable = wc_x
    displacements = 'wc_x wc_y wc_z'
    component = 0
    base_name = couple
  [../]
  [./y_couple]
    type = StressDivergenceTensors
    variable = wc_y
    displacements = 'wc_x wc_y wc_z'
    component = 1
    base_name = couple
  [../]
  [./x_moment]
    type = MomentBalancing
    variable = wc_x
    component = 0
  [../]
  [./y_moment]
    type = MomentBalancing
    variable = wc_y
    component = 1
  [../]
[]

[BCs]
  [./bottomx]
    type = DirichletBC
    variable = disp_x
    boundary = back
    value = 0.0
  [../]
  [./bottomy]
    type = DirichletBC
    variable = disp_y
    boundary = back
    value = 0.0
  [../]
  [./bottomz]
    type = DirichletBC
    variable = disp_z
    boundary = back
    value = 0.0
  [../]

  [./topx]
    type = FunctionDirichletBC
    variable = disp_x
    boundary = front
    function = 32*t/3.333333333333E+00
  [../]
  [./topy]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = front
    function = 24*t/3.333333333333E+00
  [../]
  [./topz]
    type = FunctionDirichletBC
    variable = disp_z
    boundary = front
    function = 10*t/8.108108108108E+00
  [../]
[]

[AuxVariables]
  [./wc_z]
  [../]
  [./stress_xx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_xy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_xz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_zx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_zy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_zz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./couple_stress_xx]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_xy]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_xz]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_yx]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_yy]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_yz]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_zx]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_zy]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./couple_stress_zz]
    family = MONOMIAL
    order = CONSTANT
  [../]
  [./strainp_xx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_xy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_xz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_yx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_yz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_zx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_zy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./strainp_zz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_xx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_xy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_xz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_yx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_yz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_zx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_zy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./straint_zz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./f_shear]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./f_tensile]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./f_compressive]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./intnl_shear]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./intnl_tensile]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./iter]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./ls]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[AuxKernels]
  [./stress_xx]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xx
    index_i = 0
    index_j = 0
  [../]
  [./stress_xy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xy
    index_i = 0
    index_j = 1
  [../]
  [./stress_xz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xz
    index_i = 0
    index_j = 2
  [../]
  [./stress_yx]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yx
    index_i = 1
    index_j = 0
  [../]
  [./stress_yy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yy
    index_i = 1
    index_j = 1
  [../]
  [./stress_yz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yz
    index_i = 1
    index_j = 2
  [../]
  [./stress_zx]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zx
    index_i = 2
    index_j = 0
  [../]
  [./stress_zy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zy
    index_i = 2
    index_j = 1
  [../]
  [./stress_zz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zz
    index_i = 2
    index_j = 2
  [../]
  [./couple_stress_xx]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_xx
    index_i = 0
    index_j = 0
  [../]
  [./couple_stress_xy]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_xy
    index_i = 0
    index_j = 1
  [../]
  [./couple_stress_xz]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_xz
    index_i = 0
    index_j = 2
  [../]
  [./couple_stress_yx]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_yx
    index_i = 1
    index_j = 0
  [../]
  [./couple_stress_yy]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_yy
    index_i = 1
    index_j = 1
  [../]
  [./couple_stress_yz]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_yz
    index_i = 1
    index_j = 2
  [../]
  [./couple_stress_zx]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_zx
    index_i = 2
    index_j = 0
  [../]
  [./couple_stress_zy]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_zy
    index_i = 2
    index_j = 1
  [../]
  [./couple_stress_zz]
    type = RankTwoAux
    rank_two_tensor = couple_stress
    variable = couple_stress_zz
    index_i = 2
    index_j = 2
  [../]
  [./strainp_xx]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_xx
    index_i = 0
    index_j = 0
  [../]
  [./strainp_xy]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_xy
    index_i = 0
    index_j = 1
  [../]
  [./strainp_xz]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_xz
    index_i = 0
    index_j = 2
  [../]
  [./strainp_yx]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_yx
    index_i = 1
    index_j = 0
  [../]
  [./strainp_yy]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_yy
    index_i = 1
    index_j = 1
  [../]
  [./strainp_yz]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_yz
    index_i = 1
    index_j = 2
  [../]
  [./strainp_zx]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_zx
    index_i = 2
    index_j = 0
  [../]
  [./strainp_zy]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_zy
    index_i = 2
    index_j = 1
  [../]
  [./strainp_zz]
    type = RankTwoAux
    rank_two_tensor = plastic_strain
    variable = strainp_zz
    index_i = 2
    index_j = 2
  [../]
  [./straint_xx]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_xx
    index_i = 0
    index_j = 0
  [../]
  [./straint_xy]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_xy
    index_i = 0
    index_j = 1
  [../]
  [./straint_xz]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_xz
    index_i = 0
    index_j = 2
  [../]
  [./straint_yx]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_yx
    index_i = 1
    index_j = 0
  [../]
  [./straint_yy]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_yy
    index_i = 1
    index_j = 1
  [../]
  [./straint_yz]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_yz
    index_i = 1
    index_j = 2
  [../]
  [./straint_zx]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_zx
    index_i = 2
    index_j = 0
  [../]
  [./straint_zy]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_zy
    index_i = 2
    index_j = 1
  [../]
  [./straint_zz]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = straint_zz
    index_i = 2
    index_j = 2
  [../]
  [./f_shear]
    type = MaterialStdVectorAux
    property = plastic_yield_function
    index = 0
    variable = f_shear
  [../]
  [./f_tensile]
    type = MaterialStdVectorAux
    property = plastic_yield_function
    index = 1
    variable = f_tensile
  [../]
  [./f_compressive]
    type = MaterialStdVectorAux
    property = plastic_yield_function
    index = 2
    variable = f_compressive
  [../]
  [./intnl_shear]
    type = MaterialStdVectorAux
    property = plastic_internal_parameter
    index = 0
    variable = intnl_shear
  [../]
  [./intnl_tensile]
    type = MaterialStdVectorAux
    property = plastic_internal_parameter
    index = 1
    variable = intnl_tensile
  [../]
  [./iter]
    type = MaterialRealAux
    property = plastic_NR_iterations
    variable = iter
  [../]
  [./ls]
    type = MaterialRealAux
    property = plastic_linesearch_needed
    variable = ls
  [../]
[]

[Postprocessors]
  [./wc_x]
    type = PointValue
    point = '0 0 0'
    variable = wc_x
  [../]
  [./wc_y]
    type = PointValue
    point = '0 0 0'
    variable = wc_y
  [../]
  [./s_xx]
    type = PointValue
    point = '0 0 0'
    variable = stress_xx
  [../]
  [./s_xy]
    type = PointValue
    point = '0 0 0'
    variable = stress_xy
  [../]
  [./s_xz]
    type = PointValue
    point = '0 0 0'
    variable = stress_xz
  [../]
  [./s_yx]
    type = PointValue
    point = '0 0 0'
    variable = stress_yx
  [../]
  [./s_yy]
    type = PointValue
    point = '0 0 0'
    variable = stress_yy
  [../]
  [./s_yz]
    type = PointValue
    point = '0 0 0'
    variable = stress_yz
  [../]
  [./s_zx]
    type = PointValue
    point = '0 0 0'
    variable = stress_zx
  [../]
  [./s_zy]
    type = PointValue
    point = '0 0 0'
    variable = stress_zy
  [../]
  [./s_zz]
    type = PointValue
    point = '0 0 0'
    variable = stress_zz
  [../]
  [./c_s_xx]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_xx
  [../]
  [./c_s_xy]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_xy
  [../]
  [./c_s_xz]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_xz
  [../]
  [./c_s_yx]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_yx
  [../]
  [./c_s_yy]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_yy
  [../]
  [./c_s_yz]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_yz
  [../]
  [./c_s_zx]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_zx
  [../]
  [./c_s_zy]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_zy
  [../]
  [./c_s_zz]
    type = PointValue
    point = '0 0 0'
    variable = couple_stress_zz
  [../]
  [./strainp_xx]
    type = PointValue
    point = '0 0 0'
    variable = strainp_xx
  [../]
  [./strainp_xy]
    type = PointValue
    point = '0 0 0'
    variable = strainp_xy
  [../]
  [./strainp_xz]
    type = PointValue
    point = '0 0 0'
    variable = strainp_xz
  [../]
  [./strainp_yx]
    type = PointValue
    point = '0 0 0'
    variable = strainp_yx
  [../]
  [./strainp_yy]
    type = PointValue
    point = '0 0 0'
    variable = strainp_yy
  [../]
  [./strainp_yz]
    type = PointValue
    point = '0 0 0'
    variable = strainp_yz
  [../]
  [./strainp_zx]
    type = PointValue
    point = '0 0 0'
    variable = strainp_zx
  [../]
  [./strainp_zy]
    type = PointValue
    point = '0 0 0'
    variable = strainp_zy
  [../]
  [./strainp_zz]
    type = PointValue
    point = '0 0 0'
    variable = strainp_zz
  [../]
  [./straint_xx]
    type = PointValue
    point = '0 0 0'
    variable = straint_xx
  [../]
  [./straint_xy]
    type = PointValue
    point = '0 0 0'
    variable = straint_xy
  [../]
  [./straint_xz]
    type = PointValue
    point = '0 0 0'
    variable = straint_xz
  [../]
  [./straint_yx]
    type = PointValue
    point = '0 0 0'
    variable = straint_yx
  [../]
  [./straint_yy]
    type = PointValue
    point = '0 0 0'
    variable = straint_yy
  [../]
  [./straint_yz]
    type = PointValue
    point = '0 0 0'
    variable = straint_yz
  [../]
  [./straint_zx]
    type = PointValue
    point = '0 0 0'
    variable = straint_zx
  [../]
  [./straint_zy]
    type = PointValue
    point = '0 0 0'
    variable = straint_zy
  [../]
  [./straint_zz]
    type = PointValue
    point = '0 0 0'
    variable = straint_zz
  [../]
  [./f_shear]
    type = PointValue
    point = '0 0 0'
    variable = f_shear
  [../]
  [./f_tensile]
    type = PointValue
    point = '0 0 0'
    variable = f_tensile
  [../]
  [./f_compressive]
    type = PointValue
    point = '0 0 0'
    variable = f_compressive
  [../]
  [./intnl_shear]
    type = PointValue
    point = '0 0 0'
    variable = intnl_shear
  [../]
  [./intnl_tensile]
    type = PointValue
    point = '0 0 0'
    variable = intnl_tensile
  [../]
  [./iter]
    type = PointValue
    point = '0 0 0'
    variable = iter
  [../]
  [./ls]
    type = PointValue
    point = '0 0 0'
    variable = ls
  [../]
[]


[UserObjects]
  [./coh]
    type = TensorMechanicsHardeningConstant
    value = 20
  [../]
  [./tanphi]
    type = TensorMechanicsHardeningConstant
    value = 0.5
  [../]
  [./tanpsi]
    type = TensorMechanicsHardeningConstant
    value = 2.055555555556E-01
  [../]
  [./t_strength]
    type = TensorMechanicsHardeningConstant
    value = 100
  [../]
  [./c_strength]
    type = TensorMechanicsHardeningConstant
    value = 100
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeLayeredCosseratElasticityTensor
    young = 10.0
    poisson = 0.25
    layer_thickness = 10.0
    joint_normal_stiffness = 2.5
    joint_shear_stiffness = 2.0
  [../]
  [./strain]
    type = ComputeCosseratIncrementalSmallStrain
  [../]
  [./admissible]
    type = ComputeMultipleInelasticCosseratStress
    inelastic_models = stress
    perform_finite_strain_rotations = false
  [../]
  [./stress]
    type = CappedWeakPlaneCosseratStressUpdate
    cohesion = coh
    tan_friction_angle = tanphi
    tan_dilation_angle = tanpsi
    tensile_strength = t_strength
    compressive_strength = c_strength
    tip_smoother = 0
    smoothing_tol = 0
    yield_function_tol = 1E-5
  [../]
[]

[Preconditioning]
  [./andy]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  solve_type = 'NEWTON'
  end_time = 1
  dt = 1
  type = Transient
[]

[Outputs]
  file_base = small_deform_cosserat4
  csv = true
[]

(modules/tensor_mechanics/test/tests/crystal_plasticity/monolithic_material_based/crysp_substep.i)

[Mesh]
  type = GeneratedMesh
  dim = 3
  elem_type = HEX8
  displacements = 'ux uy uz'
[]

[Variables]
  [./ux]
    block = 0
  [../]
  [./uy]
    block = 0
  [../]
  [./uz]
    block = 0
  [../]
[]

[AuxVariables]
  [./stress_zz]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
  [./fp_zz]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
  [./rotout]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
  [./e_zz]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
  [./gss1]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
[]

[Functions]
  [./tdisp]
    type = ParsedFunction
    value = 0.01*t
  [../]
[]

[Kernels]
  [./TensorMechanics]
    displacements = 'ux uy uz'
    use_displaced_mesh = true
  [../]
[]

[AuxKernels]
  [./stress_zz]
    type = RankTwoAux
    variable = stress_zz
    rank_two_tensor = stress
    index_j = 2
    index_i = 2
    execute_on = timestep_end
    block = 0
  [../]
  [./fp_zz]
    type = RankTwoAux
    variable = fp_zz
    rank_two_tensor = fp
    index_j = 2
    index_i = 2
    execute_on = timestep_end
    block = 0
  [../]
  [./e_zz]
    type = RankTwoAux
    variable = e_zz
    rank_two_tensor = lage
    index_j = 2
    index_i = 2
    execute_on = timestep_end
    block = 0
  [../]
  [./gss1]
    type = MaterialStdVectorAux
    variable = gss1
    property = gss
    index = 0
    execute_on = timestep_end
    block = 0
  [../]
[]

[BCs]
  [./symmy]
    type = DirichletBC
    variable = uy
    boundary = bottom
    value = 0
  [../]
  [./symmx]
    type = DirichletBC
    variable = ux
    boundary = left
    value = 0
  [../]
  [./symmz]
    type = DirichletBC
    variable = uz
    boundary = back
    value = 0
  [../]
  [./tdisp]
    type = FunctionDirichletBC
    variable = uz
    boundary = front
    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
    gen_random_stress_flag = false
    maximum_substep_iteration = 2
  [../]
  [./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
  [../]
  [./strain]
    type = ComputeFiniteStrain
    block = 0
    displacements = 'ux uy uz'
  [../]
[]

[Postprocessors]
  [./stress_zz]
    type = ElementAverageValue
    variable = stress_zz
    block = 'ANY_BLOCK_ID 0'
  [../]
  [./fp_zz]
    type = ElementAverageValue
    variable = fp_zz
    block = 'ANY_BLOCK_ID 0'
  [../]
  [./e_zz]
    type = ElementAverageValue
    variable = e_zz
    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 = 0.5
  dtmax = 10.0
  dtmin = 0.5

  num_steps = 3
[]

[Outputs]
  file_base = crysp_substep_out
  exodus = true
  csv = true
  gnuplot = true
[]

(modules/porous_flow/test/tests/thermal_conductivity/ThermalCondPorosity01.i)

# Trivial test of PorousFlowThermalConductivityFromPorosity
# Porosity = 0.1
# Solid thermal conductivity = 3
# Fluid thermal conductivity = 2
# Expected porous medium thermal conductivity = 3 * (1 - 0.1) + 2 * 0.1 = 2.9

[Mesh]
  type = GeneratedMesh
  dim = 3
  xmin = 0
  xmax = 1
  ymin = 0
  ymax = 1
  zmin = -1
  zmax = 0
  nx = 1
  ny = 1
  nz = 1
  # This test uses ElementalVariableValue postprocessors on specific
  # elements, so element numbering needs to stay unchanged
  allow_renumbering = false
[]

[GlobalParams]
  PorousFlowDictator = dictator
[]

[Modules]
  [FluidProperties]
    [simple_fluid]
      type = SimpleFluidProperties
    []
  []
[]

[Variables]
  [temp]
    initial_condition = 1
  []
  [pp]
    initial_condition = 0
  []
[]

[Kernels]
  [heat_conduction]
    type = PorousFlowHeatConduction
    variable = temp
  []
  [dummy]
    type = Diffusion
    variable = pp
  []
[]

[BCs]
  [temp]
    type = DirichletBC
    variable = temp
    boundary = 'front back'
    value = 1
  []
  [pp]
    type = DirichletBC
    variable = pp
    boundary = 'front back'
    value = 0
  []
[]

[AuxVariables]
  [lambda_x]
    order = CONSTANT
    family = MONOMIAL
  []
  [lambda_y]
    order = CONSTANT
    family = MONOMIAL
  []
  [lambda_z]
    order = CONSTANT
    family = MONOMIAL
  []
[]

[AuxKernels]
  [lambda_x]
    type = MaterialRealTensorValueAux
    property = PorousFlow_thermal_conductivity_qp
    row = 0
    column = 0
    variable = lambda_x
  []
  [lambda_y]
    type = MaterialRealTensorValueAux
    property = PorousFlow_thermal_conductivity_qp
    row = 1
    column = 1
    variable = lambda_y
  []
  [lambda_z]
    type = MaterialRealTensorValueAux
    property = PorousFlow_thermal_conductivity_qp
    row = 2
    column = 2
    variable = lambda_z
  []
[]

[Postprocessors]
  [lambda_x]
    type = ElementalVariableValue
    elementid = 0
    variable = lambda_x
    execute_on = 'timestep_end'
  []
  [lambda_y]
    type = ElementalVariableValue
    elementid = 0
    variable = lambda_y
    execute_on = 'timestep_end'
  []
  [lambda_z]
    type = ElementalVariableValue
    elementid = 0
    variable = lambda_z
    execute_on = 'timestep_end'
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'pp temp'
    number_fluid_phases = 1
    number_fluid_components = 1
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
    temperature = temp
  []
  [ppss_qp]
    type = PorousFlow1PhaseFullySaturated
    porepressure = pp
  []
  [simple_fluid]
    type = PorousFlowSingleComponentFluid
    fp = simple_fluid
    phase = 0
  []
  [porosity_qp]
    type = PorousFlowPorosityConst
    porosity = 0.1
  []
  [lambda]
    type = PorousFlowThermalConductivityFromPorosity
    lambda_s = '3 0 0  0 3 0  0 0 3'
    lambda_f = '2 0 0  0 2 0  0 0 2'
  []
[]

[Preconditioning]
  [andy]
    type = SMP
    full = true
  []
[]

[Executioner]
  solve_type = Newton
  type = Steady
[]

[Outputs]
  file_base = ThermalCondPorosity01
  csv = true
  execute_on = 'timestep_end'
[]

(modules/tensor_mechanics/test/tests/crystal_plasticity/monolithic_material_based/crysp_user_object.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
  [../]
[]

[Functions]
  [./tdisp]
    type = ParsedFunction
    value = 0.01*t
  [../]
[]

[UserObjects]
  [./prop_read]
    type = PropertyReadFile
    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
  [../]
[]

[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_user_object_out
  exodus = true
[]

[Kernels]
  [./TensorMechanics]
    displacements = 'disp_x disp_y'
    use_displaced_mesh = true
  [../]
[]

(test/tests/postprocessors/avg_nodal_var_value/avg_nodal_var_value_ts_begin.i)

[Mesh]
  file = square-2x2-nodeids.e
[]

[Variables]
  active = 'u v'

  [./u]
    order = SECOND
    family = LAGRANGE
  [../]

  [./v]
    order = SECOND
    family = LAGRANGE
  [../]
[]

[Functions]
  active = 'force_fn exact_fn left_bc'

  [./force_fn]
    type = ParsedFunction
    value = '1-x*x+2*t'
  [../]

  [./exact_fn]
    type = ParsedFunction
    value = '(1-x*x)*t'
  [../]

  [./left_bc]
    type = ParsedFunction
    value = t
  [../]
[]

[Kernels]
  active = '
    time_u diff_u ffn_u
    time_v diff_v'

  [./time_u]
    type = TimeDerivative
    variable = u
  [../]

  [./diff_u]
    type = Diffusion
    variable = u
  [../]

  [./ffn_u]
    type = BodyForce
    variable = u
    function = force_fn
  [../]

  [./time_v]
    type = TimeDerivative
    variable = v
  [../]

  [./diff_v]
    type = Diffusion
    variable = v
  [../]
[]

[BCs]
  active = 'all_u left_v right_v'

  [./all_u]
    type = FunctionDirichletBC
    variable = u
    boundary = '1'
    function = exact_fn
  [../]

  [./left_v]
    type = FunctionDirichletBC
    variable = v
    boundary = '3'
    function = left_bc
  [../]

  [./right_v]
    type = DirichletBC
    variable = v
    boundary = '2'
    value = 0
  [../]
[]

[Postprocessors]
  [./l2]
    type = ElementL2Error
    variable = u
    function = exact_fn
  [../]

  [./node1]
    type = AverageNodalVariableValue
    variable = u
    boundary = 10
    execute_on = TIMESTEP_BEGIN
  [../]

  [./node4]
    type = AverageNodalVariableValue
    variable = v
    boundary = 13
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'

  dt = 0.1
  start_time = 0
  end_time = 1
[]

[Outputs]
  execute_on = 'timestep_end'
  file_base = out_avg_nodal_var_value_ts_begin
  exodus = true
[]

(test/tests/time_integrators/newmark-beta/newmark_beta_inactive_steps.i)

###########################################################
# This is a simple test with a time-dependent problem
# demonstrating the use of the TimeIntegrator system.
#
# Testing that the active_time parameter works as intended.
#
###########################################################

