oofem::StructuralMaterial Class Reference

#include <structuralmaterial.h>

Inheritance diagram for oofem::StructuralMaterial:

Collaboration diagram for oofem::StructuralMaterial:

Public Member Functions
	StructuralMaterial (int n, Domain *d)
bool	hasMaterialModeCapability (MaterialMode mode) const override
const char *	giveClassName () const override
void	initializeFrom (InputRecord &ir) override
void	giveInputRecord (DynamicInputRecord &input) override
void	giveCharacteristicMatrix (FloatMatrix &answer, MatResponseMode type, GaussPoint *gp, TimeStep *tStep) const override
	Returns characteristic matrix of the receiver.
void	giveCharacteristicVector (FloatArray &answer, FloatArray &flux, MatResponseMode type, GaussPoint *gp, TimeStep *tStep) const override
	Returns characteristic vector of the receiver.
virtual void	giveStiffnessMatrix (FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep) const
virtual void	giveRealStressVector (FloatArray &answer, GaussPoint *gp, const FloatArray &reducedStrain, TimeStep *tStep) const
virtual FloatArrayF< 6 >	giveRealStressVector_3d (const FloatArrayF< 6 > &strain, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector for second Piola-Kirchoff stress.
virtual FloatArrayF< 4 >	giveRealStressVector_PlaneStrain (const FloatArrayF< 4 > &strain, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector_3d.
virtual FloatArray	giveRealStressVector_StressControl (const FloatArray &reducedE, const IntArray &strainControl, GaussPoint *gp, TimeStep *tStep) const
	Iteratively calls giveRealStressVector_3d to find the stress controlled equal to zero·
virtual FloatArray	giveRealStressVector_ShellStressControl (const FloatArray &reducedE, const IntArray &strainControl, GaussPoint *gp, TimeStep *tStep) const
virtual FloatArrayF< 3 >	giveRealStressVector_PlaneStress (const FloatArrayF< 3 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector_StressControl.
virtual FloatArrayF< 1 >	giveRealStressVector_1d (const FloatArrayF< 1 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector_StressControl.
virtual FloatArrayF< 2 >	giveRealStressVector_Warping (const FloatArrayF< 2 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector_StressControl.
virtual FloatArrayF< 2 >	giveRealStressVector_2dBeamLayer (const FloatArrayF< 2 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector_StressControl.
virtual FloatArrayF< 5 >	giveRealStressVector_PlateLayer (const FloatArrayF< 5 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector_StressControl.
virtual FloatArrayF< 3 >	giveRealStressVector_Fiber (const FloatArrayF< 3 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector_StressControl.
virtual FloatArrayF< 3 >	giveRealStressVector_2dPlateSubSoil (const FloatArrayF< 3 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
	Default implementation is not provided.
virtual FloatArrayF< 6 >	giveRealStressVector_3dBeamSubSoil (const FloatArrayF< 6 > &reducedE, GaussPoint *gp, TimeStep *tStep) const
Methods associated with the First PK stress tensor.
Computes the first Piola-Kirchhoff stress vector for given total deformation gradient and integration point. The total deformation gradient is computed directly from displacement field at the given time step. The stress independent parts (temperature, eigenstrains) are subtracted in constitutive driver. The service should use previously reached equilibrium history variables. Also it should update temporary history variables in status according to newly reached state. The temporary history variables are moved into equilibrium ones after global structure equilibrium has been reached by iteration process. The First Piola-Kirchhoff stress vector is computed in Total Lagrangian mode Parameters answer Contains result. gp Integration point. reducedF Deformation gradient in in reduced form. tStep Current time step (most models are able to respond only when tStep is current time step).
virtual FloatArrayF< 9 >	giveFirstPKStressVector_3d (const FloatArrayF< 9 > &vF, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveRealStressVector for second Piola-Kirchoff stress.
virtual FloatArrayF< 5 >	giveFirstPKStressVector_PlaneStrain (const FloatArrayF< 5 > &vF, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveFirstPKStressVector_3d.
virtual FloatArray	giveFirstPKStressVector_StressControl (const FloatArray &reducedvF, const IntArray &FControl, GaussPoint *gp, TimeStep *tStep) const
	Iteratively calls giveRealStressVector_3d to find the stress controlled equal to zero·
virtual FloatArrayF< 4 >	giveFirstPKStressVector_PlaneStress (const FloatArrayF< 4 > &vF, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveFirstPKStressVector_StressControl.
virtual FloatArrayF< 1 >	giveFirstPKStressVector_1d (const FloatArrayF< 1 > &vF, GaussPoint *gp, TimeStep *tStep) const
	Default implementation relies on giveFirstPKStressVector_StressControl.
Public Member Functions inherited from oofem::Material
	Material (int n, Domain *d)
virtual	~Material ()=default
	Destructor.
virtual bool	isCharacteristicMtrxSymmetric (MatResponseMode rMode) const
virtual double	giveCharacteristicValue (MatResponseMode type, GaussPoint *gp, TimeStep *tStep) const
	Returns characteristic value of the receiver.
virtual double	give (int aProperty, GaussPoint *gp) const
virtual bool	hasProperty (int aProperty, GaussPoint *gp) const
virtual void	modifyProperty (int aProperty, double value, GaussPoint *gp)
double	giveCastingTime () const
virtual bool	isActivated (TimeStep *tStep) const
virtual bool	hasCastingTimeSupport () const
void	printYourself () override
	Prints receiver state on stdout. Useful for debugging.
virtual void	saveIPContext (DataStream &stream, ContextMode mode, GaussPoint *gp)
virtual void	restoreIPContext (DataStream &stream, ContextMode mode, GaussPoint *gp)
int	checkConsistency () override
virtual void	restoreConsistency (GaussPoint *gp)
virtual int	initMaterial (Element *element)
virtual MaterialStatus *	giveStatus (GaussPoint *gp) const
virtual int	packUnknowns (DataStream &buff, TimeStep *tStep, GaussPoint *ip)
virtual int	unpackAndUpdateUnknowns (DataStream &buff, TimeStep *tStep, GaussPoint *ip)
virtual int	estimatePackSize (DataStream &buff, GaussPoint *ip)
virtual double	predictRelativeComputationalCost (GaussPoint *gp)
virtual double	predictRelativeRedistributionCost (GaussPoint *gp)
virtual std::unique_ptr< MaterialStatus >	CreateStatus (GaussPoint *gp) const
virtual void	initTempStatus (GaussPoint *gp) const
void	saveContext (DataStream &stream, ContextMode mode) override
void	restoreContext (DataStream &stream, ContextMode mode) override
Public Member Functions inherited from oofem::FEMComponent
	FEMComponent (int n, Domain *d)
virtual	~FEMComponent ()=default
	Virtual destructor.
virtual const char *	giveInputRecordName () const =0
Domain *	giveDomain () const
virtual void	setDomain (Domain *d)
int	giveNumber () const
void	setNumber (int num)
virtual void	updateLocalNumbering (EntityRenumberingFunctor &f)
virtual void	initializeFrom (InputRecord &ir, int priority)
virtual void	initializeFinish ()
virtual void	postInitialize ()
	Performs post initialization steps. Called after all components are created and initialized.
virtual void	printOutputAt (FILE *file, TimeStep *tStep)
virtual Interface *	giveInterface (InterfaceType t)
std::string	errorInfo (const char *func) const
	Returns string for prepending output (used by error reporting macros).

Static Public Member Functions
static int	giveSymVI (int ind1, int ind2)
static int	giveVI (int ind1, int ind2)

Static Public Attributes
static std::array< std::array< int, 3 >, 3 >	vIindex
	Voigt index map.
static std::array< std::array< int, 3 >, 3 >	svIndex
	Symmetric Voigt index map.

Protected Attributes
double	referenceTemperature = 0.
	Reference temperature (temperature, when material has been built into structure).
MatResponseMode	SCStiffMode = TangentStiffness
	stifness mode used in stress control
double	SCRelTol = 1.e-3
	relative tolerance for stress control
double	SCAbsTol = 1.e-12
	absolute stress tolerance for stress control
int	SCMaxiter = 100000
	maximum iterations for stress-control
Protected Attributes inherited from oofem::Material
Dictionary	propertyDictionary
double	castingTime
int	preCastingTimeMat
	Material existing before casting time - optional parameter, zero by default.
Protected Attributes inherited from oofem::FEMComponent
int	number
	Component number.
Domain *	domain
	Link to domain object, useful for communicating with other FEM components.

Methods associated with the Cauchy stress tensor.
Computes the Cauchy stress vector for given increment of deformation gradient and given integration point. The increment of deformation gradient is computed directly from displacement field at the given time step and it is computed wrt configuration which was reached in the last step. The stress independent parts (temperature, eigenstrains) are subtracted in constitutive driver. The service should use previously reached equilibrium history variables. Also it should update temporary history variables in status according to newly reached state. The temporary history variables are moved into equilibrium ones after global structure equilibrium has been reached by iteration process. The Cauchy stress vector is computed in Updated Lagrangian mode Parameters answer Contains result. gp Integration point. reducedF Deformation gradient in in reduced form. tStep Current time step (most models are able to respond only when tStep is current time step).
class	CrossSection
class	StructuralCrossSection
class	SimpleCrossSection
class	LayeredCrossSection
static FloatMatrixF< 9, 9 >	convert_dSdE_2_dPdF_3D (const FloatMatrixF< 6, 6 > &dSdE, const FloatArrayF< 6 > &S, const FloatArrayF< 9 > &F)
static FloatMatrixF< 5, 5 >	convert_dSdE_2_dPdF_PlaneStrain (const FloatMatrixF< 4, 4 > &dSdE, const FloatArrayF< 4 > &S, const FloatArrayF< 5 > &F)
static FloatMatrixF< 4, 4 >	convert_dSdE_2_dPdF_PlaneStress (const FloatMatrixF< 3, 3 > &dSdE, const FloatArrayF< 3 > &S, const FloatArrayF< 4 > &F)
static FloatMatrixF< 1, 1 >	convert_dSdE_2_dPdF_1D (const FloatMatrixF< 1, 1 > &dSdE, const FloatArrayF< 1 > &S, const FloatArrayF< 1 > &F)
static void	computePrincipalValues (FloatArray &answer, const FloatArray &s, stressStrainPrincMode mode)
	Common functions for convenience.
static FloatArrayF< 3 >	computePrincipalValues (const FloatMatrixF< 3, 3 > &s)
static FloatArrayF< 3 >	computePrincipalValues (double I1, double I2, double I3)
static void	computePrincipalValDir (FloatArray &answer, FloatMatrix &dir, const FloatArray &s, stressStrainPrincMode mode)
static std::pair< FloatArrayF< 3 >, FloatMatrixF< 3, 3 > >	computePrincipalValDir (const FloatMatrixF< 3, 3 > &s)
static FloatArrayF< 6 >	computeDeviator (const FloatArrayF< 6 > &s)
static std::pair< FloatArrayF< 6 >, double >	computeDeviatoricVolumetricSplit (const FloatArrayF< 6 > &s)
static FloatArrayF< 6 >	computeDeviatoricVolumetricSum (const FloatArrayF< 6 > &dev, double mean)
static FloatArrayF< 6 >	applyDeviatoricElasticCompliance (const FloatArrayF< 6 > &stress, double EModulus, double nu)
static FloatArrayF< 6 >	applyDeviatoricElasticCompliance (const FloatArrayF< 6 > &stress, double GModulus)
static FloatArrayF< 6 >	applyDeviatoricElasticStiffness (const FloatArrayF< 6 > &strain, double EModulus, double nu)
static FloatArrayF< 6 >	applyDeviatoricElasticStiffness (const FloatArrayF< 6 > &strain, double GModulus)
static FloatArrayF< 6 >	applyElasticStiffness (const FloatArrayF< 6 > &strain, double EModulus, double nu)
static FloatArrayF< 6 >	applyElasticCompliance (const FloatArrayF< 6 > &stress, double EModulus, double nu)
static double	computeStressNorm (const FloatArrayF< 6 > &stress)
static double	computeFirstInvariant (const FloatArrayF< 6 > &s)
static double	computeSecondStressInvariant (const FloatArrayF< 6 > &s)
static double	computeThirdStressInvariant (const FloatArrayF< 6 > &s)
static double	computeFirstCoordinate (const FloatArrayF< 6 > &s)
static double	computeSecondCoordinate (const FloatArrayF< 6 > &s)
static double	computeThirdCoordinate (const FloatArrayF< 6 > &s)
static int	giveVoigtVectorMask (IntArray &answer, MaterialMode mmode)
static int	giveVoigtSymVectorMask (IntArray &answer, MaterialMode mmode)
static void	giveInvertedVoigtVectorMask (IntArray &answer, MaterialMode mmode)
static int	giveSizeOfVoigtVector (MaterialMode mmode)
static int	giveSizeOfVoigtSymVector (MaterialMode mmode)
static void	giveFullVectorForm (FloatArray &answer, const FloatArray &strainVector, MaterialMode matMode)
	Converts the reduced symmetric Voigt vector (2nd order tensor) to full form.
static void	giveFullVectorFormF (FloatArray &answer, const FloatArray &strainVector, MaterialMode matMode)
	Converts the reduced deformation gradient Voigt vector (2nd order tensor).
static void	giveFullSymVectorForm (FloatArray &answer, const FloatArray &vec, MaterialMode matMode)
	Converts the reduced unsymmetric Voigt vector (2nd order tensor) to full form.
static void	giveReducedVectorForm (FloatArray &answer, const FloatArray &vec, MaterialMode matMode)
	Converts the full symmetric Voigt vector (2nd order tensor) to reduced form.
static void	giveReducedSymVectorForm (FloatArray &answer, const FloatArray &vec, MaterialMode matMode)
	Converts the full unsymmetric Voigt vector (2nd order tensor) to reduced form.
static void	giveFullSymMatrixForm (FloatMatrix &answer, const FloatMatrix &red, MaterialMode matMode)
	Converts the full unsymmetric Voigt matrix (4th order tensor) to reduced form.
static void	giveReducedMatrixForm (FloatMatrix &answer, const FloatMatrix &full, MaterialMode matMode)
	Converts the full symmetric Voigt matrix (4th order tensor) to reduced form.
static void	giveReducedSymMatrixForm (FloatMatrix &answer, const FloatMatrix &full, MaterialMode matMode)
	Converts the full unsymmetric Voigt matrix (4th order tensor) to reduced form.
static FloatArrayF< 6 >	transformStrainVectorTo (const FloatMatrixF< 3, 3 > &base, const FloatArrayF< 6 > &strain, bool transpose=false)
static FloatArrayF< 6 >	transformStressVectorTo (const FloatMatrixF< 3, 3 > &base, const FloatArrayF< 6 > &stress, bool transpose=false)
static double	computeVonMisesStress (const FloatArray &currentStress)
static double	computeVonMisesStress_3D (const FloatArrayF< 6 > &stress)
static double	computeVonMisesStress_PlaneStress (const FloatArrayF< 3 > &stress)
static FloatMatrixF< 6, 6 >	giveStrainVectorTranformationMtrx (const FloatMatrixF< 3, 3 > &base, bool transpose=false)
static FloatMatrixF< 3, 3 >	give2DStrainVectorTranformationMtrx (const FloatMatrixF< 2, 2 > &base, bool transpose=false)
static FloatMatrixF< 6, 6 >	giveStressVectorTranformationMtrx (const FloatMatrixF< 3, 3 > &base, bool transpose=false)
static FloatMatrixF< 3, 3 >	givePlaneStressVectorTranformationMtrx (const FloatMatrixF< 2, 2 > &base, bool transpose=false)
static void	sortPrincDirAndValCloseTo (FloatArray &pVal, FloatMatrix &pDir, const FloatMatrix &toPDir)
virtual void	giveCauchyStressVector_3d (FloatArray &answer, GaussPoint *gp, const FloatArray &reducedF, TimeStep *tStep)
virtual void	giveCauchyStressVector_PlaneStrain (FloatArray &answer, GaussPoint *gp, const FloatArray &reducedF, TimeStep *tStep)
virtual void	giveCauchyStressVector_PlaneStress (FloatArray &answer, GaussPoint *gp, const FloatArray &reducedF, TimeStep *tStep)
virtual void	giveCauchyStressVector_1d (FloatArray &answer, GaussPoint *gp, const FloatArray &reducedF, TimeStep *tStep)
virtual void	giveEshelbyStressVector_PlaneStrain (FloatArray &answer, GaussPoint *gp, const FloatArray &reducedF, TimeStep *tStep)
virtual FloatArrayF< 6 >	giveThermalDilatationVector (GaussPoint *gp, TimeStep *tStep) const
double	giveReferenceTemperature ()
virtual FloatArray	computeStressIndependentStrainVector (GaussPoint *gp, TimeStep *tStep, ValueModeType mode) const
FloatArrayF< 6 >	computeStressIndependentStrainVector_3d (GaussPoint *gp, TimeStep *tStep, ValueModeType mode) const
virtual FloatMatrixF< 6, 6 >	give3dMaterialStiffnessMatrix (MatResponseMode mode, GaussPoint *gp, TimeStep *tStep) const
virtual void	giveStiffnessMatrix_dPdF (FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep)
virtual FloatMatrixF< 9, 9 >	give3dMaterialStiffnessMatrix_dPdF (MatResponseMode mode, GaussPoint *gp, TimeStep *tStep) const
virtual void	give3dMaterialStiffnessMatrix_dCde (FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep)
void	giveStressDependentPartOfStrainVector (FloatArray &answer, GaussPoint *gp, const FloatArray &reducedStrainVector, TimeStep *tStep, ValueModeType mode) const
int	setIPValue (const FloatArray &value, GaussPoint *gp, InternalStateType type) override
int	giveIPValue (FloatArray &answer, GaussPoint *gp, InternalStateType type, TimeStep *tStep) override
virtual FloatMatrixF< 3, 3 >	givePlaneStressStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual FloatMatrixF< 4, 4 >	givePlaneStressStiffnessMatrix_dPdF (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual void	givePlaneStressStiffMtrx_dCde (FloatMatrix &answer, MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep)
virtual FloatMatrixF< 4, 4 >	givePlaneStrainStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual FloatMatrixF< 5, 5 >	givePlaneStrainStiffnessMatrix_dPdF (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual void	givePlaneStrainStiffMtrx_dCde (FloatMatrix &answer, MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep)
virtual FloatMatrixF< 1, 1 >	give1dStressStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual FloatMatrixF< 1, 1 >	give1dStressStiffnessMatrix_dPdF (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual void	give1dStressStiffMtrx_dCde (FloatMatrix &answer, MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep)
virtual FloatMatrixF< 2, 2 >	give2dBeamLayerStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual FloatMatrixF< 5, 5 >	givePlateLayerStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual FloatMatrixF< 3, 3 >	giveFiberStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual FloatMatrixF< 3, 3 >	give2dPlateSubSoilStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const
virtual FloatMatrixF< 6, 6 >	give3dBeamSubSoilStiffMtrx (MatResponseMode mmode, GaussPoint *gp, TimeStep *tStep) const

