SolidModel.C File Reference

Go to the source code of this file.

Functions
	registerMooseObject ("SolidMechanicsApp", SolidModel)
template<>
InputParameters	validParams< SolidModel > ()

Function Documentation

registerMooseObject()

registerMooseObject	(	"SolidMechanicsApp"	,
		SolidModel
	)

validParams< SolidModel >()

template<>

InputParameters validParams< SolidModel >

(

)

Definition at line 31 of file SolidModel.C.

{
  MooseEnum formulation(
      "Nonlinear3D NonlinearRZ AxisymmetricRZ SphericalR Linear PlaneStrain NonlinearPlaneStrain");
  MooseEnum compute_method("NoShearRetention ShearRetention");
 
  InputParameters params = validParams<Material>();
  params.addParam<std::string>(
      "appended_property_name", "", "Name appended to material properties to make them unique");
  params.addParam<Real>("bulk_modulus", "The bulk modulus for the material.");
  params.addParam<Real>("lambda", "Lame's first parameter for the material.");
  params.addParam<Real>("poissons_ratio", "Poisson's ratio for the material.");
  params.addParam<FunctionName>("poissons_ratio_function",
                                "Poisson's ratio as a function of temperature.");
  params.addParam<Real>("shear_modulus", "The shear modulus of the material.");
  params.addParam<Real>("youngs_modulus", "Young's modulus of the material.");
  params.addParam<FunctionName>("youngs_modulus_function",
                                "Young's modulus as a function of temperature.");
  params.addParam<Real>("thermal_expansion", "The thermal expansion coefficient.");
  params.addParam<FunctionName>("thermal_expansion_function",
                                "Thermal expansion coefficient as a function of temperature.");
  params.addCoupledVar("temp", "Coupled Temperature");
  params.addParam<Real>(
      "stress_free_temperature",
      "The stress-free temperature.  If not specified, the initial temperature is used.");
  params.addParam<Real>("thermal_expansion_reference_temperature",
                        "Reference temperature for mean thermal expansion function.");
  MooseEnum cte_function_type("instantaneous mean");
  params.addParam<MooseEnum>("thermal_expansion_function_type",
                             cte_function_type,
                             "Type of thermal expansion function.  Choices are: " +
                                 cte_function_type.getRawNames());
  params.addParam<std::vector<Real>>("initial_stress",
                                     "The initial stress tensor (xx, yy, zz, xy, yz, zx)");
  params.addParam<std::string>(
      "cracking_release",
      "abrupt",
      "The cracking release type.  Choices are abrupt (default) and exponential.");
  params.addParam<Real>("cracking_stress",
                        0.0,
                        "The stress threshold beyond which cracking occurs.  Must be positive.");
  params.addParam<Real>(
      "cracking_residual_stress",
      0.0,
      "The fraction of the cracking stress allowed to be maintained following a crack.");
  params.addParam<Real>("cracking_beta", 1.0, "The coefficient used in the exponetional model.");
  params.addParam<MooseEnum>(
      "compute_method", compute_method, "The method  used in the stress calculation.");
  params.addParam<FunctionName>(
      "cracking_stress_function", "", "The cracking stress as a function of time and location");
  params.addParam<std::vector<unsigned int>>(
      "active_crack_planes", "Planes on which cracks are allowed (0,1,2 -> x,z,theta in RZ)");
  params.addParam<unsigned int>(
      "max_cracks", 3, "The maximum number of cracks allowed at a material point.");
  params.addParam<Real>("cracking_neg_fraction",
                        "The fraction of the cracking strain at which a "
                        "transitition begins during decreasing strain to "
                        "the original stiffness.");
  params.addParam<MooseEnum>("formulation",
                             formulation,
                             "Element formulation.  Choices are: " + formulation.getRawNames());
  params.addParam<std::string>("increment_calculation",
                               "RashidApprox",
                               "The algorithm to use when computing the "
                               "incremental strain and rotation (RashidApprox or "
                               "Eigen). For use with Nonlinear3D/RZ formulation.");
  params.addParam<bool>("large_strain",
                        false,
                        "Whether to include large strain terms in "
                        "AxisymmetricRZ, SphericalR, and PlaneStrain "
                        "formulations.");
  params.addParam<bool>("compute_JIntegral", false, "Whether to compute the J Integral.");
  params.addParam<bool>(
      "compute_InteractionIntegral", false, "Whether to compute the Interaction Integral.");
  params.addCoupledVar("disp_r", "The r displacement");
  params.addCoupledVar("disp_x", "The x displacement");
  params.addCoupledVar("disp_y", "The y displacement");
  params.addCoupledVar("disp_z", "The z displacement");
  params.addCoupledVar("strain_zz", "The zz strain");
  params.addCoupledVar("scalar_strain_zz", "The zz strain (scalar variable)");
  params.addParam<std::vector<std::string>>(
      "dep_matl_props", "Names of material properties this material depends on.");
  params.addParam<std::string>("constitutive_model", "ConstitutiveModel to use (optional)");
  params.addParam<bool>("volumetric_locking_correction",
                        true,
                        "Set to false to turn off volumetric locking correction");
  return params;
}

Referenced by validParams< AbaqusCreepMaterial >(), validParams< AbaqusUmatMaterial >(), validParams< CLSHPlasticMaterial >(), validParams< ConstitutiveModel >(), validParams< Elastic >(), validParams< LinearStrainHardening >(), validParams< PLC_LSH >(), and validParams< PowerLawCreep >().