[Mesh]
  type = GeneratedMesh
  dim = 2
  xmin = -1
  xmax = 1
  ymin = -1
  ymax = 1
  nx = 1
  ny = 1
[]

[Variables]
  [u]
  []
[]

[Functions]
  [forcing_fn]
    type = PiecewiseLinear
    x = '0.0 0.1 0.6'
    y = '0.0 1.0 1.0'
  []
[]

[Kernels]
  [ie]
    type = TimeDerivative
    variable = u
  []

  [diff]
    type = Diffusion
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = 'left'
    value = 0
  []
  [right]
    type = FunctionDirichletBC
    variable = u
    boundary = 'right'
    function = forcing_fn
  []
[]

[Executioner]
  type = Transient
  start_time = 0.0
  num_steps = 6
  dt = 0.1
  [TimeIntegrator]
    type = NewmarkBeta
    inactive_tsteps = 1
  []
[]

[Postprocessors]
  [udot]
    type = ElementAverageTimeDerivative
    variable = u
  []
  [udotdot]
    type = ElementAverageSecondTimeDerivative
    variable = u
  []
  [u]
    type = ElementAverageValue
    variable = u
  []
[]

[Outputs]
  csv = true
[]

(test/tests/transfers/multiapp_copy_transfer/constant_monomial_from_sub/sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[AuxVariables]
  [./aux]
    family = MONOMIAL
    order = CONSTANT
  [../]
[]

[AuxKernels]
  [./aux]
    type = FunctionAux
    variable = aux
    execute_on = initial
    function = 10*x*y
  [../]
[]

[Problem]
  type = FEProblem
  solve = false
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 1
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 2
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 1
  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  hide = 'u'
  exodus = true
[]

(modules/heat_conduction/test/tests/verify_against_analytical/2d_steady_state.i)

# This test solves a 2D steady state heat equation
# The error is found by comparing to the analytical solution

# Note that the thermal conductivity, specific heat, and density in this problem
# Are set to 1, and need to be changed to the constants of the material being
# Analyzed

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 30
  ny = 30
  xmax = 2
  ymax = 2
[]

[Variables]
  [./T]
  [../]
[]

[Kernels]
  [./HeatDiff]
    type = HeatConduction
    variable = T
  [../]
[]

[BCs]
  [./zero]
    type = DirichletBC
    variable = T
    boundary = 'left right bottom'
    value = 0
  [../]
  [./top]
    type = FunctionDirichletBC
    variable = T
    boundary = top
    function = '10*sin(pi*x*0.5)'
  [../]
[]

[Materials]
  [./properties]
    type = GenericConstantMaterial
    prop_names = 'thermal_conductivity specific_heat density'
    prop_values = '1 1 1'
  [../]
[]

[Postprocessors]
  [./nodal_error]
    type = NodalL2Error
    function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
    variable = T
  [../]
  [./elemental_error]
    type = ElementL2Error
    function = '10/(sinh(pi))*sin(pi*x*0.5)*sinh(pi*y*0.5)'
    variable = T
  [../]
[]

[Executioner]
  type = Steady
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/lagrangian/updated/cross_material/convergence/plastic_j2.i)

# Simple 3D test

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
  large_kinematics = false
[]

[Variables]
  [disp_x]
  []
  [disp_y]
  []
  [disp_z]
  []
[]

[Mesh]
  [msh]
    type = GeneratedMeshGenerator
    dim = 3
    nx = 4
    ny = 4
    nz = 4
  []
[]

[ICs]
  [disp_x]
    type = RandomIC
    variable = disp_x
    min = -0.02
    max = 0.02
  []
  [disp_y]
    type = RandomIC
    variable = disp_y
    min = -0.02
    max = 0.02
  []
  [disp_z]
    type = RandomIC
    variable = disp_z
    min = -0.02
    max = 0.02
  []
[]

[Kernels]
  [sdx]
    type = UpdatedLagrangianStressDivergence
    variable = disp_x
    component = 0
    use_displaced_mesh = false
  []
  [sdy]
    type = UpdatedLagrangianStressDivergence
    variable = disp_y
    component = 1
    use_displaced_mesh = false
  []
  [sdz]
    type = UpdatedLagrangianStressDivergence
    variable = disp_z
    component = 2
    use_displaced_mesh = false
  []
[]

[Functions]
  [pullx]
    type = ParsedFunction
    value = '4000 * t'
  []
  [pully]
    type = ParsedFunction
    value = '-2000 * t'
  []
  [pullz]
    type = ParsedFunction
    value = '3000 * t'
  []
[]

[BCs]
  [leftx]
    type = DirichletBC
    preset = true
    boundary = left
    variable = disp_x
    value = 0.0
  []
  [lefty]
    type = DirichletBC
    preset = true
    boundary = left
    variable = disp_y
    value = 0.0
  []
  [leftz]
    type = DirichletBC
    preset = true
    boundary = left
    variable = disp_z
    value = 0.0
  []
  [pull_x]
    type = FunctionNeumannBC
    boundary = right
    variable = disp_x
    function = pullx
  []
  [pull_y]
    type = FunctionNeumannBC
    boundary = top
    variable = disp_y
    function = pully
  []
  [pull_z]
    type = FunctionNeumannBC
    boundary = right
    variable = disp_z
    function = pullz
  []
[]

[UserObjects]
  [./str]
    type = TensorMechanicsHardeningPowerRule
    value_0 = 100.0
    epsilon0 = 1.0
    exponent = 1.0
  [../]
  [./j2]
    type = TensorMechanicsPlasticJ2
    yield_strength = str
    yield_function_tolerance = 1E-3
    internal_constraint_tolerance = 1E-9
  [../]
[]

[Materials]
  [elastic_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 100000.0
    poissons_ratio = 0.3
  []
  [compute_stress]
    type = ComputeLagrangianWrappedStress
  []
  [compute_stress_base]
    type = ComputeMultiPlasticityStress
    plastic_models = j2
    ep_plastic_tolerance = 1E-9
  []
  [compute_strain]
    type = ComputeLagrangianStrain
  []
[]

[Preconditioning]
  [smp]
    type = SMP
    full = true
  []
[]

[Executioner]
  type = Transient

  solve_type = 'newton'
  line_search = none

  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'

  l_max_its = 2
  l_tol = 1e-14
  nl_max_its = 15
  nl_rel_tol = 1e-8
  nl_abs_tol = 1e-10

  start_time = 0.0
  dt = 1.0
  dtmin = 1.0
  end_time = 1.0
[]

(modules/tensor_mechanics/test/tests/lagrangian/total/homogenization/small-tests/2d-mixed.i)

# 2D with mixed conditions on stress/strain

[GlobalParams]
  displacements = 'disp_x disp_y'
  large_kinematics = false
  constraint_types = 'stress strain stress'
  ndim = 2
  macro_gradient = hvar
[]

[Mesh]
  [base]
    type = FileMeshGenerator
    file = '2d.exo'
  []

  [sidesets]
    type = SideSetsFromNormalsGenerator
    input = base
    normals = '-1 0 0
                1 0 0
                0 -1 0
                0 1 0'
    fixed_normal = true
    new_boundary = 'left right bottom top'
  []
[]

[Variables]
  [disp_x]
  []
  [disp_y]
  []
  [hvar]
    family = SCALAR
    order = THIRD
  []
[]

[AuxVariables]
  [sxx]
    family = MONOMIAL
    order = CONSTANT
  []
  [syy]
    family = MONOMIAL
    order = CONSTANT
  []
  [sxy]
    family = MONOMIAL
    order = CONSTANT
  []
  [exx]
    family = MONOMIAL
    order = CONSTANT
  []
  [eyy]
    family = MONOMIAL
    order = CONSTANT
  []
  [exy]
    family = MONOMIAL
    order = CONSTANT
  []
[]

[AuxKernels]
  [sxx]
    type = RankTwoAux
    variable = sxx
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 0
  []
  [syy]
    type = RankTwoAux
    variable = syy
    rank_two_tensor = pk1_stress
    index_i = 1
    index_j = 1
  []
  [sxy]
    type = RankTwoAux
    variable = sxy
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 1
  []
  [exx]
    type = RankTwoAux
    variable = exx
    rank_two_tensor = mechanical_strain
    index_i = 0
    index_j = 0
  []
  [eyy]
    type = RankTwoAux
    variable = eyy
    rank_two_tensor = mechanical_strain
    index_i = 1
    index_j = 1
  []
  [exy]
    type = RankTwoAux
    variable = exy
    rank_two_tensor = mechanical_strain
    index_i = 0
    index_j = 1
  []
[]

[UserObjects]
  [integrator]
    type = HomogenizationConstraintIntegral
    targets = 'stress11 strain22 stress12'
    execute_on = 'initial linear'
  []
[]

[Kernels]
  [sdx]
    type = HomogenizedTotalLagrangianStressDivergence
    variable = disp_x
    component = 0
  []
  [sdy]
    type = HomogenizedTotalLagrangianStressDivergence
    variable = disp_y
    component = 1
  []
[]

[ScalarKernels]
  [enforce]
    type = HomogenizationConstraintScalarKernel
    variable = hvar
    integrator = integrator
  []
[]

[Functions]
  [stress11]
    type = ParsedFunction
    value = '400*t'
  []
  [strain22]
    type = ParsedFunction
    value = '-2.0e-2*t'
  []
  [stress12]
    type = ParsedFunction
    value = '100*t'
  []
[]

[BCs]
  [Periodic]
    [x]
      variable = disp_x
      auto_direction = 'x y'
    []
    [y]
      variable = disp_y
      auto_direction = 'x y'
    []
  []

  [fix1_x]
    type = DirichletBC
    boundary = "fix1"
    variable = disp_x
    value = 0
  []
  [fix1_y]
    type = DirichletBC
    boundary = "fix1"
    variable = disp_y
    value = 0
  []

  [fix2_y]
    type = DirichletBC
    boundary = "fix2"
    variable = disp_y
    value = 0
  []
[]

[Materials]
  [elastic_tensor_1]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 100000.0
    poissons_ratio = 0.3
    block = '1'
  []
  [elastic_tensor_2]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 120000.0
    poissons_ratio = 0.21
    block = '2'
  []
  [elastic_tensor_3]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 80000.0
    poissons_ratio = 0.4
    block = '3'
  []
  [compute_stress]
    type = ComputeLagrangianLinearElasticStress
  []
  [compute_strain]
    type = ComputeLagrangianStrain
    homogenization_gradient_names = 'homogenization_gradient'
  []
  [compute_homogenization_gradient]
    type = ComputeHomogenizedLagrangianStrain
  []
[]

[Preconditioning]
  [smp]
    type = SMP
    full = true
  []
[]

[Postprocessors]
  [sxx]
    type = ElementAverageValue
    variable = sxx
    execute_on = 'initial timestep_end'
  []
  [syy]
    type = ElementAverageValue
    variable = syy
    execute_on = 'initial timestep_end'
  []
  [sxy]
    type = ElementAverageValue
    variable = sxy
    execute_on = 'initial timestep_end'
  []
  [exx]
    type = ElementAverageValue
    variable = exx
    execute_on = 'initial timestep_end'
  []
  [eyy]
    type = ElementAverageValue
    variable = eyy
    execute_on = 'initial timestep_end'
  []
  [exy]
    type = ElementAverageValue
    variable = exy
    execute_on = 'initial timestep_end'
  []
[]

[Executioner]
  type = Transient

  solve_type = 'newton'
  line_search = none

  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'

  l_max_its = 2
  l_tol = 1e-14
  nl_max_its = 30
  nl_rel_tol = 1e-8
  nl_abs_tol = 1e-10

  start_time = 0.0
  dt = 0.2
  dtmin = 0.2
  end_time = 1.0
[]

[Outputs]
  exodus = false
  csv = true
[]

(modules/heat_conduction/test/tests/radiation_transfer_action/radiative_transfer_action_external_boundary.i)

[Problem]
  kernel_coverage_check = false
[]

[Mesh]
  [./cmg]
    type = CartesianMeshGenerator
    dim = 2
    dx = '1 1.3 1.9'
    ix = '3 3 3'
    dy = '6'
    iy = '9'
    subdomain_id = '0 1 2'
  [../]

    [./inner_left]
      type = SideSetsBetweenSubdomainsGenerator
      input = cmg
      primary_block = 0
      paired_block = 1
      new_boundary = 'inner_left'
    [../]

    [./inner_right]
      type = SideSetsBetweenSubdomainsGenerator
      input = inner_left
      primary_block = 2
      paired_block = 1
      new_boundary = 'inner_right'
    [../]

    [./inner_top]
      type = ParsedGenerateSideset
      combinatorial_geometry = 'abs(y - 6) < 1e-10'
      normal = '0 1 0'
      included_subdomain_ids = 1
      new_sideset_name = 'inner_top'
      input = 'inner_right'
    [../]

    [./inner_bottom]
      type = ParsedGenerateSideset
      combinatorial_geometry = 'abs(y) < 1e-10'
      normal = '0 -1 0'
      included_subdomain_ids = 1
      new_sideset_name = 'inner_bottom'
      input = 'inner_top'
    [../]

    [./rename]
      type = RenameBlockGenerator
      old_block = '2'
      new_block = '0'
      input = inner_bottom
    [../]
[]

[Variables]
  [./temperature]
    block = 0
  [../]
[]

[Kernels]
  [./heat_conduction]
    type = HeatConduction
    variable = temperature
    block = 0
    diffusion_coefficient = 5
  [../]
[]

[GrayDiffuseRadiation]
  [./cavity]
    boundary = '4 5 6 7'
    emissivity = '0.9 0.8 0.4 1'
    n_patches = '2 2 2 3'
    partitioners = 'centroid centroid centroid centroid'
    centroid_partitioner_directions = 'x y y x'
    temperature = temperature
    adiabatic_boundary = '7'
    fixed_temperature_boundary = '6'
    fixed_boundary_temperatures = '800'
    view_factor_calculator = analytical
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = temperature
    boundary = left
    value = 1000
  [../]

  [./right]
    type = DirichletBC
    variable = temperature
    boundary = right
    value = 300
  [../]
[]

[Postprocessors]
  [./average_T_inner_right]
    type = SideAverageValue
    variable = temperature
    boundary = inner_right
  [../]
[]

[Executioner]
  type = Steady
[]

[Outputs]
  exodus = true
[]

(test/tests/transfers/multiapp_variable_value_sample_transfer/master_quad.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[AuxVariables]
  [./master_aux]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[Functions]
  [./func]
    type = ParsedFunction
    value = x*y*t
  [../]
[]

[Kernels]
  [./diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  [../]
  [./time]
    type = TimeDerivative
    variable = u
  [../]
[]

[AuxKernels]
  [./func_aux]
    type = FunctionAux
    variable = master_aux
    function = func
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 5
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
[]

[MultiApps]
  [./quad]
    type = TransientMultiApp
    app_type = MooseTestApp
    positions = '0.05 0.05 0 0.95 0.05 0 0.05 0.95 0 0.95 0.95 0'
    input_files = quad_sub.i
  [../]
[]

[Transfers]
  [./master_to_sub]
    type = MultiAppVariableValueSamplePostprocessorTransfer
    to_multi_app = quad
    source_variable = master_aux
    postprocessor = pp
  [../]
[]

(test/tests/outputs/displacement/displacement_transient_test.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  xmin = -1
  xmax = 1
  ymin = -1
  ymax = 1
  nx = 5
  ny = 5
  elem_type = QUAD4

  displacements = 'u v'
[]

[Functions]
  [./right_u]
    type = ParsedFunction
    value = 0.1*t
  [../]

  [./fn_v]
    type = ParsedFunction
    value = (x+1)*y*0.1*t
  [../]
[]

[Variables]
  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
  [./v]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  [./td_u]
    type = TimeDerivative
    variable = u
  [../]
  [./diff_u]
    type = Diffusion
    variable = u
  [../]

  [./td_v]
    type = TimeDerivative
    variable = v
  [../]
  [./diff_v]
    type = Diffusion
    variable = v
  [../]
[]

[BCs]
  [./left_u]
    type = DirichletBC
    variable = u
    boundary = 3
    value = 0
  [../]
  [./right_u]
    type = FunctionDirichletBC
    variable = u
    boundary = 1
    function = right_u
  [../]

  [./left_v]
    type = FunctionDirichletBC
    variable = v
    boundary = '0 2'
    function = fn_v
  [../]
[]

[Executioner]
  type = Transient

  dt = 0.1
  start_time = 0
  num_steps = 10


  solve_type = 'PJFNK'
[]

[Outputs]
  [./out_displaced]
    type = Exodus
    use_displaced = true
  [../]
[]

(test/tests/outputs/format/output_test_nemesis.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 2
  nz = 0
  zmin = 0
  zmax = 0
  elem_type = QUAD4
[]

[Variables]
  active = 'u'

  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  active = 'diff'

  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  active = 'left right'

  [./left]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = 3
    value = 1
  [../]
[]

[Postprocessors]
  [./avg_block]
    type = ElementAverageValue
    variable = u
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'
[]

[Outputs]
  file_base = out
  nemesis = 1
[]

(test/tests/materials/has_material/has_block_prop.i)

[Mesh]
  type = FileMesh
  file = rectangle.e
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  active = 'u_diff'
  [./u_diff]
    type = MatCoefDiffusion
    variable = u
    block = '1 2'
    conductivity = k
  [../]
[]

[BCs]
  [./left]
    type = NeumannBC
    variable = u
    boundary = 1
    value = 1
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = 2
    value = 0
  [../]
[]

[Materials]
  [./right]
    type = GenericConstantMaterial
    block = 2
    prop_names = 'k k_right'
    prop_values = '1 2'
  [../]
  [./left]
    type = GenericConstantMaterial
    block = 1
    prop_names = 'k'
    prop_values = '0.1'
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
[]

[Outputs]
  execute_on = 'timestep_end'
  exodus = true
[]

(modules/navier_stokes/test/tests/auxkernels/reynolds-number-functor-aux/fe.i)

rho=1
mu=1

[GlobalParams]
  gravity = '0 0 0'
  pspg = true
[]

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 10
    ny = 10
  []
  [corner_node]
    type = ExtraNodesetGenerator
    new_boundary = 'pinned_node'
    nodes = '0'
    input = gen
  []
[]

[AuxVariables]
  [Reynolds]
    family = MONOMIAL
    order = CONSTANT
  []
[]

[AuxKernels]
  [Reynolds]
    type = ReynoldsNumberFunctorAux
    variable = Reynolds
    speed = speed
    rho = ${rho}
    mu = ${mu}
  []
[]

[Variables]
  [vel_x]
  []
  [vel_y]
  []
  [p]
  []
[]

[Kernels]
  # mass
  [mass]
    type = INSMass
    variable = p
    u = vel_x
    v = vel_y
    pressure = p
  []
  # x-momentum, space
  [x_momentum_space]
    type = INSMomentumLaplaceForm
    variable = vel_x
    u = vel_x
    v = vel_y
    pressure = p
    component = 0
  []
  # y-momentum, space
  [y_momentum_space]
    type = INSMomentumLaplaceForm
    variable = vel_y
    u = vel_x
    v = vel_y
    pressure = p
    component = 1
  []
[]

[BCs]
  [x_no_slip]
    type = DirichletBC
    variable = vel_x
    boundary = 'bottom right left'
    value = 0.0
  []
  [lid]
    type = FunctionDirichletBC
    variable = vel_x
    boundary = 'top'
    function = 'lid_function'
  []
  [y_no_slip]
    type = DirichletBC
    variable = vel_y
    boundary = 'bottom right top left'
    value = 0.0
  []
  [pressure_pin]
    type = DirichletBC
    variable = p
    boundary = 'pinned_node'
    value = 0
  []
[]

[Materials]
  [const]
    type = GenericConstantMaterial
    block = 0
    prop_names = 'rho mu'
    prop_values = '${rho}  ${mu}'
  []
  [speed]
    type = ADVectorMagnitudeFunctorMaterial
    x_functor = vel_x
    y_functor = vel_y
    vector_magnitude_name = speed
  []
[]

[Functions]
  [lid_function]
    # We pick a function that is exactly represented in the velocity
    # space so that the Dirichlet conditions are the same regardless
    # of the mesh spacing.
    type = ParsedFunction
    value = '4*x*(1-x)'
  []
[]

[Preconditioning]
  [SMP]
    type = SMP
    full = true
    solve_type = 'NEWTON'
  []
[]

[Executioner]
  type = Steady
  petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type'
  petsc_options_value = 'asm      2               lu'
  line_search = 'none'
  nl_rel_tol = 1e-12
[]

[Outputs]
  exodus = true
[]

(modules/heat_conduction/test/tests/gap_heat_transfer_mortar_action/modular_gap_heat_transfer_mortar_displaced_radiation_conduction_action.i)

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Mesh]
  [file]
    type = FileMeshGenerator
    file = 2blk-gap.e
  []
  allow_renumbering = false
[]

[Problem]
  kernel_coverage_check = false
  material_coverage_check = false
[]

[Variables]
  [temp]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
  [disp_x]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
  [disp_y]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
[]

[Materials]
  [left]
    type = ADHeatConductionMaterial
    block = 1
    thermal_conductivity = 0.01
    specific_heat = 1
  []

  [right]
    type = ADHeatConductionMaterial
    block = 2
    thermal_conductivity = 0.005
    specific_heat = 1
  []
[]

[Kernels]
  [hc_displaced_block]
    type = ADHeatConduction
    variable = temp
    use_displaced_mesh = true
    block = '1'
  []
  [hc_undisplaced_block]
    type = ADHeatConduction
    variable = temp
    use_displaced_mesh = false
    block = '2'
  []
  [disp_x]
    type = Diffusion
    variable = disp_x
    block = '1 2'
  []
  [disp_y]
    type = Diffusion
    variable = disp_y
    block = '1 2'
  []
[]

[MortarGapHeatTransfer]
  [mortar_heat_transfer]
   temperature = temp

   primary_emissivity = 1.0
   secondary_emissivity = 1.0
   boundary = 100
   use_displaced_mesh = true
   gap_conductivity = 0.02

   primary_boundary = 100
   secondary_boundary = 101
   gap_flux_options = 'CONDUCTION RADIATION'
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = temp
    boundary = 'left'
    value = 100
  []

  [right]
    type = DirichletBC
    variable = temp
    boundary = 'right'
    value = 0
  []

  [left_disp_x]
    type = DirichletBC
    preset = false
    variable = disp_x
    boundary = 'left'
    value = .1
  []
  [right_disp_x]
    type = DirichletBC
    preset = false
    variable = disp_x
    boundary = 'right'
    value = 0
  []
  [bottom_disp_y]
    type = DirichletBC
    preset = false
    variable = disp_y
    boundary = 'bottom'
    value = 0
  []
[]

[Preconditioning]
  [fmp]
    type = SMP
    full = true
    solve_type = 'NEWTON'
  []
[]

[Executioner]
  type = Steady
  nl_rel_tol = 1e-11
  nl_abs_tol = 1.0e-10
[]

[VectorPostprocessors]
  [NodalTemperature]
    type = NodalValueSampler
    sort_by = id
    boundary = '100 101'
    variable = 'temp'
  []
[]

[Outputs]
  csv = true
  [exodus]
    type = Exodus
    show = 'temp'
  []
[]

(modules/combined/test/tests/cavity_pressure/rz.i)

#
# Cavity Pressure Test
#
# This test is designed to compute an internal pressure based on
#   p = n * R * T / V
# where
#   p is the pressure
#   n is the amount of material in the volume (moles)
#   R is the universal gas constant
#   T is the temperature
#   V is the volume
#
# The mesh is composed of one block (2) with an interior cavity of volume 8.
#   Block 1 sits in the cavity and has a volume of 1.  Thus, the total
#   initial volume is 7.
# The test adjusts T in the following way:
#   T => T0 + beta * t
# with
#   beta = T0
#   T0 = 240.54443866068704
#   V0 = 7
#   n0 = f(p0)
#   p0 = 100
#   R = 8.314472 J * K^(-1) * mol^(-1)
#
# So, n0 = p0 * V0 / R / T0 = 100 * 7 / 8.314472 / 240.544439
#        = 0.35
#
# At t = 1, p = 200.