Detailed Description

Todo

Update documentation

Abstract base class for all "structural" constitutive models. It declares common services provided by all structural material models. The implementation of these services is partly left on derived classes, which will implement constitutive model dependent part. Some general purpose services are implemented on this level. For details, how to store material model related history variables in integration points, see base class Material documentation.

The constitutive model can in general support several material modes (plane stress, plane strain ,... modes). Its capabilities can be examined using hasMaterialModeCapability service. It is generally assumed, that results obtained from constitutive model services are according to valid material mode. This mode is determined from integration point, which is compulsory parameter of all material services. Structural material introduces several stress/strain modes. Full and reduced formats of stress/strain vectors are introduced for convenience. The full format includes all components, even if they are zero due to stress/strain mode nature, but in the reduced format, only generally nonzero components are stored. (full format must used only if absolutely necessary, to avoid wasting of space. It is used by output routines to print results in general form). Methods for converting vectors between full and reduced format are provided.

If in particular mode particular stress component is zero, the corresponding strain is not computed and not stored in reduced vector, and in full vector there is zero value on corresponding position. On the other hand, if some zero strain is imposed, On the other hand, if zero strain component is imposed this condition must be taken into account in geometrical relations (at element level), and corresponding component are included stress/strain reduced vectors.

Structural material introduces following basic stress/strain modes

• 3d state - all components of general stress/strain vector are generally nonzero. General 3d strain vector has following components {sig_xx, sig_yy, sig_zz, tau_yz, tau_xz, tau_xy}
• plane stress - sig_zz = tau_yz = tau_xz = 0.
• plane strain - eps_z = gamma_xz = gamma_yz = 0. Note: as already described, if zero strain component is imposed (Plane strain, ..) this condition must be taken into account in geometrical relations, and corresponding component has to be included in reduced vector.
• 1d uniaxial state - sigma_y = sigma_z = tau_yz = tau_zx = tau_xy = 0.
• 2d beam layer - sigma_y=sigma_z=tau_zy=tau_xy = 0.
• 3d shell layer, 2d plate layer - sigma_z = 0.

Derived classes can of course extend those modes. Generally speaking, there are following major tasks, covered by declared services.

• Computing real/second PK stress vector (tensor) at integration point for given strain increment and updating its state (still temporary state, after overall equilibrium is reached).
• Updating its state (final state), when equilibrium has been reached.
• Returning its material stiffness (and/or flexibility) matrices for given material mode.
• Storing/restoring its context to stream.
• Returning its material properties.

Structural material services should not be called directly by elements. Instead, they always should pass their requests to corresponding cross section model. Cross section performs all necessary integration over its volume and invokes material model services.

Author

almost everyone

Jim Brouzoulis

Mikael Öhman

Definition at line 120 of file structuralmaterial.h.

Constructor & Destructor Documentation

StructuralMaterial()

oofem::StructuralMaterial::StructuralMaterial	(	int	n,
		Domain *	d )

Constructor. Creates material with given number, belonging to given domain.

Parameters

n	Material number.
d	Domain to which new material will belong.

Definition at line 66 of file structuralmaterial.C.

References oofem::Material::Material().

Referenced by oofem::AbaqusUserMaterial::AbaqusUserMaterial(), oofem::AnisotropicDamageMaterial::AnisotropicDamageMaterial(), oofem::BlatzKoMaterial::BlatzKoMaterial(), oofem::CompoDamageMat::CompoDamageMat(), oofem::ConcreteDPM::ConcreteDPM(), oofem::ConcreteDPM2::ConcreteDPM2(), oofem::DeformationTheoryMaterial::DeformationTheoryMaterial(), oofem::DruckerPragerPlasticitySM::DruckerPragerPlasticitySM(), oofem::DustMaterial::DustMaterial(), oofem::FCMMaterial::FCMMaterial(), oofem::RheoChainMaterial::give1dStressStiffMtrx(), oofem::RheoChainMaterial::give3dMaterialStiffnessMatrix(), oofem::LargeStrainMasterMaterial::give3dMaterialStiffnessMatrix_dPdF(), oofem::PerfectlyPlasticMaterial::giveEffectiveMaterialStiffnessMatrix(), oofem::RCM2Material::giveEffectiveMaterialStiffnessMatrix(), oofem::LargeStrainMasterMaterial::giveFirstPKStressVector_3d(), oofem::LargeStrainMasterMaterial::giveIPValue(), oofem::RCM2Material::giveNormalElasticStiffnessMatrix(), oofem::RheoChainMaterial::givePlaneStrainStiffMtrx(), oofem::RheoChainMaterial::givePlaneStressStiffMtrx(), oofem::RheoChainMaterial::giveRealStressVector(), oofem::HyperelasticMaterial1d::HyperelasticMaterial1d(), oofem::IsotropicAsymmetric1DMaterial::IsotropicAsymmetric1DMaterial(), oofem::IsotropicAsymmetric1DMaterial::IsotropicAsymmetric1DMaterial(), oofem::IsotropicDamageMaterial::IsotropicDamageMaterial(), oofem::LargeStrainMasterMaterial::LargeStrainMasterMaterial(), oofem::LatticeStructuralMaterial::LatticeStructuralMaterial(), oofem::LinearElasticMaterial::LinearElasticMaterial(), oofem::MFrontUserMaterial::MFrontUserMaterial(), oofem::MicroMaterial::MicroMaterial(), oofem::MicroplaneMaterial::MicroplaneMaterial(), oofem::MisesMat::MisesMat(), oofem::MooneyRivlinCompressibleMaterial::MooneyRivlinCompressibleMaterial(), oofem::MPlasticMaterial::MPlasticMaterial(), oofem::MPlasticMaterial2::MPlasticMaterial2(), oofem::OgdenCompressibleMaterial::OgdenCompressibleMaterial(), oofem::PerfectlyPlasticMaterial::PerfectlyPlasticMaterial(), oofem::PlasticMaterial::PlasticMaterial(), oofem::RankineMat::RankineMat(), oofem::RCM2Material::RCM2Material(), oofem::RheoChainMaterial::RheoChainMaterial(), oofem::SimoPisterMaterial::SimoPisterMaterial(), oofem::SimpleVitrificationMaterial::SimpleVitrificationMaterial(), oofem::SteelRelaxMat::SteelRelaxMat(), oofem::StructuralFE2Material::StructuralFE2Material(), oofem::StructuralMaterialSettable::StructuralMaterialSettable(), oofem::StructuralPythonMaterial::StructuralPythonMaterial(), oofem::TrabBone3D::TrabBone3D(), oofem::TrabBoneEmbed::TrabBoneEmbed(), oofem::TrabBoneMaterial::TrabBoneMaterial(), oofem::TutorialMaterial::TutorialMaterial(), oofem::WinklerMaterial::WinklerMaterial(), and oofem::WinklerPasternakMaterial::WinklerPasternakMaterial().

Member Function Documentation

applyDeviatoricElasticCompliance() [1/2]

FloatArrayF< 6 > oofem::StructuralMaterial::applyDeviatoricElasticCompliance ( const FloatArrayF< 6 > & stress, double EModulus, double nu )

static

Definition at line 1526 of file structuralmaterial.C.

References applyDeviatoricElasticCompliance().

Referenced by applyDeviatoricElasticCompliance(), oofem::TutorialMaterial::giveRealStressVector_3d(), oofem::DruckerPragerPlasticitySM::performLocalStressReturn(), and oofem::MisesMat::performPlasticityReturn().

applyDeviatoricElasticCompliance() [2/2]

FloatArrayF< 6 > oofem::StructuralMaterial::applyDeviatoricElasticCompliance ( const FloatArrayF< 6 > & stress, double GModulus )

static

Definition at line 1532 of file structuralmaterial.C.

applyDeviatoricElasticStiffness() [1/2]

FloatArrayF< 6 > oofem::StructuralMaterial::applyDeviatoricElasticStiffness ( const FloatArrayF< 6 > & strain, double EModulus, double nu )

static

Definition at line 1546 of file structuralmaterial.C.

References applyDeviatoricElasticStiffness().

Referenced by applyDeviatoricElasticStiffness(), oofem::DruckerPragerPlasticitySM::performLocalStressReturn(), and oofem::MisesMat::performPlasticityReturn().

applyDeviatoricElasticStiffness() [2/2]

FloatArrayF< 6 > oofem::StructuralMaterial::applyDeviatoricElasticStiffness ( const FloatArrayF< 6 > & strain, double GModulus )

static

Definition at line 1552 of file structuralmaterial.C.

applyElasticCompliance()

FloatArrayF< 6 > oofem::StructuralMaterial::applyElasticCompliance ( const FloatArrayF< 6 > & stress, double EModulus, double nu )

static

Definition at line 1580 of file structuralmaterial.C.