[Problem]
  coord_type = RZ
[]

[GlobalParams]
  displacements = 'disp_r disp_z'
[]

[Mesh]
  file = rz.e
[]

[Functions]
  [./temperature]
    type = PiecewiseLinear
    x = '0 1'
    y = '1 2'
    scale_factor = 240.54443866068704
  [../]
[]

[Variables]
  [./disp_r]
  [../]
  [./disp_z]
  [../]
  [./temp]
    initial_condition = 240.54443866068704
  [../]
[]

[Kernels]
  [./TensorMechanics]
    use_displaced_mesh = true
  [../]
  [./heat]
    type = Diffusion
    variable = temp
    use_displaced_mesh = true
  [../]
[]

[BCs]
  [./no_x]
    type = DirichletBC
    variable = disp_r
    boundary = '1 2'
    value = 0.0
  [../]
  [./no_y]
    type = DirichletBC
    variable = disp_z
    boundary = '1 2'
    value = 0.0
  [../]
  [./temperatureInterior]
    type = FunctionDirichletBC
    boundary = 2
    function = temperature
    variable = temp
  [../]
  [./CavityPressure]
    [./1]
      boundary = 2
      initial_pressure = 100
      R = 8.314472
      temperature = aveTempInterior
      volume = internalVolume
      startup_time = 0.5
      output = ppress
    [../]
  [../]
[]

[Materials]
  [./elastic_tensor1]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 1e6
    poissons_ratio = 0.3
    block = 1
  [../]
  [./strain1]
    type = ComputeAxisymmetricRZFiniteStrain
    block = 1
  [../]
  [./stress1]
    type = ComputeFiniteStrainElasticStress
    block = 1
  [../]
  [./elastic_tensor2]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 1e6
    poissons_ratio = 0.3
    block = 2
  [../]
  [./strain2]
    type = ComputeAxisymmetricRZFiniteStrain
    block = 2
  [../]
  [./stress2]
    type = ComputeFiniteStrainElasticStress
    block = 2
  [../]
[]

[Executioner]
  type = Transient

  petsc_options_iname = '-pc_type -sub_pc_type'
  petsc_options_value = 'asm       lu'

  nl_abs_tol = 1e-10

  l_max_its = 20

  dt = 0.5
  end_time = 1.0
[]

[Postprocessors]
  [./internalVolume]
    type = InternalVolume
    boundary = 2
    execute_on = 'initial linear'
  [../]
  [./aveTempInterior]
    type = SideAverageValue
    boundary = 2
    variable = temp
    execute_on = 'initial linear'
  [../]
[]

[Outputs]
  exodus = true
  [./checkpoint]
    type = Checkpoint
    num_files = 1
  [../]
[]

(modules/porous_flow/examples/flow_through_fractured_media/fine_transient.i)

# Using a mixed-dimensional mesh
# Transient flow and solute transport along a fracture in a porous matrix
# advective dominated flow in the fracture and diffusion into the porous matrix
#
# Note that fine_steady.i must be run to initialise the porepressure properly

[Mesh]
  file = 'gold/fine_steady_out.e'
[]

[GlobalParams]
  PorousFlowDictator = dictator
  gravity = '0 0 0'
[]

[Variables]
  [pp]
    initial_from_file_var = pp
    initial_from_file_timestep = 1
  []
  [massfrac0]
  []
[]

[AuxVariables]
  [velocity_x]
    family = MONOMIAL
    order = CONSTANT
    block = fracture
  []
  [velocity_y]
    family = MONOMIAL
    order = CONSTANT
    block = fracture
  []
[]

[AuxKernels]
  [velocity_x]
    type = PorousFlowDarcyVelocityComponentLowerDimensional
    variable = velocity_x
    component = x
    aperture = 6E-4
  []
  [velocity_y]
    type = PorousFlowDarcyVelocityComponentLowerDimensional
    variable = velocity_y
    component = y
    aperture = 6E-4
  []
[]

[ICs]
  [massfrac0]
    type = ConstantIC
    variable = massfrac0
    value = 0
  []
[]

[BCs]
  [top]
    type = DirichletBC
    value = 0
    variable = massfrac0
    boundary = top
  []
  [bottom]
    type = DirichletBC
    value = 1
    variable = massfrac0
    boundary = bottom
  []
  [ptop]
    type = DirichletBC
    variable = pp
    boundary =  top
    value = 1e6
  []
  [pbottom]
    type = DirichletBC
    variable = pp
    boundary = bottom
    value = 1.002e6
  []
[]

[Kernels]
  [mass0]
    type = PorousFlowMassTimeDerivative
    fluid_component = 0
    variable = pp
  []
  [adv0]
    type = PorousFlowAdvectiveFlux
    fluid_component = 0
    variable = pp
  []
  [diff0]
    type = PorousFlowDispersiveFlux
    fluid_component = 0
    variable = pp
    disp_trans = 0
    disp_long = 0
  []
  [mass1]
    type = PorousFlowMassTimeDerivative
    fluid_component = 1
    variable = massfrac0
  []
  [adv1]
    type = PorousFlowAdvectiveFlux
    fluid_component = 1
    variable = massfrac0
  []
  [diff1]
    type = PorousFlowDispersiveFlux
    fluid_component = 1
    variable = massfrac0
    disp_trans = 0
    disp_long = 0
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'pp massfrac0'
    number_fluid_phases = 1
    number_fluid_components = 2
  []
[]

[Modules]
  [FluidProperties]
    [simple_fluid]
      type = SimpleFluidProperties
      bulk_modulus = 2e9
      density0 = 1000
      thermal_expansion = 0
      viscosity = 1e-3
    []
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
  []
  [ppss]
    type = PorousFlow1PhaseFullySaturated
    porepressure = pp
  []
  [massfrac]
    type = PorousFlowMassFraction
    mass_fraction_vars = massfrac0
  []
  [simple_fluid]
    type = PorousFlowSingleComponentFluid
    fp = simple_fluid
    phase = 0
  []
  [poro_fracture]
    type = PorousFlowPorosityConst
    porosity = 6e-4   # = a * phif
    block = 'fracture'
  []
  [poro_matrix]
    type = PorousFlowPorosityConst
    porosity = 0.1
    block = 'matrix1 matrix2'
  []
  [diff1]
    type = PorousFlowDiffusivityConst
    diffusion_coeff = '1e-9 1e-9'
    tortuosity = 1.0
    block = 'fracture'
  []
  [diff2]
    type = PorousFlowDiffusivityConst
    diffusion_coeff = '1e-9 1e-9'
    tortuosity = 0.1
    block = 'matrix1 matrix2'
  []
  [relp]
    type = PorousFlowRelativePermeabilityConst
    phase = 0
  []
  [permeability_fracture]
    type = PorousFlowPermeabilityConst
    permeability = '1.8e-11 0 0 0 1.8e-11 0 0 0 1.8e-11' # kf=3e-8, a=6e-4m.  1.8e-11 = kf * a
    block = 'fracture'
  []
  [permeability_matrix]
    type = PorousFlowPermeabilityConst
    permeability = '1e-20 0 0 0 1e-20 0 0 0 1e-20'
    block = 'matrix1 matrix2'
  []
[]

[Functions]
  [dt_controller]
     type = PiecewiseConstant
     x = '0    30   40 100 200 83200'
     y = '0.01 0.1  1  10  100 32'
  []
[]

[Preconditioning]
  active = basic
  [mumps_is_best_for_parallel_jobs]
    type = SMP
    full = true
    petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
    petsc_options_value = ' lu       mumps'
  []
  [basic]
    type = SMP
    full = true
    petsc_options_iname = '-ksp_type -pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap'
    petsc_options_value = 'gmres      asm      lu           NONZERO                   2             '
  []
[]

[Executioner]
  type = Transient
  solve_type = NEWTON
  end_time = 86400

  [TimeStepper]
    type = FunctionDT
    function = dt_controller
  []

# controls for nonlinear iterations
  nl_max_its = 15
  nl_rel_tol = 1e-14
  nl_abs_tol = 1e-9
[]


[VectorPostprocessors]
  [xmass]
    type = LineValueSampler
    start_point = '0.4 0 0'
    end_point = '0.5 0 0'
    sort_by = x
    num_points = 167
    variable = massfrac0
  []
[]

[Outputs]
  perf_graph = true
  console = true
  csv = true
  exodus = true
[]

(test/tests/executioners/eigen_executioners/ane.i)

[Mesh]
 type = GeneratedMesh
 dim = 2
 xmin = 0
 xmax = 10
 ymin = 0
 ymax = 10
 elem_type = QUAD4
 nx = 8
 ny = 8

 uniform_refine = 0
[]

# the minimum eigenvalue is (2*PI*(p-1)^(1/p)/a/p/sin(PI/p))^p;
# Its inverse is 35.349726539758187. Here a is equal to 10.

[Variables]
  active = 'u'

  [./u]
    # second order is way better than first order
    order = FIRST
    family = LAGRANGE
  [../]
[]

[ICs]
  [./uic]
    type = RandomIC
    variable = u
  [../]
[]

[Kernels]
  active = 'diff rhs'

  [./diff]
    type = PHarmonic
    variable = u
    p = 3
  [../]

  [./rhs]
    type = PMassEigenKernel
    variable = u
    p = 3
  [../]
[]

[BCs]
  active = 'homogeneous'

  [./homogeneous]
    type = DirichletBC
    variable = u
    boundary = '0 2'
    value = 0
  [../]
[]

[Executioner]
  type = NonlinearEigen

  bx_norm = 'unorm'

  free_power_iterations = 10
  nl_abs_tol = 1e-12
  nl_rel_tol = 1e-50
  k0 = 1.0
# important: constant initial value set by auto_initilization does not
# converge to the fundamental mode
  auto_initialization = false
  output_after_power_iterations = false

  #Preconditioned JFNK (default)
  solve_type = 'PJFNK'
  l_max_its = 100
[]

[Postprocessors]
  active = 'unorm udiff'

  [./unorm]
    type = ElementIntegralVariablePostprocessor
    variable = u
    # execute on residual is important for nonlinear eigen solver!
    execute_on = linear
  [../]

  [./udiff]
    type = ElementL2Diff
    variable = u
    outputs = console
  [../]
[]

[Outputs]
  execute_on = 'timestep_end'
  file_base = ane
  exodus = true
[]

(test/tests/multiapps/restart/sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 1
  xmin = 0
  xmax = 1
  nx = 10
[]

[Functions]
  [./u_fn]
    type = ParsedFunction
    value = t*x
  [../]
  [./ffn]
    type = ParsedFunction
    value = x
  [../]
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
  [./fn]
    type = BodyForce
    variable = u
    function = ffn
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = FunctionDirichletBC
    variable = u
    boundary = right
    function = u_fn
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 5
  dt = 0.1
  solve_type = 'PJFNK'
[]

[Outputs]
  exodus = true
[]

(test/tests/transfers/multiapp_conservative_transfer/master_userobject.i)

[Mesh]
  type = GeneratedMesh
  dim = 3
  nx = 20
  ny = 20
  nz = 20
  # The MultiAppUserObjectTransfer object only works with ReplicatedMesh
  parallel_type = replicated
[]

[Variables]
  [./u]
  [../]
[]

[AuxVariables]
  [./multi_layered_average]
  [../]
  [./element_multi_layered_average]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 1
  dt = 0.001 # This will be constrained by the multiapp

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
  l_tol = 1e-8
  nl_rel_tol = 1e-10
[]


[Outputs]
  exodus = true
  csv = true
[]

[VectorPostprocessors]
  [to_nearest_point]
    type = NearestPointIntegralVariablePostprocessor
    variable = multi_layered_average
    points = '0.3 0.1 0.3 0.7 0.1 0.3'
    execute_on = 'transfer'
  []

  [to_nearest_point_element]
    type = NearestPointIntegralVariablePostprocessor
    variable = element_multi_layered_average
    points = '0.3 0.1 0.3 0.7 0.1 0.3'
    execute_on = 'transfer'
  []
[]

[MultiApps]
  [./sub_app]
    positions = '0.3 0.1 0.3 0.7 0.1 0.3'
    type = TransientMultiApp
    input_files = sub_userobject.i
    app_type = MooseTestApp
  [../]
[]

[Transfers]
  [./layered_transfer]
    user_object = layered_average
    variable = multi_layered_average
    type = MultiAppUserObjectTransfer
    from_multi_app = sub_app

    from_postprocessors_to_be_preserved  = 'from_postprocessor'
    to_postprocessors_to_be_preserved  = 'to_nearest_point'
  [../]
  [./element_layered_transfer]
    user_object = layered_average
    variable = element_multi_layered_average
    type = MultiAppUserObjectTransfer
    from_multi_app = sub_app

    from_postprocessors_to_be_preserved  = 'from_postprocessor'
    to_postprocessors_to_be_preserved  = 'to_nearest_point_element'
  [../]
[]

(modules/tensor_mechanics/test/tests/strain_energy_density/rate_model_small.i)

# Single element test to check the strain energy density calculation

[GlobalParams]
  displacements = 'disp_x disp_y'
  volumetric_locking_correction = true
[]

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 1
  ny = 1
  xmin = 0
  xmax = 1
  ymin = 0
  ymax = 2
[]

[AuxVariables]
  [./SERD]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[Functions]
  [./rampConstantUp]
    type = PiecewiseLinear
    x = '0. 1.'
    y = '0. 1.'
    scale_factor = -100
  [../]
  [./ramp_disp_y]
    type = PiecewiseLinear
    x = '0. 1. 2.'
    y = '0. 6.8e-6 1.36e-5'
  [../]
[]

[Modules/TensorMechanics/Master]
  [./master]
    strain = SMALL
    add_variables = true
    incremental = true
    generate_output = 'stress_xx stress_yy stress_zz vonmises_stress elastic_strain_xx elastic_strain_yy elastic_strain_zz strain_xx strain_yy strain_zz'
    planar_formulation = PLANE_STRAIN
  [../]
[]

[AuxKernels]
  [./SERD]
    type = MaterialRealAux
    variable = SERD
    property = strain_energy_rate_density
    execute_on = timestep_end
  [../]
[]

[BCs]
  [./no_x]
    type = DirichletBC
    variable = disp_x
    preset = false
    boundary = 'left'
    value = 0.0
  [../]
  [./no_y]
    type = DirichletBC
    variable = disp_y
    preset = false
    boundary = 'bottom'
    value = 0.0
  [../]
  [./top_disp]
    type = FunctionDirichletBC
    variable = disp_y
    preset = false
    boundary = 'top'
    function = ramp_disp_y
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 206800
    poissons_ratio = 0.0
  [../]
  [./radial_return_stress]
    type = ComputeMultipleInelasticStress
    inelastic_models = 'powerlawcrp'
  [../]
  [./powerlawcrp]
    type = PowerLawCreepStressUpdate
    coefficient = 3.125e-21 # 7.04e-17 #
    n_exponent = 4.0
    m_exponent = 0.0
    activation_energy = 0.0
    # max_inelastic_increment = 0.01
  [../]
  [./strain_energy_rate_density]
    type = StrainEnergyRateDensity
    inelastic_models = 'powerlawcrp'
  [../]
[]

[Executioner]
   type = Transient

  petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
  petsc_options_value = '201                hypre    boomeramg      4'

  line_search = 'none'

   l_max_its = 50
   nl_max_its = 20
   nl_abs_tol = 3e-7
   nl_rel_tol = 1e-12
   l_tol = 1e-2

   start_time = 0.0
   dt = 1

   end_time = 2
   num_steps = 2
[]

[Postprocessors]
  [./etxx]
    type = ElementalVariableValue
    variable = strain_xx
    elementid = 0
  [../]
  [./etyy]
    type = ElementalVariableValue
    variable = strain_yy
    elementid = 0
  [../]
  [./etzz]
    type = ElementalVariableValue
    variable = strain_zz
    elementid = 0
  [../]
  [./sigxx]
    type = ElementAverageValue
    variable = stress_xx
  [../]
  [./sigyy]
    type = ElementAverageValue
    variable = stress_yy
  [../]
  [./sigzz]
    type = ElementAverageValue
    variable = stress_zz
  [../]
  [./SERD]
    type = ElementAverageValue
    variable = SERD
  [../]
[]

[Outputs]
  exodus = true
  csv = true
[]

(test/tests/controls/time_periods/dampers/enable_disable.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Dampers]
  [./const_damp]
    type = ConstantDamper
    damping = 0.9
  [../]
[]

[Outputs]
  exodus = true
[]

(modules/porous_flow/test/tests/pressure_pulse/pressure_pulse_1d_3comp_fully_saturated.i)

# Pressure pulse in 1D with 1 phase, 3 component - transient
# using the PorousFlowFullySaturatedDarcyFlow Kernel
[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 20
  xmin = 0
  xmax = 100
[]

[GlobalParams]
  PorousFlowDictator = dictator
[]

[Variables]
  [pp]
    initial_condition = 2E6
  []
  [f0]
    initial_condition = 0
  []
  [f1]
    initial_condition = 0.2
  []
[]

[Kernels]
  [mass0]
    type = PorousFlowMassTimeDerivative
    fluid_component = 0
    variable = pp
  []
  [flux0]
    type = PorousFlowFullySaturatedDarcyFlow
    variable = pp
    gravity = '0 0 0'
    fluid_component = 0
  []
  [mass1]
    type = PorousFlowMassTimeDerivative
    fluid_component = 1
    variable = f0
  []
  [flux1]
    type = PorousFlowFullySaturatedDarcyFlow
    variable = f0
    gravity = '0 0 0'
    fluid_component = 1
  []
  [mass2]
    type = PorousFlowMassTimeDerivative
    fluid_component = 2
    variable = f1
  []
  [flux2]
    type = PorousFlowFullySaturatedDarcyFlow
    variable = f1
    gravity = '0 0 0'
    fluid_component = 2
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'pp f0 f1'
    number_fluid_phases = 1
    number_fluid_components = 3
  []
[]

[Modules]
  [FluidProperties]
    [simple_fluid]
      type = SimpleFluidProperties
      bulk_modulus = 2e9
      density0 = 1000
      thermal_expansion = 0
      viscosity = 1e-3
    []
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
  []
  [ppss]
    type = PorousFlow1PhaseFullySaturated
    porepressure = pp
  []
  [massfrac_nodes]
    type = PorousFlowMassFraction
    mass_fraction_vars = 'f0 f1'
  []
  [simple_fluid]
    type = PorousFlowSingleComponentFluid
    fp = simple_fluid
    phase = 0
  []
  [porosity]
    type = PorousFlowPorosityConst
    porosity = 0.1
  []
  [permeability]
    type = PorousFlowPermeabilityConst
    permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
  []
[]

[BCs]
  [left]
    type = DirichletBC
    boundary = left
    preset = false
    value = 3E6
    variable = pp
  []
[]

[Preconditioning]
  [andy]
    type = SMP
    full = true
    petsc_options_iname = '-ksp_type -pc_type -snes_atol -snes_rtol -snes_max_it -pc_factor_shift_type'
    petsc_options_value = 'bcgs lu 1E-15 1E-10 10000 NONZERO'
  []
[]

[Executioner]
  type = Transient
  solve_type = Newton
  dt = 1E3
  end_time = 1E4
[]

[Postprocessors]
  [p005]
    type = PointValue
    variable = pp
    point = '5 0 0'
    execute_on = 'initial timestep_end'
  []
  [p015]
    type = PointValue
    variable = pp
    point = '15 0 0'
    execute_on = 'initial timestep_end'
  []
  [p025]
    type = PointValue
    variable = pp
    point = '25 0 0'
    execute_on = 'initial timestep_end'
  []
  [p035]
    type = PointValue
    variable = pp
    point = '35 0 0'
    execute_on = 'initial timestep_end'
  []
  [p045]
    type = PointValue
    variable = pp
    point = '45 0 0'
    execute_on = 'initial timestep_end'
  []
  [p055]
    type = PointValue
    variable = pp
    point = '55 0 0'
    execute_on = 'initial timestep_end'
  []
  [p065]
    type = PointValue
    variable = pp
    point = '65 0 0'
    execute_on = 'initial timestep_end'
  []
  [p075]
    type = PointValue
    variable = pp
    point = '75 0 0'
    execute_on = 'initial timestep_end'
  []
  [p085]
    type = PointValue
    variable = pp
    point = '85 0 0'
    execute_on = 'initial timestep_end'
  []
  [p095]
    type = PointValue
    variable = pp
    point = '95 0 0'
    execute_on = 'initial timestep_end'
  []
[]

[Outputs]
  file_base = pressure_pulse_1d_3comp_fully_saturated
  print_linear_residuals = false
  csv = true
[]

(test/tests/markers/combo_marker/combo_marker_test.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
  nz = 0
  zmax = 0
  elem_type = QUAD4
[]

[Variables]
  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = 2
    value = 1
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'
[]

[Adaptivity]
  [./Markers]
    [./box]
      type = BoxMarker
      bottom_left = '0.3 0.3 0'
      top_right = '0.6 0.6 0'
      inside = refine
      outside = do_nothing
    [../]
    [./combo]
      type = ComboMarker
      markers = 'box box2'
    [../]
    [./box2]
      type = BoxMarker
      bottom_left = '0.5 0.5 0'
      top_right = '0.8 0.8 0'
      inside = refine
      outside = coarsen
    [../]
  [../]
[]

[Outputs]
  exodus = true
[]

(python/peacock/tests/input_tab/InputTreeWriter/gold/simple_diffusion_inactive.i)

inactive = 'Kernels BCs Executioner'
[Mesh]
  [generate]
    type = GeneratedMeshGenerator
    dim = 2
    nx = 10
    ny = 10
  []
[]

[Variables]
  [u]
  []
[]

[Kernels]
  inactive = 'diff'
  [diff]
    type = Diffusion
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = 'left'
    value = 0
  []
  [right]
    type = DirichletBC
    variable = u
    boundary = 'right'
    value = 1
  []
[]

[Executioner]
  # Preconditioned JFNK (default)
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(test/tests/executioners/steady_time/steady_time.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  xmin = 0
  xmax = 1
  ymin = 0
  ymax = 1
  elem_type = QUAD4
  nx = 4
  ny = 4
[]

[Variables]
  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]

  [./force]
    type = BodyForce
    variable = u
    function = time_function
  [../]
[]

[Functions]
  [./time_function]
    type = ParsedFunction
    value = 't+1'
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = 'left right bottom top'
    value = 0
  [../]
[]

[Postprocessors]
  [./norm]
    type = ElementL2Norm
    variable = u
  [../]
[]

[Executioner]
  type = Steady
[]

[Outputs]
  exodus = true
[]

(modules/heat_conduction/test/tests/heat_conduction/2d_quadrature_gap_heat_transfer/nonmatching.i)

[Mesh]
  file = nonmatching.e
[]

[Variables]
  [./temp]
  [../]
[]

[Kernels]
  [./hc]
    type = HeatConduction
    variable = temp
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = temp
    boundary = leftleft
    value = 1000
  [../]
  [./right]
    type = DirichletBC
    variable = temp
    boundary = rightright
    value = 400
  [../]
[]

[ThermalContact]
  [./left_to_right]
    emissivity_primary = 0
    emissivity_secondary = 0
    secondary = leftright
    quadrature = true
    primary = rightleft
    variable = temp
    type = GapHeatTransfer
  [../]
[]

[Materials]
  [./hcm]
    type = HeatConductionMaterial
    block = 'left right'
    specific_heat = 1
    thermal_conductivity = 1
  [../]
  [./gap_conductance]
    type = GenericConstantMaterial
    prop_names = 'gap_conductance gap_conductance_dT'
    boundary = 'leftright rightleft'
    prop_values = '1 0'
  [../]
[]

[Postprocessors]
  [./left]
    type = SideDiffusiveFluxIntegral
    variable = temp
    boundary = leftright
    diffusivity = thermal_conductivity
  [../]
  [./right]
    type = SideDiffusiveFluxIntegral
    variable = temp
    boundary = rightleft
    diffusivity = thermal_conductivity
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(modules/navier_stokes/test/tests/finite_element/ins/RZ_cone/rz_cone_by_parts_steady_stabilized.i)

# This input file tests several different things:
# .) The axisymmetric (RZ) form of the governing equations.
# .) An open boundary.
# .) Not integrating the pressure by parts, thereby requiring a pressure pin.
# .) Natural boundary condition at the outlet.
[GlobalParams]
  integrate_p_by_parts = true
  laplace = true
  gravity = '0 0 0'
  supg = true
  pspg = true
  order = FIRST
[]

[Mesh]
  file = '2d_cone.msh'
[]

[Problem]
  coord_type = RZ
[]

[Preconditioning]
  [./SMP_PJFNK]
    type = SMP
    full = true
    solve_type = Newton
  [../]
[]

[Executioner]
  type = Steady

  petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_levels'
  petsc_options_value = 'bjacobi  ilu          4'

  nl_rel_tol = 1e-12
  nl_max_its = 6
[]

[Outputs]
  csv = true
  console = true
  [./out]
    type = Exodus
  [../]
[]

[Variables]
  [./vel_x]
    # Velocity in radial (r) direction
  [../]
  [./vel_y]
    # Velocity in axial (z) direction
  [../]
  [./p]
  [../]
[]

[BCs]
  [./u_in]
    type = DirichletBC
    boundary = bottom
    variable = vel_x
    value = 0
  [../]
  [./v_in]
    type = FunctionDirichletBC
    boundary = bottom
    variable = vel_y
    function = 'inlet_func'
  [../]
  [./u_axis_and_walls]
    type = DirichletBC
    boundary = 'left right'
    variable = vel_x
    value = 0
  [../]
  [./v_no_slip]
    type = DirichletBC
    boundary = 'right'
    variable = vel_y
    value = 0
  [../]
[]


[Kernels]
  [./mass]
    type = INSMassRZ
    variable = p
    u = vel_x
    v = vel_y
    pressure = p
  [../]
  [./x_momentum_space]
    type = INSMomentumLaplaceFormRZ
    variable = vel_x
    u = vel_x
    v = vel_y
    pressure = p
    component = 0
  [../]
  [./y_momentum_space]
    type = INSMomentumLaplaceFormRZ
    variable = vel_y
    u = vel_x
    v = vel_y
    pressure = p
    component = 1
  [../]
[]

[Materials]
  [./const]
    type = GenericConstantMaterial
    block = 'volume'
    prop_names = 'rho mu'
    prop_values = '1  1'
  [../]
[]

[Functions]
  [./inlet_func]
    type = ParsedFunction
    value = '-4 * x^2 + 1'
  [../]
[]

[Postprocessors]
  [./flow_in]
    type = VolumetricFlowRate
    vel_x = vel_x
    vel_y = vel_y
    boundary = 'bottom'
    execute_on = 'timestep_end'
  [../]
  [./flow_out]
    type = VolumetricFlowRate
    vel_x = vel_x
    vel_y = vel_y
    boundary = 'top'
    execute_on = 'timestep_end'
  [../]
[]

(test/tests/dampers/bounding_value_nodal_damper/bounding_value_max_test.i)

# This model tests the BoundingValueNodalDamper. The converged solution
# for u starts out in the range from 0 to 1, but after several steps,
# a volumetric source drives it to a value greater than 1, which is
# outside the range of the damper. At that point, the solution can
# no longer converge, and the model errors out with a failure to converge.
# The test verifies that the damper computes the correct value in the first
# nonlinear iteration when the solution exceeds the bounds.

[Mesh]
  type = GeneratedMesh
  dim = 2
  xmin = 0
  xmax = 1
  ymin = 0
  ymax = 1
  nx = 2
  ny = 2
  elem_type = QUAD9
[]

[Variables]
  [./u]
    order = SECOND
    family = LAGRANGE
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]

  [./source]
    type = BodyForce
    variable = u
    function = 't'
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Dampers]
  [./bounding_value_damp]
    type = BoundingValueNodalDamper
    min_value = 0.0
    max_value = 1.0
    variable = u
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'
  end_time = 3.0
  dt = 0.5
  dtmin = 0.5
  nl_max_its = 5
[]

(test/tests/kernels/ad_value/generic_value.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 2
[]

[Variables]
  [./u]
  [../]
  [./v]
  [../]
[]

[AuxVariables]
  [./u_jac]
  [../]
  [./v_jac]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./diff_v]
    type = Diffusion
    variable = v
  [../]
  [./value_test_v]
    type = GenericValueTest
    variable = v
    diag_save_in = v_jac
  [../]
  [./ad_value_test]
    type = ADGenericValueTest
    variable = u
    diag_save_in = u_jac
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
  [./left_v]
    type = DirichletBC
    variable = v
    boundary = left
    value = 0
  [../]
  [./right_v]
    type = DirichletBC
    variable = v
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'Newton'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(modules/heat_conduction/test/tests/gap_heat_transfer_mortar/bc_gap_heat_transfer_displaced_conduction.i)

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Mesh]
  [file]
    type = FileMeshGenerator
    file = 2blk-gap.e
  []
  allow_renumbering = false
[]

[Problem]
  kernel_coverage_check = false
  material_coverage_check = false
[]

[Variables]
  [temp]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
  [disp_x]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
  [disp_y]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
[]

[Materials]
  [left]
    type = ADHeatConductionMaterial
    block = 1
    thermal_conductivity = 0.01
    specific_heat = 1
  []

  [right]
    type = ADHeatConductionMaterial
    block = 2
    thermal_conductivity = 0.005
    specific_heat = 1
  []
[]

[Kernels]
  [hc_displaced_block]
    type = ADHeatConduction
    variable = temp
    use_displaced_mesh = true
    block = '1'
  []
  [hc_undisplaced_block]
    type = ADHeatConduction
    variable = temp
    use_displaced_mesh = false
    block = '2'
  []
  [disp_x]
    type = Diffusion
    variable = disp_x
    block = '1 2'
  []
  [disp_y]
    type = Diffusion
    variable = disp_y
    block = '1 2'
  []
[]

[ThermalContact]
  [thermal_contact]
    type = GapHeatTransfer
    variable = temp
    primary = 100
    secondary = 101
    emissivity_primary = 0.0
    emissivity_secondary = 0.0
    gap_conductivity = 100.0
    quadrature = true
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = temp
    boundary = 'left'
    value = 100
  []

  [right]
    type = DirichletBC
    variable = temp
    boundary = 'right'
    value = 0
  []

  [left_disp_x]
    type = DirichletBC
    preset = false
    variable = disp_x
    boundary = 'left'
    value = .1
  []
  [right_disp_x]
    type = DirichletBC
    preset = false
    variable = disp_x
    boundary = 'right'
    value = 0
  []
  [bottom_disp_y]
    type = DirichletBC
    preset = false
    variable = disp_y
    boundary = 'bottom'
    value = 0
  []
[]

[Preconditioning]
  [fmp]
    type = SMP
    full = true
    solve_type = 'NEWTON'
  []
[]

[Executioner]
  type = Steady
  nl_rel_tol = 1e-11
  nl_abs_tol = 1.0e-10
[]

[VectorPostprocessors]
  [NodalTemperature]
    type = NodalValueSampler
    sort_by = id
    boundary = '100 101'
    variable = 'temp'
  []
[]

[Outputs]
  exodus = false
  csv = true
[]

(test/tests/geomsearch/2d_penetration_locator/2d_penetration_locator_test.i)

[Mesh]
  file = 2d_contact_test.e
[]

[Variables]
  active = 'u'

  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[AuxVariables]
  [./penetration]
    order = FIRST
    family = LAGRANGE
  [../]
  [./tangential_distance]
    order = FIRST
    family = LAGRANGE
  [../]
  [./normal_x]
    order = FIRST
    family = LAGRANGE
  [../]
  [./normal_y]
    order = FIRST
    family = LAGRANGE
  [../]
  [./closest_point_x]
    order = FIRST
    family = LAGRANGE
  [../]
  [./closest_point_y]
    order = FIRST
    family = LAGRANGE
  [../]
  [./element_id]
    order = FIRST
    family = LAGRANGE
  [../]
  [./side]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  active = 'diff'

  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[AuxKernels]
  [./penetrate]
    type = PenetrationAux
    variable = penetration
    boundary = 2
    paired_boundary = 3
  [../]

  [./penetrate2]
    type = PenetrationAux
    variable = penetration
    boundary = 3
    paired_boundary = 2
  [../]

  [./penetrate3]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 2
    paired_boundary = 3
    quantity = tangential_distance
  [../]

  [./penetrate4]
    type = PenetrationAux
    variable = tangential_distance
    boundary = 3
    paired_boundary = 2
    quantity = tangential_distance
  [../]

  [./penetrate5]
    type = PenetrationAux
    variable = normal_x
    boundary = 2
    paired_boundary = 3
    quantity = normal_x
  [../]

  [./penetrate6]
    type = PenetrationAux
    variable = normal_x
    boundary = 3
    paired_boundary = 2
    quantity = normal_x
  [../]

  [./penetrate7]
    type = PenetrationAux
    variable = normal_y
    boundary = 2
    paired_boundary = 3
    quantity = normal_y
  [../]

  [./penetrate8]
    type = PenetrationAux
    variable = normal_y
    boundary = 3
    paired_boundary = 2
    quantity = normal_y
  [../]

  [./penetrate9]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 2
    paired_boundary = 3
    quantity = closest_point_x
  [../]

  [./penetrate10]
    type = PenetrationAux
    variable = closest_point_x
    boundary = 3
    paired_boundary = 2
    quantity = closest_point_x
  [../]

  [./penetrate11]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 2
    paired_boundary = 3
    quantity = closest_point_y
  [../]

  [./penetrate12]
    type = PenetrationAux
    variable = closest_point_y
    boundary = 3
    paired_boundary = 2
    quantity = closest_point_y
  [../]

  [./penetrate13]
    type = PenetrationAux
    variable = element_id
    boundary = 2
    paired_boundary = 3
    quantity = element_id
  [../]

  [./penetrate14]
    type = PenetrationAux
    variable = element_id
    boundary = 3
    paired_boundary = 2
    quantity = element_id
  [../]

  [./penetrate15]
    type = PenetrationAux
    variable = side
    boundary = 2
    paired_boundary = 3
    quantity = side
  [../]

  [./penetrate16]
    type = PenetrationAux
    variable = side
    boundary = 3
    paired_boundary = 2
    quantity = side
  [../]
[]

[BCs]
  active = 'block1_left block1_right block2_left block2_right'

  [./block1_left]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 0
  [../]

  [./block1_right]
    type = DirichletBC
    variable = u
    boundary = 2
    value = 1
  [../]

  [./block2_left]
    type = DirichletBC
    variable = u
    boundary = 3
    value = 0
  [../]

  [./block2_right]
    type = DirichletBC
    variable = u
    boundary = 4
    value = 1
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'
[]

[Outputs]
  file_base = out
  exodus = true
[]

(test/tests/transfers/multiapp_userobject_transfer/two_pipe_master.i)

[Mesh]
  [gen]
    type = GeneratedMeshGenerator
    dim = 3
    xmin = 0
    xmax = 5
    nx = 5

    ymin = 0
    ymax = 5
    ny = 5

    zmin = 0
    zmax = 5
    nz = 5
  []
  [./blocks]
    input = gen
    type = SubdomainBoundingBoxGenerator
    block_id = 1
    bottom_left = '1 1 0'
    top_right = '4 4 5'
  [../]
[]

[AuxVariables]
  [./from_sub_app_var]
    order = CONSTANT
    family = MONOMIAL
    block = 1
    initial_condition = 0
  [../]
[]

[Variables]
  [u]
  []
[]

[Kernels]
  [diff]
    type = Diffusion
    variable = u
  []
  [td]
    type = TimeDerivative
    variable = u
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = front
    value = -1
  []
  [right]
    type = DirichletBC
    variable = u
    boundary = back
    value = 1
  []
[]

[Executioner]
  type = Transient
  num_steps = 2
  dt = 5

  solve_type = 'NEWTON'
  l_tol = 1e-8
  nl_rel_tol = 1e-10
[]

[Outputs]
  exodus = true
  execute_on = final
[]

[MultiApps]
  [sub_app]
    type = TransientMultiApp
    positions = '0 0 0'
    input_files = two_pipe_sub.i
    app_type = MooseTestApp
    execute_on = TIMESTEP_END
  []
[]

[Transfers]
  [layered_transfer_from_sub_app]
    type = MultiAppUserObjectTransfer
    user_object = sub_app_uo
    variable = from_sub_app_var
    from_multi_app = sub_app
    displaced_source_mesh = true
    skip_bounding_box_check = true
  []
[]

(modules/tensor_mechanics/test/tests/volumetric_deform_grad/elastic_stress.i)

[Mesh]
  type = GeneratedMesh
  dim = 3
  elem_type = HEX8
  displacements = 'disp_x disp_y disp_z'
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
  [./disp_z]
  [../]
[]

[Kernels]
  [./TensorMechanics]
    displacements = 'disp_x disp_y disp_z'
    use_displaced_mesh = true
  [../]
[]

[AuxVariables]
  [./stress_zz]
    order = CONSTANT
    family = MONOMIAL
    block = 0
  [../]
[]

[AuxKernels]
  [./stress_zz]
    type = RankTwoAux
    variable = stress_zz
    rank_two_tensor = stress
    index_j = 2
    index_i = 2
    execute_on = timestep_end
    block = 0
  [../]
[]

[BCs]
  [./symmy]
    type = DirichletBC
    variable = disp_y
    boundary = bottom
    value = 0
  [../]
  [./symmx]
    type = DirichletBC
    variable = disp_x
    boundary = left
    value = 0
  [../]
  [./symmz]
    type = DirichletBC
    variable = disp_z
    boundary = back
    value = 0
  [../]
  [./tdisp]
    type = FunctionDirichletBC
    variable = disp_z
    boundary = front
    function = '0.01*t'
  [../]
[]

[Materials]
  [./strain]
    type = ComputeFiniteStrain
    block = 0
    displacements = 'disp_x disp_y disp_z'
  [../]
  [./elastic_stress]
    type = ComputeDeformGradBasedStress
    deform_grad_name = deformation_gradient
    elasticity_tensor_name = elasticity_tensor
    stress_name = stress
    jacobian_name = Jacobian_mult
    block = 0
  [../]
  [./elasticity_tensor]
    type = ComputeElasticityTensor
    block = 0
    C_ijkl = '2.8e5 1.2e5 1.2e5 2.8e5 1.2e5 2.8e5 0.8e5 0.8e5 0.8e5'
    fill_method = symmetric9
  [../]
[]

[Postprocessors]
  [./stress_zz]
    type = ElementAverageValue
    variable = stress_zz
    block = 'ANY_BLOCK_ID 0'
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient
  dt = 0.02
  #Preconditioned JFNK (default)
  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type -pc_hypre_type -ksp_gmres_restart'
  petsc_options_value = 'hypre boomeramg 101'
  dtmax = 10.0
  nl_rel_tol = 1e-10
  dtmin = 0.02
  num_steps = 10
[]

[Outputs]
  csv = true
[]

(examples/ex09_stateful_materials/ex09.i)

[Mesh]
  file = square.e
  uniform_refine = 4
[]

[Variables]
  [./convected]
    order = FIRST
    family = LAGRANGE
  [../]

  [./diffused]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  [./convected_ie]
    type = TimeDerivative
    variable = convected
  [../]

  [./example_diff]
    # This Kernel uses "diffusivity" from the active material
    type = ExampleDiffusion
    variable = convected
  [../]

  [./conv]
    type = ExampleConvection
    variable = convected
    some_variable = diffused
  [../]

  [./diffused_ie]
    type = TimeDerivative
    variable = diffused
  [../]

  [./diff]
    type = Diffusion
    variable = diffused
  [../]
[]

[BCs]
  [./left_convected]
    type = DirichletBC
    variable = convected
    boundary = 'left'
    value = 0
  [../]

  [./right_convected]
    type = DirichletBC
    variable = convected
    boundary = 'right'
    value = 1

    some_var = diffused
  [../]

  [./left_diffused]
    type = DirichletBC
    variable = diffused
    boundary = 'left'
    value = 0
  [../]

  [./right_diffused]
    type = DirichletBC
    variable = diffused
    boundary = 'right'
    value = 1
  [../]

[]

[Materials]
  [./example_material]
    type = ExampleMaterial
    block = 1
    initial_diffusivity = 0.05
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'
  num_steps = 10
  dt = 1.0
[]

[Outputs]
  execute_on = 'timestep_end'
  exodus = true
[]

(modules/xfem/test/tests/diffusion_xfem/diffusion_flux_bc.i)

# The Neumann BC is applied on the cutted boundary.
# The solution is not correct because so far integration along the cutted element faces is not right.
# To correct this, we need to re-calcuate the weights based on area/volume fraction. This will be implemented soon.