Referenced by oofem::ConcreteDPM::performPlasticityReturn().

applyElasticStiffness()

FloatArrayF< 6 > oofem::StructuralMaterial::applyElasticStiffness ( const FloatArrayF< 6 > & strain, double EModulus, double nu )

static

Definition at line 1565 of file structuralmaterial.C.

Referenced by oofem::ConcreteDPM::giveRealStressVector_3d(), and oofem::ConcreteDPM::performPlasticityReturn().

computeDeviator()

FloatArrayF< 6 > oofem::StructuralMaterial::computeDeviator ( const FloatArrayF< 6 > & s )

static

Computes split of receiver into deviatoric and volumetric part.

Parameters

dev	Deviatoric part.
s	Input vector

Returns

Volumetric part (diagonal components divided by 3).

Definition at line 1504 of file structuralmaterial.C.

References oofem::FloatArrayF< N >::at().

Referenced by oofem::ConcreteDPM2::computeDCosThetaDStress(), oofem::ConcreteDPM::computeDCosThetaDStress(), oofem::ConcreteDPM2::computeDDCosThetaDDStress(), oofem::ConcreteDPM2::computeDDRhoDDStress(), oofem::ConcreteDPM::computeDDRhoDDStress(), oofem::ConcreteDPM2::computeDRhoDStress(), oofem::ConcreteDPM::computeDRhoDStress(), oofem::DruckerPragerCutMat::computeReducedSSGradientMatrix(), oofem::DruckerPragerCutMat::computeStressGradientVector(), oofem::ConcreteDPM2Status::giveDeviatoricPlasticStrainNorm(), oofem::ConcreteDPMStatus::giveDeviatoricPlasticStrainNorm(), oofem::DruckerPragerPlasticitySM::giveRegAlgorithmicStiffMatrix(), and oofem::DruckerPragerPlasticitySM::giveVertexAlgorithmicStiffMatrix().

computeDeviatoricVolumetricSplit()

std::pair< FloatArrayF< 6 >, double > oofem::StructuralMaterial::computeDeviatoricVolumetricSplit ( const FloatArrayF< 6 > & s )

static

Definition at line 1489 of file structuralmaterial.C.

References oofem::FloatArrayF< N >::at().

Referenced by oofem::ConcreteDPM2::computeCoordinates(), oofem::ConcreteDPM2::computeDDGDDStress(), oofem::ConcreteDPM2::computeDDGDStressDKappa(), oofem::ConcreteDPM2::computeDDKappaDDeltaLambdaDStress(), oofem::ConcreteDPM2::computeDGDStress(), oofem::ConcreteDPM::computeTrialCoordinates(), oofem::DruckerPragerCutMat::computeYieldValueAt(), oofem::TutorialMaterial::giveRealStressVector_3d(), oofem::DruckerPragerPlasticitySM::performLocalStressReturn(), oofem::MisesMat::performPlasticityReturn(), oofem::ConcreteDPM2::performRegularReturn(), oofem::ConcreteDPM::performRegularReturn(), oofem::DustMaterial::performStressReturn(), oofem::ConcreteDPM2::performVertexReturn(), and oofem::ConcreteDPM::performVertexReturn().

computeDeviatoricVolumetricSum()

FloatArrayF< 6 > oofem::StructuralMaterial::computeDeviatoricVolumetricSum ( const FloatArrayF< 6 > & dev, double mean )

static

Definition at line 1516 of file structuralmaterial.C.

Referenced by oofem::DustMaterial::computePlastStrainDirM1(), oofem::DustMaterial::computePlastStrainDirM2(), oofem::DustMaterial::computePlastStrainDirM3(), oofem::TutorialMaterial::giveRealStressVector_3d(), oofem::DruckerPragerPlasticitySM::performLocalStressReturn(), oofem::MisesMat::performPlasticityReturn(), and oofem::DustMaterial::performStressReturn().

computeFirstCoordinate()

double oofem::StructuralMaterial::computeFirstCoordinate ( const FloatArrayF< 6 > & s )

static

Definition at line 1624 of file structuralmaterial.C.

References computeFirstInvariant().

computeFirstInvariant()

double oofem::StructuralMaterial::computeFirstInvariant ( const FloatArrayF< 6 > & s )

static

Definition at line 1600 of file structuralmaterial.C.

Referenced by computeFirstCoordinate().

computePrincipalValDir() [1/2]

std::pair< FloatArrayF< 3 >, FloatMatrixF< 3, 3 > > oofem::StructuralMaterial::computePrincipalValDir ( const FloatMatrixF< 3, 3 > & s )

static

Computes principal values and directions of stress or strain matrix (must be symmetric).

Parameters

dir	Principal directions (stored column wise).
s	Stress/strain matrix.

Returns

Computed principal values.

Definition at line 1317 of file structuralmaterial.C.

References oofem::eig().

computePrincipalValDir() [2/2]

void oofem::StructuralMaterial::computePrincipalValDir ( FloatArray & answer, FloatMatrix & dir, const FloatArray & s, stressStrainPrincMode mode )

static

Computes principal values and directions of stress or strain vector.

Parameters

answer	Computed principal values.
dir	Principal directions (stored column wise).
s	Stress/strain vector.
mode	Stress strain principal mode.

Definition at line 1337 of file structuralmaterial.C.

References oofem::FloatArray::at(), oofem::FloatMatrix::at(), oofem::FloatArray::giveSize(), oofem::FloatMatrix::jaco_(), OOFEM_SERROR, oofem::principal_deviatoricstress, oofem::principal_strain, oofem::principal_stress, oofem::FloatArray::resize(), oofem::FloatMatrix::resize(), oofem::FloatArray::zero(), and oofem::FloatMatrix::zero().

Referenced by oofem::FCMMaterial::checkStrengthCriterion(), oofem::ConcreteDPM2::computeAlpha(), oofem::ConcreteDPM2::computeDCosThetaDStress(), oofem::ConcreteDPM::computeDCosThetaDStress(), oofem::ConcreteDPM2::computeDDCosThetaDDStress(), oofem::IsotropicDamageMaterial1::computeEta(), oofem::DruckerPragerCutMat::computeStressGradientVector(), oofem::RankinePlasticMaterial::computeStressGradientVector(), giveIPValue(), oofem::MDM::giveRawMDMParameters(), oofem::FCMMaterial::giveRealStressVector(), oofem::RCM2Material::giveRealStressVector(), oofem::RCSDEMaterial::giveRealStressVector(), oofem::RCSDMaterial::giveRealStressVector(), oofem::RCSDNLMaterial::giveRealStressVector(), oofem::Concrete2::giveRealStressVector_PlateLayer(), oofem::IDNLMaterial::giveRemoteNonlocalStiffnessContribution(), oofem::ConcreteDPM2::initDamaged(), oofem::ConcreteDPM::initDamaged(), oofem::IsotropicDamageMaterial1::initDamaged(), oofem::MazarsMaterial::initDamaged(), oofem::NCPrincipalStrain::nucleateEnrichmentItems(), oofem::NCPrincipalStress::nucleateEnrichmentItems(), oofem::ConcreteDPM2::performRegularReturn(), oofem::ConcreteDPM::performRegularReturn(), and oofem::PLPrincipalStrain::propagateInterface().

computePrincipalValues() [1/3]

FloatArrayF< 3 > oofem::StructuralMaterial::computePrincipalValues ( const FloatMatrixF< 3, 3 > & s )

static

Compute principal values of a stress/strain matrix. Matrix must be symmetric.

Parameters

answer	Computed principal values.
s	Symmetric matrix.

Returns

Sorted eigenvalues.

Definition at line 1266 of file structuralmaterial.C.

References computePrincipalValues().

computePrincipalValues() [2/3]

FloatArrayF< 3 > oofem::StructuralMaterial::computePrincipalValues ( double I1, double I2, double I3 )

static

Compute principal values from invariants.

Parameters

I1	First invariant
I2	Second invariant
I3	Third invariant

Returns

Sorted list of principal values.

Definition at line 1279 of file structuralmaterial.C.

References oofem::clamp(), CUBIC_ZERO, and M_PI.

computePrincipalValues() [3/3]

void oofem::StructuralMaterial::computePrincipalValues ( FloatArray & answer, const FloatArray & s, stressStrainPrincMode mode )

static

Common functions for convenience.

Auxiliary member function that computes principal values of stress/strain vector.

Parameters

answer	Computed principal values.
s	Stress/strain vector which eigenvalues are computed.
mode	Stress strain principal mode..

Definition at line 1107 of file structuralmaterial.C.

References oofem::FloatArray::at(), oofem::cubic3r(), oofem::FloatArray::giveSize(), OOFEM_SERROR, oofem::principal_deviatoricstress, oofem::principal_strain, oofem::principal_stress, oofem::FloatArray::pY(), oofem::FloatArray::resize(), oofem::solve(), and oofem::FloatArray::zero().

Referenced by oofem::RCSDEMaterial::computeCurrEquivStrain(), oofem::RCSDMaterial::computeCurrEquivStrain(), oofem::MazarsMaterial::computeDamageParam(), oofem::ConcreteDPM::computeDuctilityMeasureDamage(), oofem::AnisotropicDamageMaterial::computeEquivalentStrain(), oofem::IsotropicDamageMaterial1::computeEquivalentStrain(), oofem::MazarsMaterial::computeEquivalentStrain(), computePrincipalValues(), oofem::ConcreteDPM2::computeRateFactor(), oofem::DruckerPragerCutMat::computeYieldValueAt(), oofem::RankinePlasticMaterial::computeYieldValueAt(), oofem::ConcreteFCMViscoElastic::giveIPValue(), oofem::DustMaterial::giveIPValue(), oofem::MPlasticMaterial2::giveIPValue(), oofem::MPlasticMaterial::giveIPValue(), oofem::PerfectlyPlasticMaterial::giveIPValue(), oofem::PlasticMaterial::giveIPValue(), giveIPValue(), and oofem::MPSDamMaterial::giveRealStressVector().

computeSecondCoordinate()

double oofem::StructuralMaterial::computeSecondCoordinate ( const FloatArrayF< 6 > & s )

static

Definition at line 1631 of file structuralmaterial.C.

References computeSecondStressInvariant().

Referenced by oofem::ConcreteDPM2::computeCoordinates(), oofem::ConcreteDPM2::computeDCosThetaDStress(), oofem::ConcreteDPM::computeDCosThetaDStress(), oofem::ConcreteDPM2::computeDDCosThetaDDStress(), oofem::ConcreteDPM2::computeDDGDDStress(), oofem::ConcreteDPM2::computeDDGDStressDKappa(), oofem::ConcreteDPM2::computeDDKappaDDeltaLambdaDStress(), oofem::ConcreteDPM2::computeDDRhoDDStress(), oofem::ConcreteDPM::computeDDRhoDDStress(), oofem::ConcreteDPM2::computeDGDStress(), oofem::ConcreteDPM2::computeDRhoDStress(), oofem::ConcreteDPM::computeDRhoDStress(), oofem::ConcreteDPM::computeTrialCoordinates(), oofem::ConcreteDPM2::performRegularReturn(), oofem::ConcreteDPM::performRegularReturn(), oofem::DustMaterial::performStressReturn(), oofem::ConcreteDPM2::performVertexReturn(), and oofem::ConcreteDPM::performVertexReturn().

computeSecondStressInvariant()

double oofem::StructuralMaterial::computeSecondStressInvariant ( const FloatArrayF< 6 > & s )

static

Definition at line 1606 of file structuralmaterial.C.

Referenced by oofem::DruckerPragerCutMat::computeReducedSSGradientMatrix(), computeSecondCoordinate(), oofem::DruckerPragerCutMat::computeStressGradientVector(), computeThirdCoordinate(), oofem::DruckerPragerCutMat::computeYieldValueAt(), oofem::TutorialMaterial::give3dMaterialStiffnessMatrix(), oofem::TutorialMaterial::giveRealStressVector_3d(), oofem::DruckerPragerPlasticitySM::giveRegAlgorithmicStiffMatrix(), oofem::DruckerPragerPlasticitySM::performLocalStressReturn(), and oofem::DruckerPragerPlasticitySM::performRegularReturn().

computeStressIndependentStrainVector()

FloatArray oofem::StructuralMaterial::computeStressIndependentStrainVector ( GaussPoint * gp, TimeStep * tStep, ValueModeType mode ) const

virtual

Computes reduced strain vector in given integration point, generated by internal processes in material, which are independent on loading in particular integration point. Default implementation takes into account temperature induced strains and eigenstrains.

Parameters

answer	Returned strain vector.
gp	Integration point.
tStep	Time step (most models are able to respond only when tStep is current time step).
mode	Determines response mode (Total or incremental).

Todo

Hack for loose gausspoints. We shouldn't ask for "gp->giveElement()". FIXME

Reimplemented in oofem::ConcreteFCMViscoElastic, and oofem::RheoChainMaterial.

Definition at line 2164 of file structuralmaterial.C.

References oofem::FloatArray::add(), oofem::FloatArray::at(), oofem::Element::computeGlobalCoordinates(), oofem::StructuralElement::computeResultingIPEigenstrainAt(), oofem::StructuralElement::computeResultingIPTemperatureAt(), oofem::FEMComponent::domain, oofem::GaussPoint::giveElement(), oofem::FieldManager::giveField(), oofem::GaussPoint::giveIntegrationRule(), oofem::TimeStep::giveIntrinsicTime(), oofem::GaussPoint::giveMaterialMode(), oofem::GaussPoint::giveNaturalCoordinates(), oofem::FEMComponent::giveNumber(), giveReducedSymVectorForm(), oofem::FloatArray::giveSize(), giveSizeOfVoigtSymVector(), giveThermalDilatationVector(), oofem::FloatArray::isEmpty(), oofem::FloatArray::isNotEmpty(), OOFEM_ERROR, and referenceTemperature.