[GlobalParams]
  order = FIRST
  family = LAGRANGE
[]

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 5
  ny = 6
  xmin = 0.0
  xmax = 1.0
  ymin = 0.0
  ymax = 1.0
  elem_type = QUAD4
[]

[XFEM]
  qrule = volfrac
  output_cut_plane = true
[]

[UserObjects]
  [./line_seg_cut_uo]
    type = LineSegmentCutUserObject
    cut_data = '0.5  1.0  0.5  0.5'
    time_start_cut = 0.0
    time_end_cut = 0.0
  [../]
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
# Define boundary conditions
  [./top_u]
    type = NeumannBC
    variable = u
    boundary = 2
    value = -1.0
  [../]

  [./bottom]
    type = DirichletBC
    variable = u
    boundary = 0
    value = 0
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
  line_search = 'none'

  l_tol = 1e-3
  nl_max_its = 15
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-10

  start_time = 0.0
  dt = 1.0
  end_time = 1.0
[]

[Outputs]
  interval = 1
  execute_on = timestep_end
  exodus = true
  [./console]
    type = Console
    output_linear = true
  [../]
[]

(modules/chemical_reactions/test/tests/parser/equilibrium_without_action.i)

# Test AqueousEquilibriumReactions parser

[Mesh]
  type = GeneratedMesh
  dim = 2
[]

[Variables]
  [./a]
  [../]
  [./b]
  [../]
[]

[AuxVariables]
  [./pressure]
  [../]
  [./pa2]
  [../]
  [./pab]
  [../]
[]

[AuxKernels]
  [./pa2]
    type = AqueousEquilibriumRxnAux
    variable = pa2
    v = a
    log_k = 2
    sto_v = 2
  [../]
  [./pab]
    type = AqueousEquilibriumRxnAux
    variable = pab
    v = 'a b'
    log_k = -2
    sto_v = '1 1'
  [../]
[]

[ICs]
  [./a]
    type = BoundingBoxIC
    variable = a
    x1 = 0.0
    y1 = 0.0
    x2 = 1.0e-10
    y2 = 1
    inside = 1.0e-2
    outside = 1.0e-10
  [../]
  [./b]
    type = BoundingBoxIC
    variable = b
    x1 = 0.0
    y1 = 0.0
    x2 = 1.0e-10
    y2 = 1
    inside = 1.0e-2
    outside = 1.0e-10
  [../]
  [./pressure]
    type = FunctionIC
    variable = pressure
    function = 2-x
  [../]
[]

[Kernels]
  [./a_ie]
    type = PrimaryTimeDerivative
    variable = a
  [../]
  [./a_diff]
    type = PrimaryDiffusion
    variable = a
  [../]
  [./a_conv]
    type = PrimaryConvection
    variable = a
    p = pressure
  [../]
  [./b_ie]
    type = PrimaryTimeDerivative
    variable = b
  [../]
  [./b_diff]
    type = PrimaryDiffusion
    variable = b
  [../]
  [./b_conv]
    type = PrimaryConvection
    variable = b
    p = pressure
  [../]
  [./a1_eq]
    type = CoupledBEEquilibriumSub
    variable = a
    log_k = 2
    weight = 2
    sto_u = 2
  [../]
  [./a1_diff]
    type = CoupledDiffusionReactionSub
    variable = a
    log_k = 2
    weight = 2
    sto_u = 2
  [../]
  [./a1_conv]
    type = CoupledConvectionReactionSub
    variable = a
    log_k = 2
    weight = 2
    sto_u = 2
    p = pressure
  [../]
  [./a2_eq]
    type = CoupledBEEquilibriumSub
    variable = a
    v = b
    log_k = -2
    weight = 1
    sto_v = 1
    sto_u = 1
  [../]
  [./a2_diff]
    type = CoupledDiffusionReactionSub
    variable = a
    v = b
    log_k = -2
    weight = 1
    sto_v = 1
    sto_u = 1
  [../]
  [./a2_conv]
    type = CoupledConvectionReactionSub
    variable = a
    v = b
    log_k = -2
    weight = 1
    sto_v = 1
    sto_u = 1
    p = pressure
  [../]
  [./b2_eq]
    type = CoupledBEEquilibriumSub
    variable = b
    v = a
    log_k = -2
    weight = 1
    sto_v = 1
    sto_u = 1
  [../]
  [./b2_diff]
    type = CoupledDiffusionReactionSub
    variable = b
    v = a
    log_k = -2
    weight = 1
    sto_v = 1
    sto_u = 1
  [../]
  [./b2_conv]
    type = CoupledConvectionReactionSub
    variable = b
    v = a
    log_k = -2
    weight = 1
    sto_v = 1
    sto_u = 1
    p = pressure
  [../]
[]

[BCs]
  [./a_left]
    type = DirichletBC
    variable = a
    boundary = left
    value = 1.0e-2
  [../]
  [./a_right]
    type = ChemicalOutFlowBC
    variable = a
    boundary = right
  [../]
  [./b_left]
    type = DirichletBC
    variable = b
    boundary = left
    value = 1.0e-2
  [../]
  [./b_right]
    type = ChemicalOutFlowBC
    variable = b
    boundary = right
  [../]
[]

[Materials]
  [./porous]
    type = GenericConstantMaterial
    prop_names = 'diffusivity conductivity porosity'
    prop_values = '1e-4 1e-4 0.2'
  [../]
[]

[Executioner]
  type = Transient
  solve_type = PJFNK
  nl_abs_tol = 1e-12
  end_time = 10
  dt = 10
[]

[Outputs]
  file_base = equilibrium_out
  exodus = true
  perf_graph = true
  print_linear_residuals = true
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

(modules/tensor_mechanics/test/tests/shell/static/pinched_cylinder_symm.i)

# Test for displacement of pinched cylinder
# Ref: Figure 10 and Table 6 from Dvorkin and Bathe, Eng. Comput., Vol. 1, 1984.

# A cylinder of radius 1 m and length 2 m (along Z axis) with clamped ends
# (at z = 0 and 2 m) is pinched at mid-length by placing point loads of 10 N
# at (1, 0, 1) and (-1, 0, 1). Due to the symmetry of the problem, only 1/8th
# of the cylinder needs to be modeled.

# The normalized series solution for the displacement at the loading point is
# w = Wc E t / P = 164.24; where Wc is the displacement in m, E is the Young's
# modulus, t is the thickness and P is the point load.

# For this problem, E = 1e6 Pa, L = 2 m, R = 1 m, t = 0.01 m, P = 10 N and
# Poisson's ratio = 0.3. FEM results from different mesh discretizations are
# presented below. Only the 10x10 mesh is included as a test.

# Mesh of 1/8 cylinder |  FEM/analytical (Moose) | FEM/analytical (Dvorkin)
#                      |ratio of normalized disp.| ratio of normalized disp.
#----------------------|-------------------------|-------------------------
#     10 x 10          |          0.806          |        0.83
#     20 x 20          |          1.06           |        0.96
#     40 x 40          |          0.95           |         -
#     80 x 160         |          0.96           |         -

# The results from FEM analysis matches well with the series solution and with
# the solution presented by Dvorkin and Bathe (1984).

[Mesh]
  [./mesh]
    type = FileMeshGenerator
    file = pinched_cyl_10_10.msh
  [../]
  [./block_100]
    type = ParsedSubdomainMeshGenerator
    input = mesh
    combinatorial_geometry = 'x > -1.1 & x < 1.1 & y > -1.1 & y < 1.1 & z > -0.1 & z < 2.1'
    block_id = 100
  [../]
  [./nodeset_1]
    type = BoundingBoxNodeSetGenerator
    input = block_100
    top_right = '1.1 1.1 0'
    bottom_left = '-1.1 -1.1 0'
    new_boundary = 'CD' #CD
  [../]
  [./nodeset_2]
    type = BoundingBoxNodeSetGenerator
    input = nodeset_1
    top_right = '1.1 1.1 1.0'
    bottom_left = '-1.1 -1.1 1.0'
    new_boundary = 'AB' #AB
  [../]
  [./nodeset_3]
    type = BoundingBoxNodeSetGenerator
    input = nodeset_2
    top_right = '0.02 1.1 1.0'
    bottom_left = '-0.1 0.98 0.0'
    new_boundary = 'AD' #AD
  [../]
  [./nodeset_4]
    type = BoundingBoxNodeSetGenerator
    input = nodeset_3
    top_right = '1.1 0.02 1.0'
    bottom_left = '0.98 -0.1 0.0'
    new_boundary = 'BC' #BC
  [../]
[]


[Variables]
  [./disp_x]
    order = FIRST
    family = LAGRANGE
  [../]
  [./disp_y]
    order = FIRST
    family = LAGRANGE
  [../]
  [./disp_z]
    order = FIRST
    family = LAGRANGE
  [../]
  [./rot_x]
    order = FIRST
    family = LAGRANGE
  [../]
  [./rot_y]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[BCs]
  [./simply_support_x]
    type = DirichletBC
    variable = disp_x
    boundary = 'CD AD'
    value = 0.0
  [../]
  [./simply_support_y]
    type = DirichletBC
    variable = disp_y
    boundary = 'CD BC'
    value = 0.0
  [../]
  [./simply_support_z]
    type = DirichletBC
    variable = disp_z
    boundary = 'CD AB'
    value = 0.0
  [../]
  [./simply_support_rot_x]
    type = DirichletBC
    variable = rot_x
    boundary = 'CD BC'
    value = 0.0
  [../]
  [./simply_support_rot_y]
    type = DirichletBC
    variable = rot_y
    boundary = 'CD AD'
    value = 0.0
  [../]
[]

[DiracKernels]
  [./point1]
    type = ConstantPointSource
    variable = disp_x
    point = '1 0 1'
    value = -2.5 # P = 10
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient
  solve_type = NEWTON
  line_search = 'none'
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-8
  dt = 1.0
  dtmin = 1.0
  end_time = 1.0
[]

[Kernels]
  [./solid_disp_x]
    type = ADStressDivergenceShell
    block = '100'
    component = 0
    variable = disp_x
    through_thickness_order = SECOND
  [../]
  [./solid_disp_y]
    type = ADStressDivergenceShell
    block = '100'
    component = 1
    variable = disp_y
    through_thickness_order = SECOND
  [../]
  [./solid_disp_z]
    type = ADStressDivergenceShell
    block = '100'
    component = 2
    variable = disp_z
    through_thickness_order = SECOND
  [../]
  [./solid_rot_x]
    type = ADStressDivergenceShell
    block = '100'
    component = 3
    variable = rot_x
    through_thickness_order = SECOND
  [../]
  [./solid_rot_y]
    type = ADStressDivergenceShell
    block = '100'
    component = 4
    variable = rot_y
    through_thickness_order = SECOND
  [../]
[]

[Materials]
  [./elasticity]
    type = ADComputeIsotropicElasticityTensorShell
    youngs_modulus = 1e6
    poissons_ratio = 0.3
    block = '100'
    through_thickness_order = SECOND
  [../]
  [./strain]
    type = ADComputeIncrementalShellStrain
    block = '100'
    displacements = 'disp_x disp_y disp_z'
    rotations = 'rot_x rot_y'
    thickness = 0.01
    through_thickness_order = SECOND
  [../]
  [./stress]
    type = ADComputeShellStress
    block = '100'
    through_thickness_order = SECOND
  [../]
[]

[Postprocessors]
  [./disp_z2]
    type = PointValue
    point = '1 0 1'
    variable = disp_x
  [../]
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/lagrangian/total/homogenization/convergence/sd-strain.i)

# 2D test with just strain control

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
  large_kinematics = false
  constraint_types = 'strain strain strain strain strain strain'
  ndim = 3
  macro_gradient = hvar
[]

[Mesh]
  [base]
    type = FileMeshGenerator
    file = '3d.exo'
  []

  [sidesets]
    type = SideSetsFromNormalsGenerator
    input = base
    normals = '-1 0 0
                1 0 0
                0 -1 0
                0 1 0
            '
              '    0 0 -1
                0 0 1'
    fixed_normal = true
    new_boundary = 'left right bottom top back front'
  []
[]

[Variables]
  [disp_x]
  []
  [disp_y]
  []
  [disp_z]
  []
  [hvar]
    family = SCALAR
    order = SIXTH
  []
[]

[ICs]
  [disp_x]
    type = RandomIC
    variable = disp_x
    min = -0.1
    max = 0.1
  []
  [disp_y]
    type = RandomIC
    variable = disp_y
    min = -0.1
    max = 0.1
  []
  [disp_z]
    type = RandomIC
    variable = disp_z
    min = -0.1
    max = 0.1
  []
  [hvar]
    type = ScalarConstantIC
    variable = hvar
    value = 0.1
  []
[]

[AuxVariables]
  [sxx]
    family = MONOMIAL
    order = CONSTANT
  []
  [syy]
    family = MONOMIAL
    order = CONSTANT
  []
  [sxy]
    family = MONOMIAL
    order = CONSTANT
  []
  [szz]
    family = MONOMIAL
    order = CONSTANT
  []
  [syz]
    family = MONOMIAL
    order = CONSTANT
  []
  [sxz]
    family = MONOMIAL
    order = CONSTANT
  []
  [exx]
    family = MONOMIAL
    order = CONSTANT
  []
  [eyy]
    family = MONOMIAL
    order = CONSTANT
  []
  [exy]
    family = MONOMIAL
    order = CONSTANT
  []
  [ezz]
    family = MONOMIAL
    order = CONSTANT
  []
  [eyz]
    family = MONOMIAL
    order = CONSTANT
  []
  [exz]
    family = MONOMIAL
    order = CONSTANT
  []
[]

[AuxKernels]
  [sxx]
    type = RankTwoAux
    variable = sxx
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 0
  []
  [syy]
    type = RankTwoAux
    variable = syy
    rank_two_tensor = pk1_stress
    index_i = 1
    index_j = 1
  []
  [sxy]
    type = RankTwoAux
    variable = sxy
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 1
  []

  [zz]
    type = RankTwoAux
    variable = szz
    rank_two_tensor = pk1_stress
    index_i = 2
    index_j = 2
  []
  [syz]
    type = RankTwoAux
    variable = syz
    rank_two_tensor = pk1_stress
    index_i = 1
    index_j = 2
  []
  [sxz]
    type = RankTwoAux
    variable = sxz
    rank_two_tensor = pk1_stress
    index_i = 0
    index_j = 2
  []

  [exx]
    type = RankTwoAux
    variable = exx
    rank_two_tensor = mechanical_strain
    index_i = 0
    index_j = 0
  []
  [eyy]
    type = RankTwoAux
    variable = eyy
    rank_two_tensor = mechanical_strain
    index_i = 1
    index_j = 1
  []
  [exy]
    type = RankTwoAux
    variable = exy
    rank_two_tensor = mechanical_strain
    index_i = 0
    index_j = 1
  []

  [ezz]
    type = RankTwoAux
    variable = ezz
    rank_two_tensor = mechanical_strain
    index_i = 2
    index_j = 2
  []
  [eyz]
    type = RankTwoAux
    variable = eyz
    rank_two_tensor = mechanical_strain
    index_i = 1
    index_j = 2
  []
  [exz]
    type = RankTwoAux
    variable = exz
    rank_two_tensor = mechanical_strain
    index_i = 0
    index_j = 2
  []
[]

[UserObjects]
  [integrator]
    type = HomogenizationConstraintIntegral
    targets = 'strain11 strain22 strain33 strain23 strain13 strain12'
    execute_on = 'initial linear'
  []
[]

[Kernels]
  [sdx]
    type = HomogenizedTotalLagrangianStressDivergence
    variable = disp_x
    component = 0
  []
  [sdy]
    type = HomogenizedTotalLagrangianStressDivergence
    variable = disp_y
    component = 1
  []
  [sdz]
    type = HomogenizedTotalLagrangianStressDivergence
    variable = disp_z
    component = 2
  []
[]

[ScalarKernels]
  [enforce]
    type = HomogenizationConstraintScalarKernel
    variable = hvar
    integrator = integrator
  []
[]

[Functions]
  [strain11]
    type = ParsedFunction
    value = '4.0e-2*t'
  []
  [strain22]
    type = ParsedFunction
    value = '-2.0e-2*t'
  []
  [strain33]
    type = ParsedFunction
    value = '8.0e-2*t'
  []
  [strain23]
    type = ParsedFunction
    value = '2.0e-2*t'
  []
  [strain13]
    type = ParsedFunction
    value = '-7.0e-2*t'
  []
  [strain12]
    type = ParsedFunction
    value = '1.0e-2*t'
  []
[]

[BCs]
  [Periodic]
    [x]
      variable = disp_x
      auto_direction = 'x y z'
    []
    [y]
      variable = disp_y
      auto_direction = 'x y z'
    []
    [z]
      variable = disp_z
      auto_direction = 'x y z'
    []
  []

  [fix1_x]
    type = DirichletBC
    boundary = "fix_all"
    variable = disp_x
    value = 0
  []
  [fix1_y]
    type = DirichletBC
    boundary = "fix_all"
    variable = disp_y
    value = 0
  []
  [fix1_z]
    type = DirichletBC
    boundary = "fix_all"
    variable = disp_z
    value = 0
  []

  [fix2_x]
    type = DirichletBC
    boundary = "fix_xy"
    variable = disp_x
    value = 0
  []
  [fix2_y]
    type = DirichletBC
    boundary = "fix_xy"
    variable = disp_y
    value = 0
  []

  [fix3_z]
    type = DirichletBC
    boundary = "fix_z"
    variable = disp_z
    value = 0
  []
[]

[Materials]
  [elastic_tensor_1]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 100000.0
    poissons_ratio = 0.3
    block = '1'
  []
  [elastic_tensor_2]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 120000.0
    poissons_ratio = 0.21
    block = '2'
  []
  [elastic_tensor_3]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 80000.0
    poissons_ratio = 0.4
    block = '3'
  []
  [elastic_tensor_4]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 76000.0
    poissons_ratio = 0.11
    block = '4'
  []
  [compute_stress]
    type = ComputeLagrangianLinearElasticStress
  []
  [compute_strain]
    type = ComputeLagrangianStrain
    homogenization_gradient_names = 'homogenization_gradient'
  []
  [compute_homogenization_gradient]
    type = ComputeHomogenizedLagrangianStrain
  []
[]

[Preconditioning]
  [smp]
    type = SMP
    full = true
  []
[]

[Postprocessors]
  [sxx]
    type = ElementAverageValue
    variable = sxx
    execute_on = 'initial timestep_end'
  []
  [syy]
    type = ElementAverageValue
    variable = syy
    execute_on = 'initial timestep_end'
  []
  [sxy]
    type = ElementAverageValue
    variable = sxy
    execute_on = 'initial timestep_end'
  []

  [szz]
    type = ElementAverageValue
    variable = szz
    execute_on = 'initial timestep_end'
  []
  [syz]
    type = ElementAverageValue
    variable = syz
    execute_on = 'initial timestep_end'
  []
  [sxz]
    type = ElementAverageValue
    variable = sxz
    execute_on = 'initial timestep_end'
  []

  [exx]
    type = ElementAverageValue
    variable = exx
    execute_on = 'initial timestep_end'
  []
  [eyy]
    type = ElementAverageValue
    variable = eyy
    execute_on = 'initial timestep_end'
  []
  [exy]
    type = ElementAverageValue
    variable = exy
    execute_on = 'initial timestep_end'
  []

  [ezz]
    type = ElementAverageValue
    variable = ezz
    execute_on = 'initial timestep_end'
  []
  [eyz]
    type = ElementAverageValue
    variable = eyz
    execute_on = 'initial timestep_end'
  []
  [exz]
    type = ElementAverageValue
    variable = exz
    execute_on = 'initial timestep_end'
  []
[]

[Executioner]
  type = Transient

  solve_type = 'newton'
  line_search = none

  #automatic_scaling = true

  petsc_options_iname = '-pc_type'
  petsc_options_value = 'lu'

  l_max_its = 2
  l_tol = 1e-14
  nl_max_its = 10
  nl_rel_tol = 1e-8
  nl_abs_tol = 1e-10

  start_time = 0.0
  dt = 0.2
  dtmin = 0.2
  end_time = 0.2
[]

[Outputs]
  exodus = false
  csv = false
[]

(modules/peridynamics/test/tests/auxkernels/boundary_offset_node_area_2D.i)

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Mesh]
  type = PeridynamicsMesh
  horizon_number = 3

  [./fmg]
    type = FileMeshGenerator
    file = 2D_square.e
  [../]
  [./mgpd]
    type = MeshGeneratorPD
    input = fmg
    retain_fe_mesh = false
  [../]
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
[]

[AuxVariables]
  [./gap_offset]
  [../]
  [./node_area]
  [../]
[]

[AuxKernels]
  [./gap_offset]
    type = BoundaryOffsetPD
    variable = gap_offset
  [../]
  [./node_area]
    type = NodalVolumePD
    variable = node_area
  [../]
[]

[Modules/Peridynamics/Mechanics/Master]
  [./blk1]
    formulation = BOND
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 1e6
    poissons_ratio = 0.3
  [../]

  [./material_pd]
    type = ComputeSmallStrainVariableHorizonMaterialBPD
  [../]
[]

[BCs]
  [./fix_x]
    type = DirichletBC
    variable = disp_x
    boundary = 1001
    value = 0
  [../]
  [./fix_y]
    type = DirichletBC
    variable = disp_y
    boundary = 1001
    value = 0
  [../]
[]

[Preconditioning]
  [./smp]
    type = SMP
    full = true
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'
  end_time = 1
[]

[Outputs]
  exodus = true
[]

(modules/contact/test/tests/sliding_block/sliding/frictional_02_penalty.i)

#  This is a benchmark test that checks constraint based frictional
#  contact using the penalty method.  In this test a constant
#  displacement is applied in the horizontal direction to simulate
#  a small block come sliding down a larger block.
#
#  A friction coefficient of 0.2 is used.  The gold file is run on one processor
#  and the benchmark case is run on a minimum of 4 processors to ensure no
#  parallel variability in the contact pressure and penetration results.
#

[Mesh]
  file = sliding_elastic_blocks_2d.e
  patch_size = 80
[]

[GlobalParams]
  volumetric_locking_correction = false
  displacements = 'disp_x disp_y'
[]

[AuxVariables]
  [./penetration]
  [../]
  [./inc_slip_x]
  [../]
  [./inc_slip_y]
  [../]
  [./accum_slip_x]
  [../]
  [./accum_slip_y]
  [../]
[]

[Functions]
  [./vertical_movement]
    type = ParsedFunction
    value = -t
  [../]
[]

[Modules/TensorMechanics/Master]
  [./all]
    add_variables = true
    strain = FINITE
  [../]
[]

[AuxKernels]
  [./zeroslip_x]
    type = ConstantAux
    variable = inc_slip_x
    boundary = 3
    execute_on = timestep_begin
    value = 0.0
  [../]
  [./zeroslip_y]
    type = ConstantAux
    variable = inc_slip_y
    boundary = 3
    execute_on = timestep_begin
    value = 0.0
  [../]
  [./accum_slip_x]
    type = AccumulateAux
    variable = accum_slip_x
    accumulate_from_variable = inc_slip_x
    execute_on = timestep_end
  [../]
  [./accum_slip_y]
    type = AccumulateAux
    variable = accum_slip_y
    accumulate_from_variable = inc_slip_y
    execute_on = timestep_end
  [../]
  [./penetration]
    type = PenetrationAux
    variable = penetration
    boundary = 3
    paired_boundary = 2
  [../]
[]

[Postprocessors]
  [./nonlinear_its]
    type = NumNonlinearIterations
    execute_on = timestep_end
  [../]
  [./penetration]
    type = NodalVariableValue
    variable = penetration
    nodeid = 222
  [../]
  [./contact_pressure]
    type = NodalVariableValue
    variable = contact_pressure
    nodeid = 222
  [../]
[]

[BCs]
  [./left_x]
    type = DirichletBC
    variable = disp_x
    boundary = 1
    value = 0.0
  [../]
  [./left_y]
    type = DirichletBC
    variable = disp_y
    boundary = 1
    value = 0.0
  [../]
  [./right_x]
    type = DirichletBC
    variable = disp_x
    boundary = 4
    value = -0.02
  [../]
  [./right_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 4
    function = vertical_movement
  [../]
[]

[Materials]
  [./left]
    type = ComputeIsotropicElasticityTensor
    block = '1 2'
    youngs_modulus = 1e6
    poissons_ratio = 0.3
  [../]
  [./stress]
    type = ComputeFiniteStrainElasticStress
    block = '1 2'
  [../]
[]


[Executioner]
  type = Transient
  solve_type = 'PJFNK'

  petsc_options = '-snes_ksp_ew'
  petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu     superlu_dist'

  line_search = 'none'

  l_max_its = 100
  nl_max_its = 1000
  dt = 0.1
  end_time = 15
  num_steps = 1000
  l_tol = 1e-6
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-6
  dtmin = 0.01

  [./Predictor]
    type = SimplePredictor
    scale = 1.0
  [../]
[]

[Outputs]
  interval = 10
  [./out]
    type = Exodus
    elemental_as_nodal = true
  [../]
  [./console]
    type = Console
    max_rows = 5
  [../]
[]

[Contact]
  [./leftright]
    secondary = 3
    primary = 2
    model = coulomb
    penalty = 1e+7
    friction_coefficient = 0.2
    formulation = penalty
    normal_smoothing_distance = 0.1
  [../]
[]

(modules/xfem/test/tests/solid_mechanics_basic/penny_crack.i)

[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
  volumetric_locking_correction = true
[]

[XFEM]
  qrule = volfrac
  output_cut_plane = true
[]

[Mesh]
  file = quarter_sym.e
[]

[UserObjects]
  [./circle_cut_uo]
    type = CircleCutUserObject
    cut_data = '-0.5 -0.5 0
                0.0 -0.5 0
                -0.5 0 0'
  [../]
[]

[AuxVariables]
  [./SED]
   order = CONSTANT
    family = MONOMIAL
  [../]
[]

[DomainIntegral]
  integrals = 'Jintegral'
  crack_front_points = '-0.5 0.0 0.0
                        -0.25 -0.07 0
                        -0.15 -0.15 0
                        -0.07 -0.25 0
                         0 -0.5 0'
  crack_end_direction_method = CrackDirectionVector
  crack_direction_vector_end_1 = '0 1 0'
  crack_direction_vector_end_2 = '1 0 0'
  crack_direction_method = CurvedCrackFront
  intersecting_boundary = '3 4' #It would be ideal to use this, but can't use with XFEM yet
  radius_inner = '0.3'
  radius_outer = '0.6'
  poissons_ratio = 0.3
  youngs_modulus = 207000
  block = 1
  incremental = true
[]

[Modules/TensorMechanics/Master]
  [./all]
    strain = FINITE
    add_variables = true
    generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
  [../]
[]

[AuxKernels]
  [./SED]
    type = MaterialRealAux
    variable = SED
    property = strain_energy_density
    execute_on = timestep_end
    block = 1
  [../]
[]

[Functions]
  [./top_trac_z]
    type = ConstantFunction
    value = 10
  [../]
[]


[BCs]
  [./top_z]
    type = FunctionNeumannBC
    boundary = 2
    variable = disp_z
    function = top_trac_z
  [../]
  [./bottom_x]
    type = DirichletBC
    boundary = 1
    variable = disp_x
    value = 0.0
  [../]
  [./bottom_y]
    type = DirichletBC
    boundary = 1
    variable = disp_y
    value = 0.0
  [../]
  [./bottom_z]
    type = DirichletBC
    boundary = 1
    variable = disp_z
    value = 0.0
  [../]
  [./sym_y]
    type = DirichletBC
    boundary = 3
    variable = disp_y
    value = 0.0
  [../]
  [./sym_x]
    type = DirichletBC
    boundary = 4
    variable = disp_x
    value = 0.0
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 207000
    poissons_ratio = 0.3
  [../]
  [./stress]
    type = ComputeFiniteStrainElasticStress
  [../]
[]

[Executioner]
  type = Transient

  solve_type = 'PJFNK'
  petsc_options_iname = '-ksp_gmres_restart -pc_type -pc_hypre_type -pc_hypre_boomeramg_max_iter'
  petsc_options_value = '201                hypre    boomeramg      8'

  line_search = 'none'

  [./Predictor]
    type = SimplePredictor
    scale = 1.0
  [../]

# controls for linear iterations
  l_max_its = 100
  l_tol = 1e-2

# controls for nonlinear iterations
  nl_max_its = 15
  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-10

# time control
  start_time = 0.0
  dt = 1.0
  end_time = 1.0
[]

[Outputs]
  file_base = penny_crack_out
  execute_on = timestep_end
  exodus = true
  [./console]
    type = Console
    output_linear = true
  [../]
[]

(test/tests/postprocessors/area_pp/area_pp.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 4
  ny = 4

  xmax = 1.2
  ymax = 2.3
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Postprocessors]
  [./right]
    type = AreaPostprocessor
    boundary = 'right'
    execute_on = 'initial timestep_end'
  [../]

  [./bottom]
    type = AreaPostprocessor
    boundary = 'bottom'
    execute_on = 'initial timestep_end'
  [../]

  [./all]
    type = AreaPostprocessor
    boundary = 'left right bottom top'
    execute_on = 'initial timestep_end'
  [../]
[]

[Executioner]
  type = Steady

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  csv = true
[]

(modules/tensor_mechanics/test/tests/multi/mc_wpt_1.i)

# checking for small deformation
# A single element is stretched by 1E-6m in x,y and z directions.
# stress_zz = Youngs Modulus*Strain = 2E6*1E-6 = 2 Pa
# wpt_tensile_strength is set to 1Pa
# Then the final stress should return to the yeild surface and its value should be 1pa.

[Mesh]
  type = GeneratedMesh
  dim = 3
  nx = 1
  ny = 1
  nz = 1
  xmin = -0.5
  xmax = 0.5
  ymin = -0.5
  ymax = 0.5
  zmin = -0.5
  zmax = 0.5
[]


[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
  [./disp_z]
  [../]
[]

[Kernels]
  [./TensorMechanics]
    displacements = 'disp_x disp_y disp_z'
  [../]
[]


[BCs]
  [./bottomx]
    type = DirichletBC
    variable = disp_x
    boundary = back
    value = 0.0
  [../]
  [./bottomy]
    type = DirichletBC
    variable = disp_y
    boundary = back
    value = 0.0
  [../]
  [./bottomz]
    type = DirichletBC
    variable = disp_z
    boundary = back
    value = 0.0
  [../]

  [./topx]
    type = DirichletBC
    variable = disp_x
    boundary = front
    value = 0E-6
  [../]
  [./topy]
    type = DirichletBC
    variable = disp_y
    boundary = front
    value = 0E-6
  [../]
  [./topz]
    type = DirichletBC
    variable = disp_z
    boundary = front
    value = 1E-6
  [../]
[]

[AuxVariables]
  [./stress_xx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_xy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_xz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_zz]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[AuxKernels]
  [./stress_xx]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xx
    index_i = 0
    index_j = 0
  [../]
  [./stress_xy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xy
    index_i = 0
    index_j = 1
  [../]
  [./stress_xz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xz
    index_i = 0
    index_j = 2
  [../]
  [./stress_yy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yy
    index_i = 1
    index_j = 1
  [../]
  [./stress_yz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yz
    index_i = 1
    index_j = 2
  [../]
  [./stress_zz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zz
    index_i = 2
    index_j = 2
  [../]
[]

[Postprocessors]
  [./s_xx]
    type = PointValue
    point = '0 0 0'
    variable = stress_xx
  [../]
  [./s_xy]
    type = PointValue
    point = '0 0 0'
    variable = stress_xy
  [../]
  [./s_xz]
    type = PointValue
    point = '0 0 0'
    variable = stress_xz
  [../]
  [./s_yy]
    type = PointValue
    point = '0 0 0'
    variable = stress_yy
  [../]
  [./s_yz]
    type = PointValue
    point = '0 0 0'
    variable = stress_yz
  [../]
  [./s_zz]
    type = PointValue
    point = '0 0 0'
    variable = stress_zz
  [../]
[]

[UserObjects]
  [./mc_coh]
    type = TensorMechanicsHardeningConstant
    value = 100
  [../]
  [./mc_phi]
    type = TensorMechanicsHardeningConstant
    value = 60
    convert_to_radians = true
  [../]
  [./mc_psi]
    type = TensorMechanicsHardeningConstant
    value = 5
    convert_to_radians = true
  [../]
  [./mc]
    type = TensorMechanicsPlasticMohrCoulomb
    cohesion = mc_coh
    friction_angle = mc_phi
    dilation_angle = mc_psi
    mc_tip_smoother = 4
    mc_edge_smoother = 25
    yield_function_tolerance = 1E-3
    internal_constraint_tolerance = 1E-9
  [../]
  [./str]
    type = TensorMechanicsHardeningConstant
    value = 1
  [../]
  [./wpt]
    type = TensorMechanicsPlasticWeakPlaneTensile
    tensile_strength = str
    yield_function_tolerance = 1E-6
    internal_constraint_tolerance = 1E-5
  [../]
[]

[Materials]
  [./mc]
    type = FiniteStrainMultiPlasticity
    block = 0
    disp_x = disp_x
    disp_y = disp_y
    disp_z = disp_z
    fill_method = symmetric_isotropic
    C_ijkl = '0 1E7'
    ep_plastic_tolerance = 1E-9
    plastic_models = 'mc wpt'
    debug_fspb = crash
    debug_jac_at_stress = '10 0 0 0 10 0 0 0 10'
    debug_jac_at_pm = 1
    debug_jac_at_intnl = 1
    debug_stress_change = 1E-5
    debug_pm_change = 1E-6
    debug_intnl_change = 1E-6
  [../]
[]


[Executioner]
  end_time = 1
  dt = 1
  type = Transient
[]


[Outputs]
  file_base = mc_wpt_1
  exodus = false
  [./csv]
    type = CSV
    [../]
[]

(modules/porous_flow/test/tests/numerical_diffusion/no_action.i)

# Using upwinded and mass-lumped PorousFlow Kernels: this is equivalent of fully_saturated_action.i with stabilization = Full
[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 100
  xmin = 0
  xmax = 1
[]

[GlobalParams]
  PorousFlowDictator = dictator
  gravity = '0 0 0'
[]

[Variables]
  [porepressure]
  []
  [tracer]
  []
[]

[ICs]
  [porepressure]
    type = FunctionIC
    variable = porepressure
    function = '1 - x'
  []
  [tracer]
    type = FunctionIC
    variable = tracer
    function = 'if(x<0.1,0,if(x>0.3,0,1))'
  []
[]

[Kernels]
  [mass0]
    type = PorousFlowMassTimeDerivative
    fluid_component = 0
    variable = tracer
  []
  [flux0]
    type = PorousFlowAdvectiveFlux
    fluid_component = 0
    variable = tracer
  []
  [mass1]
    type = PorousFlowMassTimeDerivative
    fluid_component = 1
    variable = porepressure
  []
  [flux1]
    type = PorousFlowAdvectiveFlux
    fluid_component = 1
    variable = porepressure
  []
[]

[BCs]
  [constant_injection_porepressure]
    type = DirichletBC
    variable = porepressure
    value = 1
    boundary = left
  []
  [no_tracer_on_left]
    type = DirichletBC
    variable = tracer
    value = 0
    boundary = left
  []
  [remove_component_1]
    type = PorousFlowPiecewiseLinearSink
    variable = porepressure
    boundary = right
    fluid_phase = 0
    pt_vals = '0 1E3'
    multipliers = '0 1E3'
    mass_fraction_component = 1
    use_mobility = true
    flux_function = 1E3
  []
  [remove_component_0]
    type = PorousFlowPiecewiseLinearSink
    variable = tracer
    boundary = right
    fluid_phase = 0
    pt_vals = '0 1E3'
    multipliers = '0 1E3'
    mass_fraction_component = 0
    use_mobility = true
    flux_function = 1E3
  []
[]

[Modules]
  [FluidProperties]
    [the_simple_fluid]
      type = SimpleFluidProperties
      bulk_modulus = 2E9
      thermal_expansion = 0
      viscosity = 1.0
      density0 = 1000.0
    []
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'porepressure tracer'
    number_fluid_phases = 1
    number_fluid_components = 2
  []
  [pc]
    type = PorousFlowCapillaryPressureConst
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
  []
  [ppss]
    type = PorousFlow1PhaseP
    porepressure = porepressure
    capillary_pressure = pc
  []
  [massfrac]
    type = PorousFlowMassFraction
    mass_fraction_vars = tracer
  []
  [simple_fluid]
    type = PorousFlowSingleComponentFluid
    fp = the_simple_fluid
    phase = 0
  []
  [relperm]
    type = PorousFlowRelativePermeabilityConst
    phase = 0
  []
  [porosity]
    type = PorousFlowPorosity
    porosity_zero = 0.1
  []
  [permeability]
    type = PorousFlowPermeabilityConst
    permeability = '1E-2 0 0   0 1E-2 0   0 0 1E-2'
  []
[]

[Preconditioning]
  active = basic
  [basic]
    type = SMP
    full = true
    petsc_options = '-ksp_diagonal_scale -ksp_diagonal_scale_fix'
    petsc_options_iname = '-pc_type -sub_pc_type -sub_pc_factor_shift_type -pc_asm_overlap'
    petsc_options_value = ' asm      lu           NONZERO                   2'
  []
  [preferred_but_might_not_be_installed]
    type = SMP
    full = true
    petsc_options_iname = '-pc_type -pc_factor_mat_solver_package'
    petsc_options_value = ' lu       mumps'
  []
[]

[VectorPostprocessors]
  [tracer]
    type = LineValueSampler
    start_point = '0 0 0'
    end_point = '1 0 0'
    num_points = 101
    sort_by = x
    variable = tracer
  []
[]

[Executioner]
  type = Transient
  solve_type = Newton
  end_time = 6
  dt = 6E-1
  nl_abs_tol = 1E-8
  timestep_tolerance = 1E-3
[]

[Outputs]
  [out]
    type = CSV
    execute_on = final
  []
[]

(test/tests/dirackernels/constant_point_source/2d_point_source.i)

[Mesh]
  [./square]
    type = GeneratedMeshGenerator
    nx = 2
    ny = 2
    dim = 2
  [../]
  uniform_refine = 4
[]

[Variables]
  active = 'u'

  [./u]
    order = FIRST
    family = LAGRANGE
  [../]

  [./v]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Kernels]
  active = 'diff'

  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[DiracKernels]
  active = 'point_source1 point_source2'
  [./point_source1]
    type = ConstantPointSource
    variable = u
    value = 1.0
    point = '0.2 0.3'
  [../]
  [./point_source2]
    type = ConstantPointSource
    variable = u
    value = -0.5
    point = '0.2 0.8'
  [../]
[]

[BCs]
  active = 'left right'

  [./left]
    type = DirichletBC
    variable = u
    boundary = 3
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 1
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
[]

[Outputs]
  file_base = 2d_out
  exodus = true
[]

(test/tests/meshgenerators/sidesets_bounding_box_generator/overlapping_sidesets.i)

[Mesh]
#active = 'gmg'
  [./gmg]
    type = GeneratedMeshGenerator
    dim = 3
    nx = 10
    ny = 10
    nz = 10
  []

  [./createNewSidesetOne]
    type = SideSetsFromBoundingBoxGenerator
    input = gmg
    boundary_id_old = 'bottom back left'
    boundary_id_new = 10
    bottom_left = '-1.1 -1.1 -1.1'
    top_right = '1.1 1.1 1.1'
    block_id = 0
    boundary_id_overlap = true
  []
  [./createNewSidesetTwo]
    type = SideSetsFromBoundingBoxGenerator
    input = createNewSidesetOne
    boundary_id_old = 'right bottom'
    boundary_id_new = 11
    bottom_left = '-1.1 -1.1 -1.1'
    top_right = '1.1 1.1 1.1'
    block_id = 0
    boundary_id_overlap = true
  []
  [./createNewSidesetThree]
    type = SideSetsFromBoundingBoxGenerator
    input = createNewSidesetTwo
    boundary_id_old = 'top front'
    boundary_id_new = 12
    bottom_left = '-1.1 -1.1 -1.1'
    top_right = '1.1 1.1 1.1'
    block_id = 0
    boundary_id_overlap = true
  [../]
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./BCone]
    type = DirichletBC
    variable = u
    boundary = 10
    value = 1
  [../]
  [./BCtwo]
    type = DirichletBC
    variable = u
    boundary = 11
    value = 1
  [../]
  [./BCthree]
    type = DirichletBC
    variable = u
    boundary = 12
    value = 0
  [../]
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(modules/contact/test/tests/verification/patch_tests/brick_1/brick1_template1.i)

[GlobalParams]
  volumetric_locking_correction = true
  displacements = 'disp_x disp_y disp_z'
[]

[Mesh]
  file = brick1_mesh.e
[]

[Problem]
  type = ReferenceResidualProblem
  extra_tag_vectors = 'ref'
  reference_vector = 'ref'
[]

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
  [./disp_z]
  [../]
[]

[AuxVariables]
  [./stress_xx]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_xy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./stress_zz]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./penetration]
  [../]
  [./saved_x]
  [../]
  [./saved_y]
  [../]
  [./saved_z]
  [../]
  [./diag_saved_x]
  [../]
  [./diag_saved_y]
  [../]
  [./diag_saved_z]
  [../]
  [./inc_slip_x]
  [../]
  [./inc_slip_y]
  [../]
  [./inc_slip_z]
  [../]
  [./accum_slip_x]
  [../]
  [./accum_slip_y]
  [../]
  [./accum_slip_z]
  [../]
[]

[Kernels]
  [./TensorMechanics]
    use_displaced_mesh = true
    save_in = 'saved_x saved_y saved_z'
    extra_vector_tags = 'ref'
  [../]
[]

[AuxKernels]
  [./stress_xx]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xx
    index_i = 0
    index_j = 0
    execute_on = timestep_end
  [../]
  [./stress_yy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yy
    index_i = 1
    index_j = 1
    execute_on = timestep_end
  [../]
  [./stress_xy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xy
    index_i = 0
    index_j = 1
    execute_on = timestep_end
  [../]
  [./stress_zz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zz
    index_i = 2
    index_j = 2
    execute_on = timestep_end
  [../]
  [./inc_slip_x]
    type = PenetrationAux
    variable = inc_slip_x
    execute_on = timestep_begin
    boundary = 4
    paired_boundary = 3
  [../]
  [./inc_slip_y]
    type = PenetrationAux
    variable = inc_slip_y
    execute_on = timestep_begin
    boundary = 4
    paired_boundary = 3
  [../]
  [./accum_slip_x]
    type = PenetrationAux
    variable = accum_slip_x
    execute_on = timestep_end
    boundary = 4
    paired_boundary = 3
  [../]
  [./accum_slip_y]
    type = PenetrationAux
    variable = accum_slip_y
    execute_on = timestep_end
    boundary = 4
    paired_boundary = 3
  [../]
  [./penetration]
    type = PenetrationAux
    variable = penetration
    boundary = 4
    paired_boundary = 3
  [../]
[]