Referenced by oofem::LatticeBondPlasticity::giveLatticeStress3d(), oofem::LatticeDamage::giveLatticeStress3d(), oofem::LatticeDamageViscoelastic::giveLatticeStress3d(), oofem::LatticeLinearElastic::giveLatticeStress3d(), oofem::LatticePlasticityDamage::giveLatticeStress3d(), oofem::LatticePlasticityDamageViscoelastic::giveLatticeStress3d(), oofem::LatticeViscoelastic::giveLatticeStress3d(), giveStressDependentPartOfStrainVector(), and oofem::LinearizedDilationForceAssembler::vectorFromElement().

computeStressIndependentStrainVector_3d()

FloatArrayF< 6 > oofem::StructuralMaterial::computeStressIndependentStrainVector_3d	(	GaussPoint *	gp,
		TimeStep *	tStep,
		ValueModeType	mode ) const

Todo

Hack for loose gausspoints. We shouldn't ask for "gp->giveElement()". FIXME

Definition at line 2268 of file structuralmaterial.C.

References oofem::FloatArray::at(), oofem::Element::computeGlobalCoordinates(), oofem::StructuralElement::computeResultingIPEigenstrainAt(), oofem::StructuralElement::computeResultingIPTemperatureAt(), oofem::FEMComponent::domain, oofem::GaussPoint::giveElement(), oofem::FieldManager::giveField(), oofem::GaussPoint::giveIntegrationRule(), oofem::TimeStep::giveIntrinsicTime(), oofem::GaussPoint::giveNaturalCoordinates(), oofem::FEMComponent::giveNumber(), oofem::FloatArray::giveSize(), oofem::FloatArrayF< N >::giveSize(), giveThermalDilatationVector(), oofem::FloatArray::isEmpty(), oofem::FloatArray::isNotEmpty(), OOFEM_ERROR, referenceTemperature, and oofem::zeros().

Referenced by oofem::LinearElasticMaterial::giveIPValue(), oofem::ConcreteDPM2::giveRealStressVector_3d(), oofem::ConcreteDPM::giveRealStressVector_3d(), oofem::DruckerPragerPlasticitySM::giveRealStressVector_3d(), oofem::DustMaterial::giveRealStressVector_3d(), oofem::LinearElasticMaterial::giveRealStressVector_3d(), oofem::SimpleVitrificationMaterial::giveRealStressVector_3d(), oofem::TutorialMaterial::giveRealStressVector_3d(), and oofem::LinearElasticMaterial::giveRealStressVector_3dDegeneratedShell().

computeStressNorm()

double oofem::StructuralMaterial::computeStressNorm ( const FloatArrayF< 6 > & stress )

static

Definition at line 1593 of file structuralmaterial.C.

Referenced by oofem::MisesMatGrad::give3dKappaMatrix(), oofem::MisesMat::give3dMaterialStiffnessMatrix(), oofem::MisesMatGrad::give3dMaterialStiffnessMatrix(), and oofem::MisesMat::performPlasticityReturn().

computeThirdCoordinate()

double oofem::StructuralMaterial::computeThirdCoordinate ( const FloatArrayF< 6 > & s )

static

Definition at line 1639 of file structuralmaterial.C.

References computeSecondStressInvariant(), and computeThirdStressInvariant().

Referenced by oofem::ConcreteDPM2::computeCoordinates(), oofem::ConcreteDPM2::computeDDKappaDDeltaLambdaDStress(), and oofem::ConcreteDPM::computeTrialCoordinates().

computeThirdStressInvariant()

double oofem::StructuralMaterial::computeThirdStressInvariant ( const FloatArrayF< 6 > & s )

static

Definition at line 1613 of file structuralmaterial.C.

Referenced by computeThirdCoordinate().

computeVonMisesStress()

double oofem::StructuralMaterial::computeVonMisesStress ( const FloatArray & currentStress )

static

Computes equivalent of von Mises stress. Returns 0 if six stress components do not exist on the material.

Parameters

currentStress

Stress vector given by 6 components.

Definition at line 1663 of file structuralmaterial.C.

References oofem::FloatArray::at(), computeVonMisesStress_3D(), computeVonMisesStress_PlaneStress(), and oofem::FloatArray::giveSize().

Referenced by giveIPValue().

computeVonMisesStress_3D()

double oofem::StructuralMaterial::computeVonMisesStress_3D ( const FloatArrayF< 6 > & stress )

static

Definition at line 1693 of file structuralmaterial.C.

References oofem::FloatArrayF< N >::at().

Referenced by computeVonMisesStress(), and giveIPValue().

computeVonMisesStress_PlaneStress()

double oofem::StructuralMaterial::computeVonMisesStress_PlaneStress ( const FloatArrayF< 3 > & stress )

static

Definition at line 1685 of file structuralmaterial.C.

References oofem::FloatArrayF< N >::at().

Referenced by computeVonMisesStress().

convert_dSdE_2_dPdF_1D()

FloatMatrixF< 1, 1 > oofem::StructuralMaterial::convert_dSdE_2_dPdF_1D ( const FloatMatrixF< 1, 1 > & dSdE, const FloatArrayF< 1 > & S, const FloatArrayF< 1 > & F )

static

Todo

is this really correct??

Definition at line 605 of file structuralmaterial.C.

References S.

convert_dSdE_2_dPdF_3D()

FloatMatrixF< 9, 9 > oofem::StructuralMaterial::convert_dSdE_2_dPdF_3D ( const FloatMatrixF< 6, 6 > & dSdE, const FloatArrayF< 6 > & S, const FloatArrayF< 9 > & F )

static

Definition at line 431 of file structuralmaterial.C.

References oofem::FloatArrayF< N >::at(), oofem::FloatMatrixF< N, M >::at(), oofem::eye(), giveSymVI(), giveVI(), and S.

Referenced by oofem::LargeStrainMasterMaterial::give3dMaterialStiffnessMatrix_dPdF(), and give3dMaterialStiffnessMatrix_dPdF().

convert_dSdE_2_dPdF_PlaneStrain()

FloatMatrixF< 5, 5 > oofem::StructuralMaterial::convert_dSdE_2_dPdF_PlaneStrain ( const FloatMatrixF< 4, 4 > & dSdE, const FloatArrayF< 4 > & S, const FloatArrayF< 5 > & F )

static

Definition at line 548 of file structuralmaterial.C.

References S.

convert_dSdE_2_dPdF_PlaneStress()

FloatMatrixF< 4, 4 > oofem::StructuralMaterial::convert_dSdE_2_dPdF_PlaneStress ( const FloatMatrixF< 3, 3 > & dSdE, const FloatArrayF< 3 > & S, const FloatArrayF< 4 > & F )

static

Definition at line 581 of file structuralmaterial.C.

References S.

give1dStressStiffMtrx()

FloatMatrixF< 1, 1 > oofem::StructuralMaterial::give1dStressStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing 1d stiffness matrix of receiver. Default implementation computes 3d stiffness matrix using give3dMaterialStiffnessMatrix and reduces it to 1d stiffness using reduce method described above. However, this reduction is quite time consuming and if it is possible, it is recommended to overload this method and provide direct method for computing particular stiffness matrix.

Parameters

mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Returns

Stiffness matrix.

Reimplemented in oofem::AnisotropicDamageMaterial, oofem::IsotropicAsymmetric1DMaterial, oofem::IsotropicDamageMaterial, oofem::IsotropicLinearElasticMaterial, oofem::MisesMat, oofem::MisesMatGrad, oofem::MisesMatNl, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::MPSDamMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RankineMat, oofem::RCM2Material, oofem::RheoChainMaterial, oofem::SteelRelaxMat, and oofem::TrabBoneMaterial.

Definition at line 1050 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix(), and oofem::inv().

Referenced by oofem::SimpleCrossSection::give2dBeamStiffMtrx(), oofem::SimpleCrossSection::give3dBeamStiffMtrx(), oofem::LinearElasticMaterial::giveRealStressVector_1d(), giveStiffnessMatrix(), and oofem::SimpleCrossSection::giveStiffnessMatrix_1d().

give1dStressStiffMtrx_dCde()

void oofem::StructuralMaterial::give1dStressStiffMtrx_dCde ( FloatMatrix & answer, MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep )

virtual

Definition at line 763 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveStiffnessMatrix_dCde().

give1dStressStiffnessMatrix_dPdF()

FloatMatrixF< 1, 1 > oofem::StructuralMaterial::give1dStressStiffnessMatrix_dPdF ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Reimplemented in oofem::HyperelasticMaterial1d.

Definition at line 725 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix(), and oofem::inv().

Referenced by giveStiffnessMatrix_dPdF(), and oofem::SimpleCrossSection::giveStiffnessMatrix_dPdF_1d().

give2dBeamLayerStiffMtrx()

FloatMatrixF< 2, 2 > oofem::StructuralMaterial::give2dBeamLayerStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing 2d beam layer stiffness matrix of receiver. Default implementation computes 3d stiffness matrix using give3dMaterialStiffnessMatrix and reduces it to 2d beam layer stiffness using reduce method described above. However, this reduction is quite time consuming and if it is possible, it is recommended to overload this method and provide direct method for computing particular stiffness matrix.

Parameters

answer	Stiffness matrix.
mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, and oofem::RCM2Material.

Definition at line 1063 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix(), and oofem::inv().

Referenced by oofem::LayeredCrossSection::give2dBeamStiffMtrx(), oofem::LinearElasticMaterial::giveRealStressVector_2dBeamLayer(), and giveStiffnessMatrix().

give2dPlateSubSoilStiffMtrx()

FloatMatrixF< 3, 3 > oofem::StructuralMaterial::give2dPlateSubSoilStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing stiffness matrix of plate subsoil model. Default method is emty; the implementation should be provided by the particular model.

Parameters

mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Returns

Stiffness matrix.

Reimplemented in oofem::WinklerMaterial, and oofem::WinklerPasternakMaterial.

Definition at line 1095 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::give2dPlateSubSoilStiffMtrx().

give2DStrainVectorTranformationMtrx()

FloatMatrixF< 3, 3 > oofem::StructuralMaterial::give2DStrainVectorTranformationMtrx ( const FloatMatrixF< 2, 2 > & base, bool transpose = false )

static

Computes 2d strain vector transformation matrix from standard vector transformation matrix.

Parameters

base	A (2,2) matrix, where on each column are stored unit direction vectors of local coordinate axes to which we do transformation.
transpose	Determines if we transpose matrix before transforming.

Returns

Transformation matrix for strain vector.

Definition at line 1769 of file structuralmaterial.C.

References oofem::FloatMatrixF< N, M >::at(), and oofem::transpose().

Referenced by oofem::FCMMaterial::initializeCrack().

give3dBeamSubSoilStiffMtrx()

FloatMatrixF< 6, 6 > oofem::StructuralMaterial::give3dBeamSubSoilStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing stiffness matrix of beam3d subsoil model. Default method is emty; the implementation should be provided by the particular model.

Parameters

mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Returns

Stiffness matrix.

Reimplemented in oofem::WinklerMaterial.

Definition at line 1101 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::Beam3d::computeSubSoilStiffnessMatrix(), and oofem::StructuralCrossSection::give3dBeamSubSoilStiffMtrx().

give3dMaterialStiffnessMatrix()

virtual FloatMatrixF< 6, 6 > oofem::StructuralMaterial::give3dMaterialStiffnessMatrix ( MatResponseMode mode, GaussPoint * gp, TimeStep * tStep ) const

inlinevirtual

Computes full 3d material stiffness matrix at given integration point, time, respecting load history in integration point.

Parameters

answer	Computed results.
mode	Material response mode.
gp	Integration point.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::AbaqusUserMaterial, oofem::AnisotropicDamageMaterial, oofem::BlatzKoMaterial, oofem::CompoDamageMat, oofem::ConcreteDPM2, oofem::ConcreteDPM, oofem::DruckerPragerPlasticitySM, oofem::DustMaterial, oofem::FCMMaterial, oofem::HyperelasticMaterial1d, oofem::IsotropicDamageMaterial, oofem::LinearElasticMaterial, oofem::M1Material, oofem::MDM, oofem::MFrontUserMaterial, oofem::MicroplaneMaterial, oofem::MisesMat, oofem::MisesMatGrad, oofem::MooneyRivlinCompressibleMaterial, oofem::MooneyRivlinCompressibleMaterial, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::MPSDamMaterial, oofem::OgdenCompressibleMaterial, oofem::OrthotropicLinearElasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RCM2Material, oofem::RheoChainMaterial, oofem::SimoPisterMaterial, oofem::SimpleVitrificationMaterial, oofem::StructuralFE2Material, oofem::StructuralMaterialSettable, oofem::TrabBone3D, oofem::TrabBoneEmbed, oofem::TrabBoneGrad3D, oofem::TrabBoneNL3D, and oofem::TutorialMaterial.

Definition at line 384 of file structuralmaterial.h.

References OOFEM_ERROR.

Referenced by oofem::XfemStructuralElementInterface::computeCohesiveTangent(), give1dStressStiffMtrx(), give1dStressStiffnessMatrix_dPdF(), give2dBeamLayerStiffMtrx(), oofem::LayeredCrossSection::give3dDegeneratedShellStiffMtrx(), oofem::SimpleCrossSection::give3dDegeneratedShellStiffMtrx(), give3dMaterialStiffnessMatrix_dPdF(), giveFiberStiffMtrx(), givePlaneStrainStiffMtrx(), givePlaneStressStiffMtrx(), givePlateLayerStiffMtrx(), giveRealStressVector_ShellStressControl(), giveRealStressVector_StressControl(), giveStiffnessMatrix(), oofem::SimpleCrossSection::giveStiffnessMatrix_3d(), and oofem::StructuralMaterialEvaluator::solveYourself().

give3dMaterialStiffnessMatrix_dCde()

void oofem::StructuralMaterial::give3dMaterialStiffnessMatrix_dCde ( FloatMatrix & answer, MatResponseMode mode, GaussPoint * gp, TimeStep * tStep )

virtual

Todo

what should be default implementaiton?