[Postprocessors]
  [./bot_react_x]
    type = NodalSum
    variable = saved_x
    boundary = 1
  [../]
  [./bot_react_y]
    type = NodalSum
    variable = saved_y
    boundary = 1
  [../]
  [./top_react_x]
    type = NodalSum
    variable = saved_x
    boundary = 5
  [../]
  [./top_react_y]
    type = NodalSum
    variable = saved_y
    boundary = 5
  [../]
  [./ref_resid_x]
    type = NodalL2Norm
    execute_on = timestep_end
    variable = saved_x
  [../]
  [./ref_resid_y]
    type = NodalL2Norm
    execute_on = timestep_end
    variable = saved_y
  [../]
  [./sigma_yy]
    type = ElementAverageValue
    variable = stress_yy
  [../]
  [./sigma_zz]
    type = ElementAverageValue
    variable = stress_zz
  [../]
  [./disp_x5]
    type = NodalVariableValue
    nodeid = 4
    variable = disp_x
  [../]
  [./disp_x8]
    type = NodalVariableValue
    nodeid = 7
    variable = disp_x
  [../]
  [./disp_x13]
    type = NodalVariableValue
    nodeid = 12
    variable = disp_x
  [../]
  [./disp_x16]
    type = NodalVariableValue
    nodeid = 15
    variable = disp_x
  [../]
  [./disp_y5]
    type = NodalVariableValue
    nodeid = 4
    variable = disp_y
  [../]
  [./disp_y8]
    type = NodalVariableValue
    nodeid = 7
    variable = disp_y
  [../]
  [./disp_y13]
    type = NodalVariableValue
    nodeid = 12
    variable = disp_y
  [../]
  [./disp_y16]
    type = NodalVariableValue
    nodeid = 15
    variable = disp_y
  [../]
  [./_dt]
    type = TimestepSize
  [../]
  [./num_lin_it]
    type = NumLinearIterations
  [../]
  [./num_nonlin_it]
    type = NumNonlinearIterations
  [../]
[]

[BCs]
  [./bot_y]
    type = DirichletBC
    variable = disp_y
    boundary = 1
    value = 0.0
  [../]
  [./side_x]
    type = DirichletBC
    variable = disp_x
    boundary = 2
    value = 0.0
  [../]
  [./back_z]
    type = DirichletBC
    variable = disp_z
    boundary = 6
    value = 0.0
  [../]
  [./top_press]
    type = Pressure
    variable = disp_y
    boundary = 5
    factor = 109.89
  [../]
[]

[Materials]
  [./bot_elas_tens]
    type = ComputeIsotropicElasticityTensor
    block = '1'
    youngs_modulus = 1e6
    poissons_ratio = 0.3
  [../]
  [./bot_strain]
    type = ComputeFiniteStrain
    block = '1'
  [../]
  [./bot_stress]
    type = ComputeFiniteStrainElasticStress
    block = '1'
  [../]
  [./top_elas_tens]
    type = ComputeIsotropicElasticityTensor
    block = '2'
    youngs_modulus = 1e6
    poissons_ratio = 0.3
  [../]
  [./top_strain]
    type = ComputeFiniteStrain
    block = '2'
  [../]
  [./top_stress]
    type = ComputeFiniteStrainElasticStress
    block = '2'
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_factor_mat_solver_type'
  petsc_options_value = 'lu     superlu_dist'

  line_search = 'none'

  nl_abs_tol = 1e-9
  nl_rel_tol = 1e-8
  l_max_its = 50
  nl_max_its = 100
  dt = 1.0
  end_time = 1.0
  num_steps = 10
  dtmin = 1.0
  l_tol = 1e-5
[]

[VectorPostprocessors]
  [./x_disp]
    type = NodalValueSampler
    variable = disp_x
    boundary = '1 3 4 5'
    sort_by = id
  [../]
  [./y_disp]
    type = NodalValueSampler
    variable = disp_y
    boundary = '1 3 4 5'
    sort_by = id
  [../]
  [./cont_press]
    type = NodalValueSampler
    variable = contact_pressure
    boundary = '3'
    sort_by = id
  [../]
[]

[Outputs]
  print_linear_residuals = true
  perf_graph = true
  [./exodus]
    type = Exodus
    elemental_as_nodal = true
  [../]
  [./console]
    type = Console
    max_rows = 5
  [../]
  [./chkfile]
    type = CSV
    show = 'bot_react_x bot_react_y disp_x5 disp_x8 disp_x13 disp_x16 disp_y5 disp_y8 disp_y13 disp_y16 stress_yy stress_zz top_react_x top_react_y x_disp y_disp cont_press'
    execute_vector_postprocessors_on = timestep_end
  [../]
  [./outfile]
    type = CSV
    delimiter = ' '
    execute_vector_postprocessors_on = none
  [../]
[]

[Contact]
  [./leftright]
    secondary = 3
    primary = 4
    normalize_penalty = true
    tangential_tolerance = 1e-3
    penalty = 1e+9
  [../]
[]

(modules/porous_flow/test/tests/poroperm/PermFromPoro04.i)

# Testing permeability from porosity
# Trivial test, checking calculated permeability is correct
# k = k_anisotropic * k
# with log k = A * phi + B

[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 3
  xmin = 0
  xmax = 3
[]

[GlobalParams]
  block = 0
  PorousFlowDictator = dictator
[]

[Variables]
  [pp]
    [InitialCondition]
      type = ConstantIC
      value = 0
    []
  []
[]

[Kernels]
  [flux]
    type = PorousFlowAdvectiveFlux
    gravity = '0 0 0'
    variable = pp
  []
[]

[BCs]
  [ptop]
    type = DirichletBC
    variable = pp
    boundary = right
    value = 0
  []
  [pbase]
    type = DirichletBC
    variable = pp
    boundary = left
    value = 1
  []
[]

[AuxVariables]
  [poro]
    order = CONSTANT
    family = MONOMIAL
  []
  [perm_x]
    order = CONSTANT
    family = MONOMIAL
  []
  [perm_y]
    order = CONSTANT
    family = MONOMIAL
  []
  [perm_z]
    order = CONSTANT
    family = MONOMIAL
  []
[]

[AuxKernels]
  [poro]
    type = PorousFlowPropertyAux
    property = porosity
    variable = poro
  []
  [perm_x]
    type = PorousFlowPropertyAux
    property = permeability
    variable = perm_x
    row = 0
    column = 0
  []
  [perm_y]
    type = PorousFlowPropertyAux
    property = permeability
    variable = perm_y
    row = 1
    column = 1
  []
  [perm_z]
    type = PorousFlowPropertyAux
    property = permeability
    variable = perm_z
    row = 2
    column = 2
  []
[]

[Postprocessors]
  [perm_x_bottom]
    type = PointValue
    variable = perm_x
    point = '0 0 0'
  []
  [perm_y_bottom]
    type = PointValue
    variable = perm_y
    point = '0 0 0'
  []
  [perm_z_bottom]
    type = PointValue
    variable = perm_z
    point = '0 0 0'
  []
  [perm_x_top]
    type = PointValue
    variable = perm_x
    point = '3 0 0'
  []
  [perm_y_top]
    type = PointValue
    variable = perm_y
    point = '3 0 0'
  []
  [perm_z_top]
    type = PointValue
    variable = perm_z
    point = '3 0 0'
  []
[]

[UserObjects]
  [dictator]
    type = PorousFlowDictator
    porous_flow_vars = 'pp'
    number_fluid_phases = 1
    number_fluid_components = 1
  []
  [pc]
    type = PorousFlowCapillaryPressureVG
    # unimportant in this fully-saturated test
    m = 0.8
    alpha = 1e-4
  []
[]

[Modules]
  [FluidProperties]
    [simple_fluid]
      type = SimpleFluidProperties
      bulk_modulus = 2.2e9
      viscosity = 1e-3
      density0 = 1000
      thermal_expansion = 0
    []
  []
[]

[Materials]
  [temperature]
    type = PorousFlowTemperature
  []
  [massfrac]
    type = PorousFlowMassFraction
  []
  [eff_fluid_pressure]
    type = PorousFlowEffectiveFluidPressure
  []
  [ppss]
    type = PorousFlow1PhaseP
    porepressure = pp
    capillary_pressure = pc
  []
  [simple_fluid]
    type = PorousFlowSingleComponentFluid
    fp = simple_fluid
    phase = 0
  []
  [porosity]
    type = PorousFlowPorosity
    porosity_zero = 0.1
  []
  [relperm]
    type = PorousFlowRelativePermeabilityCorey
    n = 0 # unimportant in this fully-saturated situation
    phase = 0
  []

  [permeability]
    type = PorousFlowPermeabilityExponential
    k_anisotropy = '1 0 0  0 2 0  0 0 0.1'
    poroperm_function = log_k
    A = 4.342945
    B = -8
  []
[]

[Preconditioning]
  [andy]
    type = SMP
    full = true
  []
[]

[Executioner]
  solve_type = Newton
  type = Steady
  l_tol = 1E-5
  nl_abs_tol = 1E-3
  nl_rel_tol = 1E-8
  l_max_its = 200
  nl_max_its = 400

  petsc_options_iname = '-pc_type -pc_asm_overlap -sub_pc_type -ksp_type -ksp_gmres_restart'
  petsc_options_value = ' asm      2              lu            gmres     200'
[]

[Outputs]
  csv = true
  execute_on = 'timestep_end'
[]

(modules/tensor_mechanics/test/tests/material_limit_time_step/elas_plas/nafems_nl1_lim.i)

#
# Tests material model IsotropicPlasticity with material based time stepper
# Boundary conditions from NAFEMS test NL1
#
[GlobalParams]
  order = FIRST
  family = LAGRANGE
  volumetric_locking_correction = true
  displacements = 'disp_x disp_y'
[]

[Mesh]#Comment
  file = one_elem2.e
[] # Mesh

[Variables]
  [./disp_x]
  [../]
  [./disp_y]
  [../]
[] # Variables

[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
  [../]
  [./vonmises]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./elastic_strain_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./plastic_strain_eff]
    order = CONSTANT
    family = MONOMIAL
  [../]
  [./tot_strain_yy]
    order = CONSTANT
    family = MONOMIAL
  [../]
[] # AuxVariables

[Kernels]
  [./TensorMechanics]
    use_displaced_mesh = true
  [../]
[]

[AuxKernels]
  [./stress_xx]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xx
    index_i = 0
    index_j = 0
  [../]
  [./stress_yy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_yy
    index_i = 1
    index_j = 1
  [../]
  [./stress_zz]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_zz
    index_i = 2
    index_j = 2
  [../]
  [./stress_xy]
    type = RankTwoAux
    rank_two_tensor = stress
    variable = stress_xy
    index_i = 0
    index_j = 1
  [../]
  [./vonmises]
    type = RankTwoScalarAux
    rank_two_tensor = stress
    variable = vonmises
    scalar_type = VonMisesStress
    execute_on = timestep_end
  [../]
  [./elastic_strain_yy]
    type = RankTwoAux
    rank_two_tensor = elastic_strain
    variable = elastic_strain_yy
    index_i = 1
    index_j = 1
  [../]
  [./plastic_strain_eff]
    type = MaterialRealAux
    property = effective_plastic_strain
    variable = plastic_strain_eff
  [../]
  [./tot_strain_yy]
    type = RankTwoAux
    rank_two_tensor = total_strain
    variable = tot_strain_yy
    index_i = 1
    index_j = 1
  [../]
[] # AuxKernels

[Functions]
  [./appl_dispx]
    type = PiecewiseLinear
    x = '0   1.0   2.0   3.0  4.0   5.0  6.0  7.0  8.0'
    y = '0.0 0.25e-4 0.50e-4 0.50e-4 0.50e-4 0.25e-4 0.0 0.0 0.0'
  [../]
  [./appl_dispy]
    type = PiecewiseLinear
    x = '0   1.0   2.0   3.0  4.0   5.0  6.0  7.0  8.0'
    y = '0.0 0.0  0.0 0.25e-4 0.50e-4 0.50e-4 0.50e-4  0.25e-4 0.0 '
  [../]
[]

[BCs]
  [./side_x]
    type = DirichletBC
    variable = disp_x
    boundary = 101
    value = 0.0
  [../]
  [./origin_x]
    type = DirichletBC
    variable = disp_x
    boundary = 103
    value = 0.0
  [../]
  [./bot_y]
    type = DirichletBC
    variable = disp_y
    boundary = 102
    value = 0.0
  [../]
  [./origin_y]
    type = DirichletBC
    variable = disp_y
    boundary = 103
    value = 0.0
  [../]
  [./top_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 1
    function = appl_dispy
  [../]
  [./right_x]
    type = FunctionDirichletBC
    variable = disp_x
    boundary = 2
    function = appl_dispx
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    block = 1
    youngs_modulus = 250e9
    poissons_ratio = 0.25
  [../]
  [./strain]
    type = ComputePlaneFiniteStrain
    block = 1
  [../]
  [./stress]
    type = ComputeMultipleInelasticStress
    inelastic_models = 'isoplas'
    block = 1
  [../]
  [./isoplas]
    type = IsotropicPlasticityStressUpdate
    yield_stress = 5e6
    hardening_constant = 0.0
    relative_tolerance = 1e-20
    absolute_tolerance = 1e-8
    max_inelastic_increment = 0.000001
  [../]
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'

  nl_rel_tol = 1e-10
  nl_abs_tol = 1e-12
  l_tol = 1e-4
  l_max_its = 100
  nl_max_its = 20

  [./TimeStepper]
    type = IterationAdaptiveDT
    dt = 0.1
    time_t = '1.0  2.0  3.0  4.0  5.0  6.0  7.0  8.0'
    time_dt = '0.1 0.1  0.1  0.1  0.1  0.1  0.1  0.1'
    optimal_iterations = 30
    iteration_window = 9
    growth_factor = 2.0
    cutback_factor = 0.5
    timestep_limiting_postprocessor = matl_ts_min
  [../]

  start_time = 0.0
  num_steps = 1000
  end_time = 8.0
[] # Executioner

[Postprocessors]
  [./matl_ts_min]
    type = MaterialTimeStepPostprocessor
  [../]
  [./stress_xx]
    type = ElementAverageValue
    variable = stress_xx
  [../]
  [./stress_yy]
    type = ElementAverageValue
    variable = stress_yy
  [../]
  [./stress_zz]
    type = ElementAverageValue
    variable = stress_zz
  [../]
  [./vonmises]
    type = ElementAverageValue
    variable = vonmises
  [../]
  [./el_strain_yy]
    type = ElementAverageValue
    variable = elastic_strain_yy
  [../]
  [./plas_strain_eff]
    type = ElementAverageValue
    variable = plastic_strain_eff
  [../]
  [./tot_strain_yy]
    type = ElementAverageValue
    variable = tot_strain_yy
  [../]
  [./disp_x1]
    type = NodalVariableValue
    nodeid = 0
    variable = disp_x
  [../]
  [./disp_x4]
    type = NodalVariableValue
    nodeid = 3
    variable = disp_x
  [../]
  [./disp_y1]
    type = NodalVariableValue
    nodeid = 0
    variable = disp_y
  [../]
  [./disp_y4]
    type = NodalVariableValue
    nodeid = 3
    variable = disp_y
  [../]
  [./_dt]
    type = TimestepSize
  [../]
[]

[Outputs]
  exodus = true
  csv = true
  [./console]
    type = Console
    output_linear = true
  [../]
[] # Outputs

(test/tests/controls/error/non_existing_dependency.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Controls]
  [./ctrl]
    type = TestControl
    test_type = 'real'
    parameter = 'BCs/left/value'
    execute_on = 'initial timestep_begin'
    depends_on = 'no-control'
  [../]
[]

(test/tests/transfers/multiapp_conservative_transfer/sub_conservative_transfer.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 20
  ny = 20
  xmin = 0.05
  xmax = 1.2
  ymin = 0.05
  ymax = 1.1
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]

  [./coupledforce]
    type = CoupledForce
    variable = u
    v = aux_u
  [../]
[]

[AuxVariables]
  [./aux_u]
    family = LAGRANGE
    order = FIRST
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Postprocessors]
  [./to_postprocessor]
    type = ElementIntegralVariablePostprocessor
    variable = aux_u
    execute_on = 'transfer'
  [../]
[]

[Problem]
  type = FEProblem
[]

[Executioner]
  type = Steady
  solve_type = 'PJFNK'
  nl_abs_tol = 1e-12
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

(test/tests/test_harness/csvdiff.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 2
  ny = 2
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  [../]
  [./time]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 5 # Gold file only has 4 steps
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Postprocessors]
  [./num_dofs]
    type = NumDOFs
  [../]
[]

[Outputs]
  csv = true
  perf_graph = true
[]

(test/tests/restart/pointer_restart_errors/pointer_store_error.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[UserObjects]
  [./restartable_types]
    type = PointerStoreError
  [../]
[]

[Problem]
  type = FEProblem
  solve = false
[]

[Executioner]
  type = Steady
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
  [./checkpoint]
    type = Checkpoint
    num_files = 1
  [../]
[]

(test/tests/multiapps/picard/picard_abs_tol_master.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
  parallel_type = replicated
[]

[Variables]
  [./u]
  [../]
[]

[AuxVariables]
  [./v]
  [../]
[]

[Kernels]
  [./diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  [../]
  [./time]
    type = TimeDerivative
    variable = u
  [../]
  [./force_u]
    type = CoupledForce
    variable = u
    v = v
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 20
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
  nl_abs_tol = 1e-12
  fixed_point_max_its = 10
  fixed_point_abs_tol = 1e-9
[]

[Outputs]
  exodus = true
[]

[MultiApps]
  [./sub]
    type = TransientMultiApp
    app_type = MooseTestApp
    positions = '0 0 0'
    input_files = picard_sub.i
  [../]
[]

[Transfers]
  [./v_from_sub]
    type = MultiAppNearestNodeTransfer
    from_multi_app = sub
    source_variable = v
    variable = v
  [../]
  [./u_to_sub]
    type = MultiAppNearestNodeTransfer
    to_multi_app = sub
    source_variable = u
    variable = u
  [../]
[]

(modules/tensor_mechanics/test/tests/crystal_plasticity/monolithic_material_based/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 = PropertyReadFile
    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
  [../]
[]

(modules/contact/test/tests/multiple_contact_pairs/multiple_pairs.i)

starting_point = 2e-1
offset = 1e-2

[GlobalParams]
  displacements = 'disp_x disp_y'
[]

[Mesh]
  file = multiple_pairs.e
[]

[Modules/TensorMechanics/Master]
  [all]
    add_variables = true
    strain = FINITE
    generate_output = 'stress_xx'
  []
[]

[Materials]
  [stiffStuff]
    type = ComputeIsotropicElasticityTensor
    block = '1 2 3'
    youngs_modulus = 1e6
    poissons_ratio = 0.3
  []
  [stiffStuff_stress]
    type = ComputeFiniteStrainElasticStress
    block = '1 2 3'
  []
[]

[ICs]
  [disp_y]
    block = '2 3'
    variable = disp_y
    value = '${fparse starting_point + offset}'
    type = ConstantIC
  []
[]

[Contact]
  [action_name]
    primary = '20 20'
    secondary = '10 101'
    penalty = 1e7
    formulation = penalty
    tangential_tolerance = 0.0001
  []
[]

[BCs]
  [botx]
    type = DirichletBC
    variable = disp_x
    preset = false
    boundary = 40
    value = 0.0
  []
  [boty]
    type = DirichletBC
    variable = disp_y
    preset = false
    boundary = 40
    value = 0.0
  []
  [topy]
    type = FunctionDirichletBC
    variable = disp_y
    preset = false
    boundary = '30 301'
    function = '${starting_point} * cos(2 * pi / 40 * t) + ${offset}'
  []
  [leftx]
    type = FunctionDirichletBC
    variable = disp_x
    preset = false
    boundary = '50 501'
    function = '1e-2 * t'
  []
[]

[Executioner]
  type = Transient
  end_time = 60
  dt = 2.0
  dtmin = .1
  solve_type = 'PJFNK'
  petsc_options = '-snes_converged_reason -ksp_converged_reason -pc_svd_monitor '
                  '-snes_linesearch_monitor'
  petsc_options_iname = '-pc_type -pc_factor_shift_type -pc_factor_shift_amount -mat_mffd_err'
  petsc_options_value = 'lu       NONZERO               1e-15                   1e-5'
  l_max_its = 30
  nl_max_its = 20
  nl_abs_tol = 1e-9
  line_search = 'none'
  snesmf_reuse_base = false
[]

[Debug]
  show_var_residual_norms = true
[]

[Outputs]
  exodus = true
  csv = true
[]

[Preconditioning]
  [smp]
    type = SMP
    full = true
  []
[]

[Postprocessors]
  active = 'num_nl cumulative'
  [num_nl]
    type = NumNonlinearIterations
  []
  [cumulative]
    type = CumulativeValuePostprocessor
    postprocessor = num_nl
  []
[]

[VectorPostprocessors]
  [cont_press]
    type = NodalValueSampler
    variable = contact_pressure
    boundary = '10 101'
    sort_by = x
    execute_on = NONLINEAR
  []
[]

(modules/tensor_mechanics/test/tests/j_integral/j_integral_2d_mouth_dir.i)

#This tests the J-Integral evaluation capability.
#This is a 2d plane strain model
#Crack direction is defined using the crack mouth coordinates.
#The analytic solution for J1 is 2.434.  This model
#converges to that solution with a refined mesh.
#Reference: National Agency for Finite Element Methods and Standards (U.K.):
#Test 1.1 from NAFEMS publication "Test Cases in Linear Elastic Fracture
#Mechanics" R0020.