Definition at line 735 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveStiffnessMatrix_dCde().

give3dMaterialStiffnessMatrix_dPdF()

FloatMatrixF< 9, 9 > oofem::StructuralMaterial::give3dMaterialStiffnessMatrix_dPdF ( MatResponseMode mode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Reimplemented in oofem::AbaqusUserMaterial, oofem::BlatzKoMaterial, oofem::HyperelasticMaterial1d, oofem::LargeStrainMasterMaterial, oofem::MFrontUserMaterial, oofem::MooneyRivlinCompressibleMaterial, oofem::MooneyRivlinCompressibleMaterial, oofem::OgdenCompressibleMaterial, oofem::SimoPisterMaterial, and oofem::StructuralPythonMaterial.

Definition at line 694 of file structuralmaterial.C.

References convert_dSdE_2_dPdF_3D(), give3dMaterialStiffnessMatrix(), oofem::Material::giveStatus(), and oofem::StructuralMaterialStatus::giveTempFVector().

Referenced by oofem::Shell7Base::computeLinearizedStiffness(), giveFirstPKStressVector_StressControl(), givePlaneStrainStiffnessMatrix_dPdF(), givePlaneStressStiffnessMatrix_dPdF(), giveStiffnessMatrix_dPdF(), and oofem::SimpleCrossSection::giveStiffnessMatrix_dPdF_3d().

giveCauchyStressVector_1d()

virtual void oofem::StructuralMaterial::giveCauchyStressVector_1d ( FloatArray & answer, GaussPoint * gp, const FloatArray & reducedF, TimeStep * tStep )

inlinevirtual

Definition at line 268 of file structuralmaterial.h.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveCauchyStresses().

giveCauchyStressVector_3d()

virtual void oofem::StructuralMaterial::giveCauchyStressVector_3d ( FloatArray & answer, GaussPoint * gp, const FloatArray & reducedF, TimeStep * tStep )

inlinevirtual

Definition at line 262 of file structuralmaterial.h.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveCauchyStresses().

giveCauchyStressVector_PlaneStrain()

virtual void oofem::StructuralMaterial::giveCauchyStressVector_PlaneStrain ( FloatArray & answer, GaussPoint * gp, const FloatArray & reducedF, TimeStep * tStep )

inlinevirtual

Definition at line 264 of file structuralmaterial.h.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveCauchyStresses().

giveCauchyStressVector_PlaneStress()

virtual void oofem::StructuralMaterial::giveCauchyStressVector_PlaneStress ( FloatArray & answer, GaussPoint * gp, const FloatArray & reducedF, TimeStep * tStep )

inlinevirtual

Definition at line 266 of file structuralmaterial.h.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveCauchyStresses().

giveCharacteristicMatrix()

void oofem::StructuralMaterial::giveCharacteristicMatrix ( FloatMatrix & answer, MatResponseMode type, GaussPoint * gp, TimeStep * tStep ) const

overridevirtual

Returns characteristic matrix of the receiver.

Reimplemented from oofem::Material.

Definition at line 80 of file structuralmaterial.C.

References giveStiffnessMatrix(), and OOFEM_ERROR.

giveCharacteristicVector()

void oofem::StructuralMaterial::giveCharacteristicVector ( FloatArray & answer, FloatArray & flux, MatResponseMode type, GaussPoint * gp, TimeStep * tStep ) const

overridevirtual

Returns characteristic vector of the receiver.

Reimplemented from oofem::Material.

Definition at line 90 of file structuralmaterial.C.

References giveRealStressVector(), and OOFEM_ERROR.

giveClassName()

const char * oofem::StructuralMaterial::giveClassName ( ) const

inlineoverridevirtual

Returns

Class name of the receiver.

Implements oofem::FEMComponent.

Reimplemented in oofem::StructuralMaterialSettable, oofem::StructuralPythonMaterial, oofem::StructuralSlipFE2Material, oofem::TrabBone3D, oofem::TrabBoneEmbed, oofem::TrabBoneGrad3D, oofem::TrabBoneMaterial, oofem::TrabBoneNL3D, oofem::TrabBoneNL, oofem::TrabBoneNLEmbed, oofem::TutorialMaterial, oofem::WinklerMaterial, and oofem::WinklerPasternakMaterial.

Definition at line 152 of file structuralmaterial.h.

giveEshelbyStressVector_PlaneStrain()

void oofem::StructuralMaterial::giveEshelbyStressVector_PlaneStrain ( FloatArray & answer, GaussPoint * gp, const FloatArray & reducedF, TimeStep * tStep )

virtual

Prototype for computation of Eshelby stress. No default implementation is provided.

Reimplemented in oofem::LinearElasticMaterial.

Definition at line 616 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveEshelbyStresses().

giveFiberStiffMtrx()

FloatMatrixF< 3, 3 > oofem::StructuralMaterial::giveFiberStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing 1d fiber stiffness matrix of receiver. Default implementation computes 3d stiffness matrix using give3dMaterialStiffnessMatrix and reduces it to 1d fiber stiffness using reduce method described above. However, this reduction is quite time consuming and if it is possible, it is recommended to overload this method and provide direct method for computing particular stiffness matrix.

Parameters

answer	Stiffness matrix.
mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::MPlasticMaterial2, oofem::MPlasticMaterial, and oofem::PlasticMaterial.

Definition at line 1084 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix(), and oofem::inv().

Referenced by oofem::FiberedCrossSection::give3dBeamStiffMtrx(), oofem::LinearElasticMaterial::giveRealStressVector_Fiber(), and giveStiffnessMatrix().

giveFirstPKStressVector_1d()

FloatArrayF< 1 > oofem::StructuralMaterial::giveFirstPKStressVector_1d ( const FloatArrayF< 1 > & vF, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveFirstPKStressVector_StressControl.

Reimplemented in oofem::HyperelasticMaterial1d.

Definition at line 422 of file structuralmaterial.C.

References giveRealStressVector_StressControl(), and giveVoigtVectorMask().

Referenced by oofem::SimpleCrossSection::giveFirstPKStress_1d().

giveFirstPKStressVector_3d()

FloatArrayF< 9 > oofem::StructuralMaterial::giveFirstPKStressVector_3d ( const FloatArrayF< 9 > & vF, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector for second Piola-Kirchoff stress.

Reimplemented in oofem::AbaqusUserMaterial, oofem::BlatzKoMaterial, oofem::HyperelasticMaterial1d, oofem::LargeStrainMasterMaterial, oofem::MooneyRivlinCompressibleMaterial, oofem::MooneyRivlinCompressibleMaterial, oofem::OgdenCompressibleMaterial, oofem::SimoPisterMaterial, and oofem::StructuralPythonMaterial.

Definition at line 330 of file structuralmaterial.C.

References oofem::dot(), E, oofem::eye(), oofem::from_voigt_form_9(), oofem::from_voigt_stress_6(), giveRealStressVector_3d(), oofem::Material::giveStatus(), S, oofem::Tdot(), oofem::to_voigt_form_33(), and oofem::to_voigt_strain_33().

Referenced by oofem::MFrontUserMaterial::give3dMaterialStiffnessMatrix_dPdF(), oofem::SimpleCrossSection::giveFirstPKStress_3d(), giveFirstPKStressVector_PlaneStrain(), and giveFirstPKStressVector_StressControl().

giveFirstPKStressVector_PlaneStrain()

FloatArrayF< 5 > oofem::StructuralMaterial::giveFirstPKStressVector_PlaneStrain ( const FloatArrayF< 5 > & vF, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveFirstPKStressVector_3d.

Definition at line 355 of file structuralmaterial.C.

References oofem::assemble(), and giveFirstPKStressVector_3d().

Referenced by oofem::SimpleCrossSection::giveFirstPKStress_PlaneStrain().

giveFirstPKStressVector_PlaneStress()

FloatArrayF< 4 > oofem::StructuralMaterial::giveFirstPKStressVector_PlaneStress ( const FloatArrayF< 4 > & vF, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveFirstPKStressVector_StressControl.

Definition at line 413 of file structuralmaterial.C.

References giveRealStressVector_StressControl(), and giveVoigtVectorMask().

Referenced by oofem::SimpleCrossSection::giveFirstPKStress_PlaneStress().

giveFirstPKStressVector_StressControl()

FloatArray oofem::StructuralMaterial::giveFirstPKStressVector_StressControl ( const FloatArray & reducedvF, const IntArray & FControl, GaussPoint * gp, TimeStep * tStep ) const

virtual

Iteratively calls giveRealStressVector_3d to find the stress controlled equal to zero·

Definition at line 366 of file structuralmaterial.C.

References oofem::FloatArray::assemble(), oofem::FloatArray::at(), oofem::IntArray::at(), oofem::FloatArray::beSubArrayOf(), oofem::FloatMatrix::beSubMatrixOf(), oofem::FloatArray::computeNorm(), oofem::IntArray::contains(), give3dMaterialStiffnessMatrix_dPdF(), giveFirstPKStressVector_3d(), oofem::IntArray::giveSize(), oofem::Material::giveStatus(), oofem::FloatArray::negated(), OOFEM_ERROR, oofem::IntArray::resize(), SCMaxiter, and oofem::FloatMatrix::solveForRhs().

giveFullSymMatrixForm()

void oofem::StructuralMaterial::giveFullSymMatrixForm ( FloatMatrix & answer, const FloatMatrix & red, MaterialMode matMode )

static

Converts the full unsymmetric Voigt matrix (4th order tensor) to reduced form.

Definition at line 2414 of file structuralmaterial.C.

References oofem::FloatMatrix::assemble(), giveVoigtSymVectorMask(), oofem::FloatMatrix::resize(), and oofem::FloatMatrix::zero().

Referenced by oofem::PerfectlyPlasticMaterial::giveEffectiveMaterialStiffnessMatrix(), and oofem::RCM2Material::giveNormalElasticStiffnessMatrix().

giveFullSymVectorForm()

void oofem::StructuralMaterial::giveFullSymVectorForm ( FloatArray & answer, const FloatArray & vec, MaterialMode matMode )

static

Converts the reduced unsymmetric Voigt vector (2nd order tensor) to full form.

Definition at line 2342 of file structuralmaterial.C.

References oofem::FloatArray::assemble(), oofem::FloatArray::giveSize(), giveVoigtSymVectorMask(), oofem::FloatArray::resize(), and oofem::FloatArray::zero().

Referenced by oofem::ConcreteFCMViscoElastic::giveIPValue(), oofem::MPSMaterial::giveIPValue(), giveIPValue(), and oofem::MisesMat::performPlasticityReturn_PlaneStress().

giveFullVectorForm()

void oofem::StructuralMaterial::giveFullVectorForm ( FloatArray & answer, const FloatArray & strainVector, MaterialMode matMode )

static

Converts the reduced symmetric Voigt vector (2nd order tensor) to full form.

Definition at line 2357 of file structuralmaterial.C.

References oofem::FloatArray::assemble(), oofem::FloatArray::giveSize(), giveVoigtVectorMask(), oofem::FloatArray::resize(), and oofem::FloatArray::zero().

giveFullVectorFormF()

void oofem::StructuralMaterial::giveFullVectorFormF ( FloatArray & answer, const FloatArray & strainVector, MaterialMode matMode )

static

Converts the reduced deformation gradient Voigt vector (2nd order tensor).

Definition at line 2372 of file structuralmaterial.C.

References oofem::FloatArray::at(), oofem::IntArray::at(), oofem::FloatArray::giveSize(), oofem::IntArray::giveSize(), giveVoigtVectorMask(), and oofem::FloatArray::resize().

giveInputRecord()

void oofem::StructuralMaterial::giveInputRecord ( DynamicInputRecord & input )

overridevirtual

Setups the input record string of receiver.

Parameters

input

Dynamic input record to be filled by receiver.

Reimplemented from oofem::Material.

Reimplemented in oofem::StructuralPythonMaterial, oofem::StructuralSlipFE2Material, oofem::TrabBoneNL3D, oofem::TrabBoneNL, oofem::TrabBoneNLEmbed, oofem::TutorialMaterial, oofem::WinklerMaterial, and oofem::WinklerPasternakMaterial.

Definition at line 2482 of file structuralmaterial.C.

References _IFT_StructuralMaterial_referencetemperature, _IFT_StructuralMaterial_StressControl_abstol, _IFT_StructuralMaterial_StressControl_reltol, _IFT_StructuralMaterial_StressControl_stiffmode, oofem::Material::giveInputRecord(), referenceTemperature, SCAbsTol, SCRelTol, SCStiffMode, and oofem::DynamicInputRecord::setField().

Referenced by oofem::AbaqusUserMaterial::giveInputRecord().

giveInvertedVoigtVectorMask()

void oofem::StructuralMaterial::giveInvertedVoigtVectorMask ( IntArray & answer, MaterialMode mmode )

static

Gives the inverted version of giveVoigtVectorMask.

Deprecated

This will eventually be removed. The normal mapping given in giveVoigtVectorMask can be used instead.

Definition at line 807 of file structuralmaterial.C.

References oofem::IntArray::at(), oofem::IntArray::giveSize(), giveVoigtSymVectorMask(), oofem::IntArray::resize(), and oofem::IntArray::zero().

giveIPValue()

int oofem::StructuralMaterial::giveIPValue ( FloatArray & answer, GaussPoint * gp, InternalStateType type, TimeStep * tStep )

overridevirtual

Returns the integration point corresponding value in Reduced form.

Parameters

answer	Contain corresponding ip value, zero sized if not available.
gp	Integration point to which the value refers.
type	Determines the type of internal variable.
tStep	Determines the time step.