[GlobalParams]
  order = FIRST
  family = LAGRANGE
  displacements = 'disp_x disp_y'
  volumetric_locking_correction = true
[]

[Mesh]
  file = crack2d.e
[]

[AuxVariables]
  [./SED]
    order = CONSTANT
    family = MONOMIAL
  [../]
[]

[Functions]
  [./rampConstant]
    type = PiecewiseLinear
    x = '0. 1.'
    y = '0. 1.'
    scale_factor = -1e2
  [../]
[]

[DomainIntegral]
  integrals = JIntegral
  boundary = 800
  crack_direction_method = CrackMouth
  crack_mouth_boundary = 900
  2d = true
  axis_2d = 2
  radius_inner = '4.0 4.5 5.0 5.5 6.0'
  radius_outer = '4.5 5.0 5.5 6.0 6.5'
  output_q = false
  incremental = true
[]

[Modules/TensorMechanics/Master]
  [./master]
    strain = FINITE
    add_variables = true
    incremental = true
    generate_output = 'stress_xx stress_yy stress_zz vonmises_stress'
    planar_formulation = PLANE_STRAIN
  [../]
[]

[AuxKernels]
  [./SED]
    type = MaterialRealAux
    variable = SED
    property = strain_energy_density
    execute_on = timestep_end
  [../]
[]

[BCs]
  [./crack_y]
    type = DirichletBC
    variable = disp_y
    boundary = 100
    value = 0.0
  [../]

  [./no_x]
    type = DirichletBC
    variable = disp_x
    boundary = 700
    value = 0.0
  [../]

  [./Pressure]
    [./Side1]
      boundary = 400
      function = rampConstant
    [../]
  [../]
[]

[Materials]
  [./elasticity_tensor]
    type = ComputeIsotropicElasticityTensor
    youngs_modulus = 207000
    poissons_ratio = 0.3
  [../]
  [./elastic_stress]
    type = ComputeFiniteStrainElasticStress
  [../]
[]

[Executioner]
  type = Transient

  petsc_options = '-snes_ksp_ew'
  petsc_options_iname = '-ksp_gmres_restart'
  petsc_options_value = '101'

  line_search = 'none'

  l_max_its = 50
  nl_max_its = 20
  nl_rel_tol = 1e-12
  nl_abs_tol = 1e-5
  l_tol = 1e-2

  start_time = 0.0
  dt = 1

  end_time = 1
  num_steps = 1
[]

[Outputs]
  file_base = j_integral_2d_mouth_dir_out
  exodus = true
  csv = true
[]

(modules/porous_flow/test/tests/pressure_pulse/pressure_pulse_1d_action.i)

# Pressure pulse in 1D with 1 phase - transient
# This input file uses the PorousFlowFullySaturated Action.  For the non-Action version, see pressure_pulse_1d.i
[Mesh]
  type = GeneratedMesh
  dim = 1
  nx = 10
  xmin = 0
  xmax = 100
[]

[GlobalParams]
  PorousFlowDictator = dictator
[]

[Variables]
  [pp]
    initial_condition = 2E6
  []
[]

[PorousFlowFullySaturated]
  porepressure = pp
  gravity = '0 0 0'
  fp = simple_fluid
  stabilization = Full
[]

[Modules]
  [FluidProperties]
    [simple_fluid]
      type = SimpleFluidProperties
      bulk_modulus = 2e9
      density0 = 1000
      thermal_expansion = 0
      viscosity = 1e-3
    []
  []
[]

[Materials]
  [porosity]
    type = PorousFlowPorosityConst
    porosity = 0.1
  []
  [permeability]
    type = PorousFlowPermeabilityConst
    permeability = '1E-15 0 0 0 1E-15 0 0 0 1E-15'
  []
[]

[BCs]
  [left]
    type = DirichletBC
    boundary = left
    value = 3E6
    variable = pp
  []
[]

[Preconditioning]
  [andy]
    type = SMP
    full = true
  []
[]

[Executioner]
  type = Transient
  solve_type = Newton
  dt = 1E3
  end_time = 1E4
[]

[Postprocessors]
  [p000]
    type = PointValue
    variable = pp
    point = '0 0 0'
    execute_on = 'initial timestep_end'
  []
  [p010]
    type = PointValue
    variable = pp
    point = '10 0 0'
    execute_on = 'initial timestep_end'
  []
  [p020]
    type = PointValue
    variable = pp
    point = '20 0 0'
    execute_on = 'initial timestep_end'
  []
  [p030]
    type = PointValue
    variable = pp
    point = '30 0 0'
    execute_on = 'initial timestep_end'
  []
  [p040]
    type = PointValue
    variable = pp
    point = '40 0 0'
    execute_on = 'initial timestep_end'
  []
  [p050]
    type = PointValue
    variable = pp
    point = '50 0 0'
    execute_on = 'initial timestep_end'
  []
  [p060]
    type = PointValue
    variable = pp
    point = '60 0 0'
    execute_on = 'initial timestep_end'
  []
  [p070]
    type = PointValue
    variable = pp
    point = '70 0 0'
    execute_on = 'initial timestep_end'
  []
  [p080]
    type = PointValue
    variable = pp
    point = '80 0 0'
    execute_on = 'initial timestep_end'
  []
  [p090]
    type = PointValue
    variable = pp
    point = '90 0 0'
    execute_on = 'initial timestep_end'
  []
  [p100]
    type = PointValue
    variable = pp
    point = '100 0 0'
    execute_on = 'initial timestep_end'
  []
[]

[Outputs]
  file_base = pressure_pulse_1d
  print_linear_residuals = false
  csv = true
[]

(test/tests/multiapps/steffensen/transient_main.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 5
  ny = 5
  parallel_type = replicated
  uniform_refine = 1
[]

[Variables]
  [u]
  []
[]

[AuxVariables]
  [v]
  []
[]

[Kernels]
  [diff]
    type = CoefDiffusion
    variable = u
    coef = 0.1
  []
  [time]
    type = TimeDerivative
    variable = u
  []
  [force_u]
    type = CoupledForce
    variable = u
    v = v
  []
[]

[BCs]
  [left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  []
  [right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  []
[]

[Postprocessors]
  [coupling_its]
    type = NumFixedPointIterations
    execute_on = 'initial timestep_end'
  []
  [unorm]
    type = ElementL2Norm
    variable = u
  []
[]

[Executioner]
  type = Transient
  num_steps = 10
  dt = 0.1
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
  nl_abs_tol = 1e-14

  fixed_point_algorithm = 'steffensen'
  fixed_point_max_its = 30
  transformed_variables = 'u'
[]

[Outputs]
  csv = true
  exodus = false
[]

[MultiApps]
  [sub]
    type = TransientMultiApp
    app_type = MooseTestApp
    positions = '0 0 0'
    input_files = 'transient_sub.i'
    clone_master_mesh = true
    execute_on = 'timestep_begin'
  []
[]

[Transfers]
  [v_from_sub]
    type = MultiAppNearestNodeTransfer
    from_multi_app = sub
    source_variable = v
    variable = v
    execute_on = 'timestep_begin'
  []
  [u_to_sub]
    type = MultiAppNearestNodeTransfer
    to_multi_app = sub
    source_variable = u
    variable = u
    execute_on = 'timestep_begin'
  []
[]

(test/tests/postprocessors/element_time_derivative/el_time_deriv_1d_test.i)

[Mesh]
  type = GeneratedMesh
  dim = 1
  xmin = -5
  xmax = 5
  ymin = -1
  nx = 5
  elem_type = EDGE
[]

[Variables]
  [./u]
    order = FIRST
    family = LAGRANGE
    [./InitialCondition]
      type = ConstantIC
      value = 0
    [../]
  [../]
[]

[Functions]
  [./forcing_fn]
    type = ParsedFunction
    value = t*x+1
  [../]
[]

[Kernels]
  [./ffn]
    type = BodyForce
    variable = u
    function = forcing_fn
  [../]
  [./diffusion]
    type = Diffusion
    variable = u
  [../]
  [./timeDer]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./all]
    type = DirichletBC
    variable = u
    boundary = '0 1'
    value = 0
  [../]
[]

[Postprocessors]
  [./elementAvgTimeDerivative]
    type = ElementAverageTimeDerivative
    variable = u
  [../]
  [./elementAvgValue]
    type = ElementAverageValue
    variable = u
  [../]
[]

[Executioner]
  type = Transient
  scheme = implicit-euler

  solve_type = 'PJFNK'

  start_time = 0.0
  num_steps = 5
  dt = 0.1
[]

[Outputs]
  execute_on = 'timestep_end'
  file_base = out_el_time_deriv_1d
  csv = true
[]

(modules/tensor_mechanics/test/tests/weak_plane_shear/large_deform3.i)

# apply a number of "random" configurations and
# check that the algorithm returns to the yield surface
#
# must be careful here - we cannot put in arbitrary values of C_ijkl, otherwise the condition
# df/dsigma * C * flow_dirn < 0 for some stresses
# The important features that must be obeyed are:
# 0 = C_0222 = C_1222  (holds for transversely isotropic, for instance)
# C_0212 < C_0202 = C_1212 (holds for transversely isotropic)
[GlobalParams]
  displacements = 'disp_x disp_y disp_z'
[]

[Mesh]
  type = GeneratedMesh
  dim = 3
  xmin = -0.5
  xmax = 0.5
  ymin = -0.5
  ymax = 0.5
  zmin = -0.5
  zmax = 0.5
[]

[Modules/TensorMechanics/Master/all]
  strain = FINITE
  add_variables = true
[]

[BCs]
  [bottomx]
    type = DirichletBC
    variable = disp_x
    boundary = back
    value = 0.0
  []
  [bottomy]
    type = DirichletBC
    variable = disp_y
    boundary = back
    value = 0.0
  []
  [bottomz]
    type = DirichletBC
    variable = disp_z
    boundary = back
    value = 0.0
  []

  # the following are "random" deformations
  # each is O(1E-1) to provide large deformations
  [topx]
    type = FunctionDirichletBC
    variable = disp_x
    boundary = front
    function = '(sin(0.1*t)+x)/1E1'
  []
  [topy]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = front
    function = '(cos(t)+x*y)/1E1'
  []
  [topz]
    type = FunctionDirichletBC
    variable = disp_z
    boundary = front
    function = 'sin(0.4321*t)*x*y*z/1E1'
  []
[]

[AuxVariables]
  [yield_fcn]
    order = CONSTANT
    family = MONOMIAL
  []
[]

[AuxKernels]
  [yield_fcn_auxk]
    type = MaterialStdVectorAux
    property = plastic_yield_function
    index = 0
    variable = yield_fcn
  []
[]

[Postprocessors]
  [yield_fcn_at_zero]
    type = PointValue
    point = '0 0 0'
    variable = yield_fcn
    outputs = 'console'
  []
  [should_be_zero]
    type = FunctionValuePostprocessor
    function = should_be_zero_fcn
  []
[]

[Functions]
  [should_be_zero_fcn]
    type = ParsedFunction
    value = 'if(a<1E-3,0,a)'
    vars = 'a'
    vals = 'yield_fcn_at_zero'
  []
[]

[UserObjects]
  [coh]
    type = TensorMechanicsHardeningConstant
    value = 1E3
  []
  [tanphi]
    type = TensorMechanicsHardeningConstant
    value = 0.577350269
  []
  [tanpsi]
    type = TensorMechanicsHardeningConstant
    value = 0.08748866
  []
  [wps]
    type = TensorMechanicsPlasticWeakPlaneShear
    cohesion = coh
    tan_friction_angle = tanphi
    tan_dilation_angle = tanpsi
    smoother = 100
    yield_function_tolerance = 1E-3
    internal_constraint_tolerance = 1E-3
  []
[]

[Materials]
  [elasticity_tensor]
    type = ComputeElasticityTensor
    # the following is transversely isotropic, i think.
    fill_method = symmetric9
    C_ijkl = '3E9 1E9 3E9 3E9 3E9 6E9 1E9 1E9 9E9'
  []
  [mc]
    type = ComputeMultiPlasticityStress
    plastic_models = wps
    transverse_direction = '0 0 1'
    max_NR_iterations = 100
    ep_plastic_tolerance = 1E-3
    debug_fspb = crash
  []
[]


[Executioner]
  end_time = 1E4
  dt = 1
  type = Transient
[]


[Outputs]
  csv = true
[]

(modules/contact/examples/2d_indenter/indenter_rz_fine.i)

[GlobalParams]
  volumetric_locking_correction = true
  displacements = 'disp_x disp_y'
[]

[Problem]
  coord_type = RZ
  type = ReferenceResidualProblem
  reference_vector = 'ref'
  extra_tag_vectors = 'ref'
[]

[Mesh]
  patch_update_strategy = auto
  patch_size = 2
  partitioner = centroid
  centroid_partitioner_direction = y

  [simple_mesh]
    type = FileMeshGenerator
    file = indenter_rz_fine_bigsideset.e
  []
  # For NodalVariableValue to work with distributed mesh
  allow_renumbering = false
[]

[Functions]
  [disp_y]
    type = PiecewiseLinear
    x = '0.  1.0     2.0    2.6   3.0'
    y = '0.  -4.5   -5.7   -5.7  -4.0'
  []
[]

[Variables]
  [disp_x]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []

  [disp_y]
    order = FIRST
    family = LAGRANGE
    block = '1 2'
  []
[]

[AuxVariables]
  [saved_x]
  []
  [saved_y]
  []
[]

[Modules/TensorMechanics/Master]
  [all]
    add_variables = true
    strain = FINITE
    block = '1 2'
    use_automatic_differentiation = false
    generate_output = 'stress_xx stress_xy stress_xz stress_yy stress_zz'
    save_in = 'saved_x saved_y'
  []
[]

[BCs]
  # Symmetries of the Problem
  [symm_x_indenter]
    type = DirichletBC
    variable = disp_x
    boundary = 5
    value = 0.0
  []

  [symm_x_material]
    type = DirichletBC
    variable = disp_x
    boundary = 9
    value = 0.0
  []

  # Material should not fly away
  [material_base_y]
    type = DirichletBC
    variable = disp_y
    boundary = 8
    value = 0.0
  []

  # Drive indenter motion
  [disp_y]
    type = FunctionDirichletBC
    variable = disp_y
    boundary = 1
    function = disp_y
  []
[]

[Contact]
  [contact]
    secondary = 4
    primary = 6
    model = frictionless
    # Investigate von Mises stress at the edge
    correct_edge_dropping = true
    formulation = mortar
    c_normal = 1e+2
  []
[]

[UserObjects]
  [slip_rate_gss]
    type = CrystalPlasticitySlipRateGSS
    variable_size = 48
    slip_sys_file_name = input_slip_sys_bcc48.txt
    num_slip_sys_flowrate_props = 2
    flowprops = '1 48 0.0001 0.01'
    uo_state_var_name = state_var_gss
    slip_incr_tol = 10.0
    block = 2
  []
  [slip_resistance_gss]
    type = CrystalPlasticitySlipResistanceGSS
    variable_size = 48
    uo_state_var_name = state_var_gss
    block = 2
  []
  [state_var_gss]
    type = CrystalPlasticityStateVariable
    variable_size = 48
    groups = '0 24 48'
    group_values = '900 1000' #120
    uo_state_var_evol_rate_comp_name = state_var_evol_rate_comp_gss
    scale_factor = 1.0
    block = 2
  []
  [state_var_evol_rate_comp_gss]
    type = CrystalPlasticityStateVarRateComponentGSS
    variable_size = 48
    hprops = '1.4 1000 1200 2.5'
    uo_slip_rate_name = slip_rate_gss
    uo_state_var_name = state_var_gss
    block = 2
  []
[]

[Materials]
  [tensor]
    type = ComputeIsotropicElasticityTensor
    block = '1'
    youngs_modulus = 1.0e7
    poissons_ratio = 0.25
  []
  [stress]
    type = ComputeFiniteStrainElasticStress
    block = '1'
  []

  [crysp]
    type = FiniteStrainUObasedCP
    block = 2
    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'
    maximum_substep_iteration = 20
  []
  [elasticity_tensor]
    type = ComputeElasticityTensorCP
    block = 2
    C_ijkl = '265190 113650 113650 265190 113650 265190 75769 75769 75760'
    fill_method = symmetric9
  []
[]

[Preconditioning]
  [SMP]
    type = SMP
    full = true
  []
[]

[Executioner]
  type = Transient
  solve_type = 'PJFNK'
  petsc_options = '-snes_ksp_ew'

  petsc_options_iname = '-pc_type -snes_linesearch_type -pc_factor_shift_type '
                        '-pc_factor_shift_amount'
  petsc_options_value = 'lu       basic                 NONZERO               1e-15'
  line_search = 'none'
  automatic_scaling = true
  nl_abs_tol = 2.0e-07
  nl_rel_tol = 2.0e-07
  l_max_its = 40
  l_abs_tol = 1e-08
  l_tol = 1e-08
  start_time = 0.0
  dt = 0.01
  end_time = 3.0 # Executioner
[]

[Postprocessors]
  [maxdisp]
    type = NodalVariableValue
    nodeid = 39
    variable = disp_y
  []
  [resid_y]
    type = NodalSum
    variable = saved_y
    boundary = 1
  []
[]

[Outputs]
  [out]
    type = Exodus
    elemental_as_nodal = true
  []
  perf_graph = true
  csv = true
[]

(test/tests/transfers/multiapp_nearest_node_transfer/parallel_master.i)

# This test was introduced for Issue #804 which saw data corruption
# during NearestNodeTransfer when running in parallel

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 100
  ny = 100
  parallel_type = replicated
[]

[Variables]
  [./u]
     order = FIRST
     family = LAGRANGE
  [../]
[]

[AuxVariables]
  [./from_sub]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 1
  dt = 1

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'
[]

[Outputs]
  exodus = true
[]

[MultiApps]
  [./sub]
    type = TransientMultiApp
    app_type = MooseTestApp
    positions = '0 1.0 0.0'
    input_files = parallel_sub.i
    execute_on = 'timestep_end'
   [../]
[]

[Transfers]
# Surface to volume data transfer
  [./from_sub]
    type = MultiAppNearestNodeTransfer
    from_multi_app = sub
    source_variable = u
    variable = from_sub
    execute_on = 'timestep_end'
  [../]
[]

(test/tests/multiapps/sub_cycling/sub_negative.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  solve_type = PJFNK
  petsc_options_iname = '-pc_type -pc_hypre_type'
  petsc_options_value = 'hypre boomeramg'

  start_time = -1.0
  end_time = 0

  [TimeStepper]
    type = IterationAdaptiveDT
    cutback_factor = 0.666
    dt = 0.2
  []
[]

[Outputs]
  exodus = true
[]

(test/tests/kernels/forcing_function/forcing_function_error_check.i)

[Mesh]
  [./square]
    type = GeneratedMeshGenerator
    nx = 2
    ny = 2
    dim = 2
  [../]
  uniform_refine = 4
[]

[Variables]
  active = 'u'

  [./u]
    order = FIRST
    family = LAGRANGE
  [../]
[]

[Functions]
  active = 'forcing_func'

  [./forcing_func]
    type = ParsedFunction
    value = '"alpha*alpha*pi*pi*sin(alpha*pi*x)"'
    vars = 'alpha'
    vals = '16'
  [../]
[]

[Kernels]
  active = 'diff forcing'

  [./diff]
    type = Diffusion
    variable = u
  [../]

  [./forcing]
    type = BodyForce
    variable = u
    function = forcing_func
  [../]
[]

[BCs]
  active = 'left right'

  [./left]
    type = DirichletBC
    variable = u
    boundary = 3
    value = 0
  [../]

  [./right]
    type = DirichletBC
    variable = u
    boundary = 1
    value = 0
  [../]
[]

[Executioner]
  type = Steady
  nl_rel_tol = 1e-12
[]

[Outputs]
  execute_on = 'timestep_end'
  file_base = out
  exodus = true
[]

(test/tests/multiapps/petsc_options/sub.i)

[Mesh]
  type = GeneratedMesh
  dim = 2
  nx = 10
  ny = 10
[]

[Variables]
  [./u]
  [../]
[]

[Kernels]
  [./diff]
    type = Diffusion
    variable = u
  [../]
  [./td]
    type = TimeDerivative
    variable = u
  [../]
[]

[BCs]
  [./left]
    type = DirichletBC
    variable = u
    boundary = left
    value = 0
  [../]
  [./right]
    type = DirichletBC
    variable = u
    boundary = right
    value = 1
  [../]
[]

[Executioner]
  type = Transient
  num_steps = 1
  dt = 1

  solve_type = 'PJFNK'

  petsc_options_iname = '-pc_type -sub_pc_type'
  petsc_options_value = 'asm ilu'
[]

[Outputs]
  exodus = true
[]

(modules/tensor_mechanics/test/tests/strain_energy_density/rate_incr_model_elas_plas.i)