Returns

Nonzero if the assignment can be done, zero if this type of variable is not supported.

Todo

What about the stress meassure in large deformations here? The internal state type should specify "Cauchy" or something.

Todo

Fill in correct full form values here! This just adds zeros!

Todo

Fill in correct full form values here! This just adds zeros!

Todo

Fill in correct full form values here! This just adds zeros!

Todo

Fill in correct full form values here! This just adds zeros!

Todo

Fill in correct full form values here! This just adds zeros!

Todo

Fill in correct full form values here! This just adds zeros!

Todo

Fill in correct full form values here! This just adds zeros!

Todo

Fill in correct full form values here! This just adds zeros!

Reimplemented from oofem::Material.

Reimplemented in oofem::StructuralPythonMaterial, oofem::TrabBone3D, oofem::TrabBoneEmbed, and oofem::TutorialMaterial.

Definition at line 1996 of file structuralmaterial.C.

References oofem::FloatArray::at(), oofem::FloatMatrix::at(), oofem::FloatArray::beColumnOf(), oofem::Element::computeGlobalCoordinates(), computePrincipalValDir(), computePrincipalValues(), oofem::StructuralElement::computeResultingIPEigenstrainAt(), computeVonMisesStress(), computeVonMisesStress_3D(), oofem::FEMComponent::domain, gc, oofem::GaussPoint::giveElement(), oofem::FieldManager::giveField(), giveFullSymVectorForm(), oofem::StructuralMaterialStatus::giveFVector(), oofem::Material::giveIPValue(), oofem::GaussPoint::giveMaterialMode(), oofem::GaussPoint::giveNaturalCoordinates(), oofem::FEMComponent::giveNumber(), oofem::FloatMatrix::giveNumberOfColumns(), oofem::StructuralMaterialStatus::givePVector(), oofem::FloatArray::giveSize(), oofem::Material::giveStatus(), oofem::StructuralMaterialStatus::giveStrainVector(), oofem::StructuralMaterialStatus::giveStressVector(), oofem::StructuralMaterialStatus::giveTempStrainVector(), oofem::StructuralMaterialStatus::giveTempStressVector(), OOFEM_ERROR, oofem::principal_strain, oofem::principal_stress, oofem::FloatArray::resize(), transformStrainVectorTo(), transformStressVectorTo(), and oofem::FloatArray::zero().

Referenced by oofem::Lattice2dBoundary::drawSpecial(), oofem::AbaqusUserMaterial::giveIPValue(), oofem::ConcreteDPM2::giveIPValue(), oofem::ConcreteDPM::giveIPValue(), oofem::LargeStrainMasterMaterial::giveIPValue(), oofem::MisesMat::giveIPValue(), oofem::SteelRelaxMat::giveIPValue(), and oofem::StructuralPythonMaterial::giveIPValue().

givePlaneStrainStiffMtrx()

FloatMatrixF< 4, 4 > oofem::StructuralMaterial::givePlaneStrainStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing plane strain stiffness matrix of receiver. Default implementation computes 3d stiffness matrix using give3dMaterialStiffnessMatrix and reduces it to plane strain stiffness using reduce method described above. However, this reduction is quite time consuming and if it is possible, it is recommended to overload this method and provide direct method for computing particular stiffness matrix. Note: as already described, if zero strain component is imposed (Plane strain, ..) this condition must be taken into account in geometrical relations, and corresponding component has to be included in reduced vector. (So plane strain conditions are \( \epsilon_z = \gamma_{xz} = \gamma_{yz} = 0 \), but relations for \( \epsilon_z\) and \(\sigma_z\) are included).

Parameters

answer	Stiffness matrix.
mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::FCMMaterial, oofem::IsotropicDamageMaterial, oofem::IsotropicLinearElasticMaterial, oofem::MDM, oofem::MisesMatGrad, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::MPSDamMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RCM2Material, oofem::RheoChainMaterial, and oofem::StructuralFE2Material.

Definition at line 1041 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix().

Referenced by giveStiffnessMatrix(), and oofem::SimpleCrossSection::giveStiffnessMatrix_PlaneStrain().

givePlaneStrainStiffMtrx_dCde()

void oofem::StructuralMaterial::givePlaneStrainStiffMtrx_dCde ( FloatMatrix & answer, MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep )

virtual

Definition at line 754 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveStiffnessMatrix_dCde().

givePlaneStrainStiffnessMatrix_dPdF()

FloatMatrixF< 5, 5 > oofem::StructuralMaterial::givePlaneStrainStiffnessMatrix_dPdF ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Reimplemented in oofem::AbaqusUserMaterial.

Definition at line 706 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix_dPdF().

Referenced by giveStiffnessMatrix_dPdF(), and oofem::SimpleCrossSection::giveStiffnessMatrix_dPdF_PlaneStrain().

givePlaneStressStiffMtrx()

FloatMatrixF< 3, 3 > oofem::StructuralMaterial::givePlaneStressStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing plane stress stiffness matrix of receiver. Default implementation computes 3d stiffness matrix using give3dMaterialStiffnessMatrix and reduces it to plane stress stiffness using reduce method described above. However, this reduction is quite time consuming and if it is possible, it is recommended to overload this method and provide direct method for computing particular stiffness matrix.

Parameters

answer	Stiffness matrix.
mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::AnisotropicDamageMaterial, oofem::FCMMaterial, oofem::IsotropicDamageMaterial, oofem::IsotropicLinearElasticMaterial, oofem::MDM, oofem::MisesMat, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::MPSDamMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RankineMat, oofem::RankineMatGrad, oofem::RankineMatNl, oofem::RCM2Material, oofem::RheoChainMaterial, oofem::StructuralFE2Material, and oofem::StructuralSlipFE2Material.

Definition at line 1031 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix(), and oofem::inv().

Referenced by oofem::SimpleCrossSection::give2dPlateStiffMtrx(), oofem::SimpleCrossSection::giveMembraneRotStiffMtrx(), oofem::LinearElasticMaterial::giveRealStressVector_PlaneStress(), giveStiffnessMatrix(), and oofem::SimpleCrossSection::giveStiffnessMatrix_PlaneStress().

givePlaneStressStiffMtrx_dCde()

void oofem::StructuralMaterial::givePlaneStressStiffMtrx_dCde ( FloatMatrix & answer, MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep )

virtual

Definition at line 745 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveStiffnessMatrix_dCde().

givePlaneStressStiffnessMatrix_dPdF()

FloatMatrixF< 4, 4 > oofem::StructuralMaterial::givePlaneStressStiffnessMatrix_dPdF ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Definition at line 715 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix_dPdF(), and oofem::inv().

Referenced by giveStiffnessMatrix_dPdF(), and oofem::SimpleCrossSection::giveStiffnessMatrix_dPdF_PlaneStress().

givePlaneStressVectorTranformationMtrx()

FloatMatrixF< 3, 3 > oofem::StructuralMaterial::givePlaneStressVectorTranformationMtrx ( const FloatMatrixF< 2, 2 > & base, bool transpose = false )

static

Computes 2d stress vector transformation matrix from standard vector transformation matrix.

Parameters

base	A (2,2) matrix, where on each column are stored unit direction vectors of local coordinate axes to which we do transformation.
transpose	Determines if we transpose matrix before transforming.

Returns

Transformation matrix for stress vector.

Definition at line 1859 of file structuralmaterial.C.

References oofem::FloatMatrixF< N, M >::at(), and oofem::transpose().

Referenced by oofem::RankineMat::computeEta(), oofem::RankineMat::evaluatePlaneStressStiffMtrx(), oofem::RankineMatGrad::giveGradientDamageStiffnessMatrix_du(), oofem::RankineMatGrad::giveGradientDamageStiffnessMatrix_du_BB(), oofem::RankineMatGrad::giveGradientDamageStiffnessMatrix_du_NB(), oofem::MPSDamMaterial::giveRealStressVector(), and oofem::FCMMaterial::initializeCrack().

givePlateLayerStiffMtrx()

FloatMatrixF< 5, 5 > oofem::StructuralMaterial::givePlateLayerStiffMtrx ( MatResponseMode mmode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Method for computing 2d plate layer stiffness matrix of receiver. Default implementation computes 3d stiffness matrix using give3dMaterialStiffnessMatrix and reduces it to 2d plate layer stiffness using reduce method described above. However, this reduction is quite time consuming and if it is possible, it is recommended to overload this method and provide direct method for computing particular stiffness matrix.

Parameters

answer	Stiffness matrix.
mmode	Material response mode.
gp	Integration point, which load history is used.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::Concrete2, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, and oofem::RCM2Material.

Definition at line 1074 of file structuralmaterial.C.

References give3dMaterialStiffnessMatrix(), and oofem::inv().

Referenced by oofem::LayeredCrossSection::give2dPlateStiffMtrx(), oofem::LayeredCrossSection::give3dShellStiffMtrx(), oofem::LinearElasticMaterial::giveRealStressVector_PlateLayer(), and giveStiffnessMatrix().

giveRealStressVector()

void oofem::StructuralMaterial::giveRealStressVector ( FloatArray & answer, GaussPoint * gp, const FloatArray & reducedStrain, TimeStep * tStep ) const

virtual

Computes the real stress vector for given total strain and integration point. The total strain is defined as strain computed directly from displacement field at given time. The stress independent parts (temperature, eigenstrains) are subtracted in constitutive driver. The service should use previously reached equilibrium history variables. Also it should update temporary history variables in status according to newly reached state. The temporary history variables are moved into equilibrium ones after global structure equilibrium has been reached by iteration process.

Parameters

answer	Stress vector in reduced form. For large deformations it is treated as the second Piola-Kirchoff stress.
gp	Integration point.
reducedStrain	Strain vector in reduced form. For large deformations it is treated as the Green-Lagrange strain.
tStep	Current time step (most models are able to respond only when tStep is current time step).

Todo

Move this to StructuralCrossSection ?

Reimplemented in oofem::AnisotropicDamageMaterial, oofem::B3SolidMaterial, oofem::CompoDamageMat, oofem::ConcreteFCMViscoElastic, oofem::Eurocode2CreepMaterial, oofem::FCMMaterial, oofem::FRCFCMNL, oofem::IsotropicDamageMaterial, oofem::KelvinChainMaterial, oofem::KelvinChainSolidMaterial, oofem::MaxwellChainMaterial, oofem::MDM, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::MPSDamMaterial, oofem::MPSMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RCM2Material, oofem::RCSDEMaterial, oofem::RCSDMaterial, oofem::RCSDNLMaterial, oofem::RheoChainMaterial, and oofem::SteelRelaxMat.

Definition at line 99 of file structuralmaterial.C.

References oofem::GaussPoint::giveMaterialMode(), giveRealStressVector_1d(), giveRealStressVector_2dBeamLayer(), giveRealStressVector_2dPlateSubSoil(), giveRealStressVector_3d(), giveRealStressVector_3dBeamSubSoil(), giveRealStressVector_Fiber(), giveRealStressVector_PlaneStrain(), giveRealStressVector_PlaneStress(), and giveRealStressVector_PlateLayer().

Referenced by oofem::IsotropicLinearElasticMaterial::giveCharacteristicVector(), and giveCharacteristicVector().

giveRealStressVector_1d()

FloatArrayF< 1 > oofem::StructuralMaterial::giveRealStressVector_1d ( const FloatArrayF< 1 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector_StressControl.

Reimplemented in oofem::AnisotropicDamageMaterial, oofem::CompoDamageMat, oofem::FCMMaterial, oofem::IsotropicAsymmetric1DMaterial, oofem::IsotropicDamageMaterial, oofem::LinearElasticMaterial, oofem::MisesMat, oofem::MisesMatNl, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RankineMat, oofem::RankineMatNl, oofem::RCM2Material, oofem::RheoChainMaterial, oofem::SteelRelaxMat, oofem::TrabBoneMaterial, and oofem::TrabBoneNL.

Definition at line 281 of file structuralmaterial.C.

References giveRealStressVector_StressControl(), and giveVoigtSymVectorMask().

Referenced by oofem::SimpleCrossSection::giveRealStress_1d(), giveRealStressVector(), and oofem::MisesMat::giveRealStressVector_1d().

giveRealStressVector_2dBeamLayer()

FloatArrayF< 2 > oofem::StructuralMaterial::giveRealStressVector_2dBeamLayer ( const FloatArrayF< 2 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector_StressControl.

Reimplemented in oofem::FCMMaterial, oofem::LinearElasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RCM2Material, and oofem::RheoChainMaterial.

Definition at line 290 of file structuralmaterial.C.

References giveRealStressVector_StressControl(), and giveVoigtSymVectorMask().

Referenced by giveRealStressVector().

giveRealStressVector_2dPlateSubSoil()

FloatArrayF< 3 > oofem::StructuralMaterial::giveRealStressVector_2dPlateSubSoil ( const FloatArrayF< 3 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation is not provided.

Reimplemented in oofem::WinklerMaterial, and oofem::WinklerPasternakMaterial.

Definition at line 317 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveGeneralizedStress_PlateSubSoil(), and giveRealStressVector().

giveRealStressVector_3d()

FloatArrayF< 6 > oofem::StructuralMaterial::giveRealStressVector_3d ( const FloatArrayF< 6 > & strain, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector for second Piola-Kirchoff stress.

Reimplemented in oofem::AbaqusUserMaterial, oofem::AnisotropicDamageMaterial, oofem::BlatzKoMaterial, oofem::CompoDamageMat, oofem::ConcreteDPM2, oofem::ConcreteDPM, oofem::DruckerPragerPlasticitySM, oofem::DustMaterial, oofem::FCMMaterial, oofem::HyperelasticMaterial1d, oofem::IsotropicDamageMaterial, oofem::LargeStrainMasterMaterial, oofem::LinearElasticMaterial, oofem::M1Material, oofem::MDM, oofem::MFrontUserMaterial, oofem::MicroMaterial, oofem::MicroplaneMaterial_Bazant, oofem::MisesMat, oofem::MisesMatNl, oofem::MooneyRivlinCompressibleMaterial, oofem::MooneyRivlinCompressibleMaterial, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::OgdenCompressibleMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RCM2Material, oofem::RheoChainMaterial, oofem::SimoPisterMaterial, oofem::SimpleVitrificationMaterial, oofem::StructuralFE2Material, oofem::StructuralMaterialSettable, oofem::TrabBone3D, oofem::TrabBoneEmbed, oofem::TrabBoneNL3D, oofem::TrabBoneNLEmbed, and oofem::TutorialMaterial.

Definition at line 128 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::XfemStructuralElementInterface::computeCohesiveForces(), giveFirstPKStressVector_3d(), oofem::SimpleCrossSection::giveRealStress_3d(), giveRealStressVector(), giveRealStressVector_PlaneStrain(), giveRealStressVector_ShellStressControl(), giveRealStressVector_StressControl(), and oofem::StructuralMaterialEvaluator::solveYourself().

giveRealStressVector_3dBeamSubSoil()

FloatArrayF< 6 > oofem::StructuralMaterial::giveRealStressVector_3dBeamSubSoil ( const FloatArrayF< 6 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Reimplemented in oofem::WinklerMaterial.

Definition at line 323 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::StructuralCrossSection::giveGeneralizedStress_3dBeamSubSoil(), and giveRealStressVector().

giveRealStressVector_Fiber()

FloatArrayF< 3 > oofem::StructuralMaterial::giveRealStressVector_Fiber ( const FloatArrayF< 3 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector_StressControl.

Reimplemented in oofem::LinearElasticMaterial, and oofem::PlasticMaterial.

Definition at line 308 of file structuralmaterial.C.

References giveRealStressVector_StressControl(), and giveVoigtSymVectorMask().

Referenced by giveRealStressVector().

giveRealStressVector_PlaneStrain()

FloatArrayF< 4 > oofem::StructuralMaterial::giveRealStressVector_PlaneStrain ( const FloatArrayF< 4 > & strain, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector_3d.

Reimplemented in oofem::AnisotropicDamageMaterial, oofem::FCMMaterial, oofem::IsotropicDamageMaterial, oofem::MDM, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RCM2Material, and oofem::RheoChainMaterial.

Definition at line 142 of file structuralmaterial.C.

References oofem::assemble(), and giveRealStressVector_3d().

Referenced by oofem::StructuralFE2Material::givePlaneStrainStiffMtrx(), oofem::SimpleCrossSection::giveRealStress_PlaneStrain(), and giveRealStressVector().

giveRealStressVector_PlaneStress()

FloatArrayF< 3 > oofem::StructuralMaterial::giveRealStressVector_PlaneStress ( const FloatArrayF< 3 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector_StressControl.

Reimplemented in oofem::AnisotropicDamageMaterial, oofem::FCMMaterial, oofem::IsotropicDamageMaterial, oofem::LinearElasticMaterial, oofem::MDM, oofem::MisesMat, oofem::MPlasticMaterial2, oofem::MPlasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RankineMat, oofem::RankineMatNl, oofem::RCM2Material, oofem::RheoChainMaterial, oofem::StructuralFE2Material, and oofem::StructuralSlipFE2Material.

Definition at line 272 of file structuralmaterial.C.

References giveRealStressVector_StressControl(), and giveVoigtSymVectorMask().

Referenced by oofem::SimpleCrossSection::giveRealStress_PlaneStress(), and giveRealStressVector().

giveRealStressVector_PlateLayer()

FloatArrayF< 5 > oofem::StructuralMaterial::giveRealStressVector_PlateLayer ( const FloatArrayF< 5 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector_StressControl.

Reimplemented in oofem::Concrete2, oofem::FCMMaterial, oofem::LinearElasticMaterial, oofem::PerfectlyPlasticMaterial, oofem::PlasticMaterial, oofem::RCM2Material, and oofem::RheoChainMaterial.

Definition at line 299 of file structuralmaterial.C.

References giveRealStressVector_StressControl(), and giveVoigtSymVectorMask().

Referenced by giveRealStressVector().

giveRealStressVector_ShellStressControl()

FloatArray oofem::StructuralMaterial::giveRealStressVector_ShellStressControl ( const FloatArray & reducedE, const IntArray & strainControl, GaussPoint * gp, TimeStep * tStep ) const

virtual

Definition at line 217 of file structuralmaterial.C.

References oofem::FloatArray::assemble(), oofem::IntArray::at(), oofem::FloatArray::beSubArrayOf(), oofem::FloatMatrix::beSubMatrixOf(), oofem::FloatArray::computeNorm(), give3dMaterialStiffnessMatrix(), giveRealStressVector_3d(), oofem::Material::giveStatus(), oofem::FloatArray::negated(), OOFEM_WARNING, oofem::IntArray::resize(), SCMaxiter, SCStiffMode, and oofem::FloatMatrix::solveForRhs().

giveRealStressVector_StressControl()

FloatArray oofem::StructuralMaterial::giveRealStressVector_StressControl ( const FloatArray & reducedE, const IntArray & strainControl, GaussPoint * gp, TimeStep * tStep ) const

virtual

Iteratively calls giveRealStressVector_3d to find the stress controlled equal to zero·

Todo

We need a relative tolerance here! A relative tolerance like this could work, but if a really small increment is performed it won't work (it will be limited by machine precision)

Reimplemented in oofem::AnisotropicDamageMaterial, and oofem::IsotropicDamageMaterial.

Definition at line 150 of file structuralmaterial.C.

References oofem::FloatArray::assemble(), oofem::FloatArray::at(), oofem::IntArray::at(), oofem::FloatMatrix::beInverseOf(), oofem::FloatArray::beProductOf(), oofem::FloatArray::beSubArrayOf(), oofem::FloatMatrix::beSubMatrixOf(), oofem::FloatArray::computeNorm(), oofem::IntArray::contains(), give3dMaterialStiffnessMatrix(), giveRealStressVector_3d(), oofem::IntArray::giveSize(), oofem::Material::giveStatus(), oofem::FloatArray::negated(), OOFEM_ERROR, oofem::IntArray::resize(), SCMaxiter, and SCStiffMode.

Referenced by giveFirstPKStressVector_1d(), giveFirstPKStressVector_PlaneStress(), giveRealStressVector_1d(), giveRealStressVector_2dBeamLayer(), giveRealStressVector_Fiber(), giveRealStressVector_PlaneStress(), and giveRealStressVector_PlateLayer().

giveRealStressVector_Warping()

FloatArrayF< 2 > oofem::StructuralMaterial::giveRealStressVector_Warping ( const FloatArrayF< 2 > & reducedE, GaussPoint * gp, TimeStep * tStep ) const

virtual

Default implementation relies on giveRealStressVector_StressControl.

Reimplemented in oofem::LinearElasticMaterial.

Definition at line 135 of file structuralmaterial.C.

References OOFEM_ERROR.

Referenced by oofem::SimpleCrossSection::giveRealStress_Warping().

giveReducedMatrixForm()

void oofem::StructuralMaterial::giveReducedMatrixForm ( FloatMatrix & answer, const FloatMatrix & full, MaterialMode matMode )

static

Converts the full symmetric Voigt matrix (4th order tensor) to reduced form.

Definition at line 2425 of file structuralmaterial.C.

References oofem::FloatMatrix::beSubMatrixOf(), and giveVoigtVectorMask().

giveReducedSymMatrixForm()

void oofem::StructuralMaterial::giveReducedSymMatrixForm ( FloatMatrix & answer, const FloatMatrix & full, MaterialMode matMode )

static

Converts the full unsymmetric Voigt matrix (4th order tensor) to reduced form.

Definition at line 2434 of file structuralmaterial.C.

References oofem::FloatMatrix::beSubMatrixOf(), and giveVoigtSymVectorMask().

Referenced by oofem::StructuralFE2Material::give3dMaterialStiffnessMatrix().

giveReducedSymVectorForm()

void oofem::StructuralMaterial::giveReducedSymVectorForm ( FloatArray & answer, const FloatArray & vec, MaterialMode matMode )

static

Converts the full unsymmetric Voigt vector (2nd order tensor) to reduced form.

Definition at line 2400 of file structuralmaterial.C.

References oofem::FloatArray::beSubArrayOf(), oofem::FloatArray::giveSize(), oofem::IntArray::giveSize(), and giveVoigtSymVectorMask().

Referenced by oofem::MPSMaterial::computeAutogenousShrinkageDefinedByTF(), oofem::MPSMaterial::computeB4AutogenousShrinkageStrainVector(), oofem::MPSMaterial::computeFibAutogenousShrinkageStrainVector(), oofem::MPSMaterial::computePointShrinkageStrainVector(), computeStressIndependentStrainVector(), oofem::NLStructuralElement::giveInternalForcesVector(), oofem::MisesMat::givePlaneStressStiffMtrx(), oofem::MPSMaterial::giveShrinkageStrainVector(), oofem::IsotropicDamageMaterial1::MMI_map(), and oofem::MisesMat::performPlasticityReturn_PlaneStress().

giveReducedVectorForm()

void oofem::StructuralMaterial::giveReducedVectorForm ( FloatArray & answer, const FloatArray & vec, MaterialMode matMode )

static

Converts the full symmetric Voigt vector (2nd order tensor) to reduced form.

Definition at line 2391 of file structuralmaterial.C.

References oofem::FloatArray::beSubArrayOf(), and giveVoigtVectorMask().

Referenced by oofem::NLStructuralElement::giveInternalForcesVector().

giveReferenceTemperature()

double oofem::StructuralMaterial::giveReferenceTemperature ( )

inline

Returns the reference temperature of receiver.

Definition at line 292 of file structuralmaterial.h.

References referenceTemperature.

giveSizeOfVoigtSymVector()

int oofem::StructuralMaterial::giveSizeOfVoigtSymVector ( MaterialMode mmode )

static

Returns the size of symmetric part of a reduced stress/strain vector according to given mode.

Parameters

mmode

Material response mode.

Definition at line 789 of file structuralmaterial.C.

References oofem::IntArray::giveSize(), and giveVoigtSymVectorMask().

Referenced by computeStressIndependentStrainVector(), oofem::NLStructuralElement::giveInternalForcesVector(), oofem::MPSDamMaterial::giveRealStressVector(), oofem::MPSMaterial::giveShrinkageStrainVector(), and oofem::MPSMaterialStatus::MPSMaterialStatus().

giveSizeOfVoigtVector()

int oofem::StructuralMaterial::giveSizeOfVoigtVector ( MaterialMode mmode )

static

Returns the size of reduced stress/strain vector according to given mode.

Parameters

mmode

Material response mode.

Definition at line 798 of file structuralmaterial.C.

References oofem::IntArray::giveSize(), and giveVoigtVectorMask().

giveStiffnessMatrix()

void oofem::StructuralMaterial::giveStiffnessMatrix ( FloatMatrix & answer, MatResponseMode mode, GaussPoint * gp, TimeStep * tStep ) const

virtual

Computes the stiffness matrix for giveRealStressVector of receiver in given integration point, respecting its history. The algorithm should use temporary or equilibrium history variables stored in integration point status to compute and return required result.

Parameters

answer	Contains result.
mode	Material response mode.
gp	Integration point.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::IsotropicGradientDamageMaterial, oofem::LargeStrainMasterMaterialGrad, oofem::LatticeStructuralMaterial, oofem::Masonry02, oofem::MisesMatGrad, oofem::RankineMatGrad, and oofem::TrabBoneGrad3D.

Definition at line 623 of file structuralmaterial.C.

References oofem::eye(), give1dStressStiffMtrx(), give2dBeamLayerStiffMtrx(), give3dMaterialStiffnessMatrix(), giveFiberStiffMtrx(), givePlaneStrainStiffMtrx(), givePlaneStressStiffMtrx(), givePlateLayerStiffMtrx(), and OOFEM_ERROR.

Referenced by oofem::IsotropicDamageMaterial1::computeEta(), giveCharacteristicMatrix(), oofem::MPlasticMaterial2::giveConsistentStiffnessMatrix(), oofem::PerfectlyPlasticMaterial::giveEffectiveMaterialStiffnessMatrix(), oofem::RCM2Material::giveEffectiveMaterialStiffnessMatrix(), oofem::MPlasticMaterial2::giveElastoPlasticStiffnessMatrix(), oofem::IDNLMaterial::giveLocalNonlocalStiffnessContribution(), oofem::RCM2Material::giveNormalElasticStiffnessMatrix(), oofem::AnisotropicDamageMaterial::giveRealStressVector(), oofem::FCMMaterial::giveRealStressVector(), oofem::IsotropicDamageMaterial::giveRealStressVector(), oofem::RheoChainMaterial::giveRealStressVector(), oofem::IDNLMaterial::giveRemoteNonlocalStiffnessContribution(), and oofem::IsotropicDamageMaterial1::initDamaged().

giveStiffnessMatrix_dPdF()

void oofem::StructuralMaterial::giveStiffnessMatrix_dPdF ( FloatMatrix & answer, MatResponseMode mode, GaussPoint * gp, TimeStep * tStep )

virtual

Computes the large strain stiffness matrix for giveFirstPKStressVector of receiver in given integration point, respecting its history. The algorithm should use temporary or equilibrium history variables stored in integration point status to compute and return required result.

Parameters

answer	Contains result.
mode	Material response mode.
gp	Integration point.
tStep	Time step (most models are able to respond only when tStep is current time step).

Definition at line 665 of file structuralmaterial.C.

References give1dStressStiffnessMatrix_dPdF(), give3dMaterialStiffnessMatrix_dPdF(), oofem::GaussPoint::giveMaterialMode(), givePlaneStrainStiffnessMatrix_dPdF(), givePlaneStressStiffnessMatrix_dPdF(), and OOFEM_ERROR.

giveStrainVectorTranformationMtrx()

FloatMatrixF< 6, 6 > oofem::StructuralMaterial::giveStrainVectorTranformationMtrx ( const FloatMatrixF< 3, 3 > & base, bool transpose = false )

static

Computes 3d strain vector transformation matrix from standard vector transformation matrix.

Parameters

base	A (3,3) matrix, where on each column are stored unit direction vectors of local coordinate axes to which we do transformation.
transpose	Determines if we transpose matrix before transforming.

Returns

Transformation matrix for strain vector.

Definition at line 1708 of file structuralmaterial.C.

References oofem::FloatMatrixF< N, M >::at(), and oofem::transpose().

Referenced by oofem::CompoDamageMat::giveMatStiffRotationMatrix(), oofem::OrthotropicLinearElasticMaterial::giveRotationMatrix(), oofem::FCMMaterial::initializeCrack(), and transformStrainVectorTo().

giveStressDependentPartOfStrainVector()

void oofem::StructuralMaterial::giveStressDependentPartOfStrainVector	(	FloatArray &	answer,
		GaussPoint *	gp,
		const FloatArray &	reducedStrainVector,
		TimeStep *	tStep,
		ValueModeType	mode ) const

Method for subtracting from reduced space strain vector its stress-independent parts (caused by temperature, shrinkage, creep and possibly by other phenomena). Calls computeStressIndependentStrainVector to obtain stress independent part of strain.

Parameters

answer	Computed strain vector.
gp	Integration point.
reducedStrainVector	Reduced strain vector.
tStep	Time step.
mode	Determines value mode.

Definition at line 772 of file structuralmaterial.C.

References computeStressIndependentStrainVector(), and oofem::FloatArray::subtract().

Referenced by oofem::HOMExportModule::average(), oofem::AnisotropicDamageMaterial::give3dMaterialStiffnessMatrix(), oofem::IsotropicDamageMaterial::giveIPValue(), oofem::LinearElasticMaterial::giveIPValue(), oofem::AnisotropicDamageMaterial::givePlaneStressStiffMtrx(), oofem::AnisotropicDamageMaterial::giveRealStressVector(), oofem::CompoDamageMat::giveRealStressVector(), oofem::FCMMaterial::giveRealStressVector(), oofem::IsotropicDamageMaterial::giveRealStressVector(), oofem::MDM::giveRealStressVector(), oofem::MPlasticMaterial2::giveRealStressVector(), oofem::MPlasticMaterial::giveRealStressVector(), oofem::PerfectlyPlasticMaterial::giveRealStressVector(), oofem::PlasticMaterial::giveRealStressVector(), oofem::RCM2Material::giveRealStressVector(), oofem::RCSDEMaterial::giveRealStressVector(), oofem::RCSDMaterial::giveRealStressVector(), oofem::RCSDNLMaterial::giveRealStressVector(), oofem::RheoChainMaterial::giveRealStressVector(), oofem::SteelRelaxMat::giveRealStressVector(), oofem::LinearElasticMaterial::giveRealStressVector_1d(), oofem::MisesMat::giveRealStressVector_1d(), oofem::LinearElasticMaterial::giveRealStressVector_2dBeamLayer(), oofem::MisesMat::giveRealStressVector_3d(), oofem::LinearElasticMaterial::giveRealStressVector_Fiber(), oofem::AnisotropicDamageMaterial::giveRealStressVector_PlaneStress(), oofem::LinearElasticMaterial::giveRealStressVector_PlaneStress(), oofem::Concrete2::giveRealStressVector_PlateLayer(), oofem::LinearElasticMaterial::giveRealStressVector_PlateLayer(), oofem::IsotropicGradientDamageMaterial::giveRealStressVectorGradientDamage(), oofem::IsotropicLinearElasticMaterial::giveRealStressVectorUP_3d(), oofem::IsotropicLinearElasticMaterial::giveRealStressVectorUP_PlaneStrain(), oofem::SteelRelaxMat::giveStressDependentPartOfStrainVector(), oofem::IDNLMaterial::updateBeforeNonlocAverage(), oofem::MazarsNLMaterial::updateBeforeNonlocAverage(), oofem::TrabBoneNL3D::updateBeforeNonlocAverage(), oofem::TrabBoneNL::updateBeforeNonlocAverage(), and oofem::TrabBoneNLEmbed::updateBeforeNonlocAverage().

giveStressVectorTranformationMtrx()

FloatMatrixF< 6, 6 > oofem::StructuralMaterial::giveStressVectorTranformationMtrx ( const FloatMatrixF< 3, 3 > & base, bool transpose = false )

static

Computes 3d stress vector transformation matrix from standard vector transformation matrix.

Parameters

base	A (3,3) matrix, where on each column are stored unit direction vectors of local coordinate axes to which we do transformation.
transpose	Determines if we transpose matrix before transforming.

Returns

Transformation matrix for stress vector.

Definition at line 1798 of file structuralmaterial.C.

References oofem::FloatMatrixF< N, M >::at(), and oofem::transpose().

Referenced by oofem::RCM2Material::giveEffectiveMaterialStiffnessMatrix(), oofem::MPSDamMaterial::giveRealStressVector(), oofem::IDNLMaterial::giveRemoteNonlocalStiffnessContribution(), oofem::FCMMaterial::initializeCrack(), and transformStressVectorTo().

giveSymVI()

int oofem::StructuralMaterial::giveSymVI ( int ind1, int ind2 )

inlinestatic

Definition at line 141 of file structuralmaterial.h.

References svIndex.

Referenced by convert_dSdE_2_dPdF_3D().

giveThermalDilatationVector()

FloatArrayF< 6 > oofem::StructuralMaterial::giveThermalDilatationVector ( GaussPoint * gp, TimeStep * tStep ) const

virtual

Returns a vector of coefficients of thermal dilatation in direction of each material principal (local) axis.

Parameters

answer	Vector of thermal dilatation coefficients.
gp	Integration point.
tStep	Time step (most models are able to respond only when tStep is current time step).

Reimplemented in oofem::DruckerPragerPlasticitySM, oofem::DustMaterial, oofem::IsotropicDamageMaterial, oofem::LatticeLinearElastic, oofem::LatticeSlip, oofem::LinearElasticMaterial, oofem::M4Material, oofem::MDM, oofem::MPlasticMaterial2, oofem::OrthotropicLinearElasticMaterial, oofem::RCM2Material, oofem::RheoChainMaterial, oofem::SimpleVitrificationMaterial, and oofem::TutorialMaterial.

Definition at line 2442 of file structuralmaterial.C.

References oofem::Material::give(), and tAlpha.

Referenced by computeStressIndependentStrainVector(), and computeStressIndependentStrainVector_3d().

giveVI()

int oofem::StructuralMaterial::giveVI ( int ind1, int ind2 )

inlinestatic

Definition at line 142 of file structuralmaterial.h.

References vIindex.

Referenced by convert_dSdE_2_dPdF_3D().

giveVoigtSymVectorMask()

int oofem::StructuralMaterial::giveVoigtSymVectorMask ( IntArray & answer, MaterialMode mmode )

static

The same as giveVoigtVectorMask but returns a mask corresponding to a symmetric second order tensor.

Returns a mask of the vector indicies corresponding to components in a symmetric second order tensor of some stress/strain/deformation measure that performes work. Thus, components corresponding to imposed zero stress (e.g. plane stress etc.) are not included. On the other hand, if zero strain components are imposed( e.g. plane strain etc.) this condition must be taken into account in geometrical relations. Therefore, these corresponding components are included in the reduced vector. Which compnents to include are given by the particular MaterialMode. Ex: PlaneStress -> [1 2 6]

Parameters

answer	Returned mask.
mmode	Material response mode.

Returns

The number of components in the corresponding full vector.

Todo

This isn't actually fixed yet. Should be made compatible with 3dShell and 2dBeam

Todo

This isn't actually fixed yet. Should be made compatible with 3dShell and 2dBeam

Definition at line 819 of file structuralmaterial.C.

References oofem::IntArray::clear(), and oofem::IntArray::enumerate().

Referenced by giveFullSymMatrixForm(), giveFullSymVectorForm(), giveInvertedVoigtVectorMask(), giveRealStressVector_1d(), giveRealStressVector_2dBeamLayer(), giveRealStressVector_Fiber(), giveRealStressVector_PlaneStress(), giveRealStressVector_PlateLayer(), giveReducedSymMatrixForm(), giveReducedSymVectorForm(), and giveSizeOfVoigtSymVector().

giveVoigtVectorMask()

int oofem::StructuralMaterial::giveVoigtVectorMask ( IntArray & answer, MaterialMode mmode )

static

Returns a mask of the vector indicies corresponding to components in a general (non-symmetric) second order tensor of some stress/strain/deformation measure that performes work. Thus, components corresponding to imposed zero stress (e.g. plane stress etc.) are not included. On the other hand, if zero strain components are imposed( e.g. plane strain etc.) this condition must be taken into account in geometrical relations. Therefore, these corresponding components are included in the reduced vector. Which compnents to include are given by the particular MaterialMode. Ex: PlaneStress -> [1 2 6 9]

Parameters

answer	Returned mask.
mmode	Material response mode.

Returns

The number of components in the corresponding full vector.

Todo

add additional modes if they relevant.

Definition at line 981 of file structuralmaterial.C.

References oofem::IntArray::at(), and oofem::IntArray::resize().

Referenced by giveFirstPKStressVector_1d(), giveFirstPKStressVector_PlaneStress(), giveFullVectorForm(), giveFullVectorFormF(), giveReducedMatrixForm(), giveReducedVectorForm(), and giveSizeOfVoigtVector().

hasMaterialModeCapability()

bool oofem::StructuralMaterial::hasMaterialModeCapability ( MaterialMode mode ) const

overridevirtual

Tests if material supports material mode.

Parameters

mode	Required material mode.

Returns

Nonzero if supported, zero otherwise.

Reimplemented from oofem::Material.

Reimplemented in oofem::TrabBoneGrad3D, oofem::TrabBoneMaterial, oofem::WinklerMaterial, and oofem::WinklerPasternakMaterial.

Definition at line 70 of file structuralmaterial.C.

Referenced by oofem::PerfectlyPlasticMaterial::giveEffectiveMaterialStiffnessMatrix().

initializeFrom()

void oofem::StructuralMaterial::initializeFrom ( InputRecord & ir )

overridevirtual

Initializes receiver according to object description stored in input record. This function is called immediately after creating object using constructor. Input record can be imagined as data record in component database belonging to receiver. Receiver may use value-name extracting functions to extract particular field from record. Note that initializeFrom may be called mutiple times.

See also

IR_GIVE_FIELD

IR_GIVE_OPTIONAL_FIELD

Parameters

ir	Input record to initialize from.
priority	Priority of the input record. This is used to determine the order of initialization

Reimplemented from oofem::Material.

Reimplemented in oofem::StructuralMaterialSettable, oofem::StructuralPythonMaterial, oofem::StructuralSlipFE2Material, oofem::TrabBone3D, oofem::TrabBoneEmbed, oofem::TrabBoneGrad3D, oofem::TrabBoneMaterial, oofem::TrabBoneNL3D, oofem::TrabBoneNL, oofem::TrabBoneNLEmbed, oofem::TutorialMaterial, oofem::WinklerMaterial, and oofem::WinklerPasternakMaterial.

Definition at line 2456 of file structuralmaterial.C.

References _IFT_StructuralMaterial_referencetemperature, _IFT_StructuralMaterial_StressControl_abstol, _IFT_StructuralMaterial_StressControl_maxiter, _IFT_StructuralMaterial_StressControl_reltol, _IFT_StructuralMaterial_StressControl_stiffmode, _IFT_StructuralMaterial_talpha, oofem::Material::initializeFrom(), IR_GIVE_OPTIONAL_FIELD, oofem::Material::propertyDictionary, referenceTemperature, SCAbsTol, SCMaxiter, SCRelTol, SCStiffMode, and tAlpha.

Referenced by oofem::AbaqusUserMaterial::initializeFrom(), oofem::BlatzKoMaterial::initializeFrom(), oofem::ConcreteDPM2::initializeFrom(), oofem::ConcreteDPM::initializeFrom(), oofem::MisesMat::initializeFrom(), oofem::MooneyRivlinCompressibleMaterial::initializeFrom(), oofem::OgdenCompressibleMaterial::initializeFrom(), oofem::SimoPisterMaterial::initializeFrom(), and oofem::SteelRelaxMat::initializeFrom().

setIPValue()

int oofem::StructuralMaterial::setIPValue ( const FloatArray & value, GaussPoint * gp, InternalStateType type )

overridevirtual

Sets the value of a certain variable at a given integration point to the given value.

Parameters

value	Contains the value(s) to be set (in reduced form).
gp	Integration point.
type	Determines the type of internal variable.
type	Determines the type of internal variable.

Returns

Nonzero if ok, zero if var not supported.

Reimplemented from oofem::Material.

Definition at line 1974 of file structuralmaterial.C.

References oofem::Material::giveStatus(), oofem::StructuralMaterialStatus::letStrainVectorBe(), oofem::StructuralMaterialStatus::letStressVectorBe(), oofem::StructuralMaterialStatus::letTempStrainVectorBe(), and oofem::StructuralMaterialStatus::letTempStressVectorBe().

Referenced by oofem::ConcreteDPM::setIPValue().

sortPrincDirAndValCloseTo()

void oofem::StructuralMaterial::sortPrincDirAndValCloseTo ( FloatArray & pVal, FloatMatrix & pDir, const FloatMatrix & toPDir )

static

Method for sorting newly computed principal values (pVal) and corresponding principal directions (pDir) to be closed to some (often previous) principal directions (toPDir). pDir and toPDir should have eigenvectors stored in columns and normalized.

Parameters

pVal	New eigenvalues.
pDir	New eigenvectors.
toPDir	Old eigenvector.

Definition at line 1924 of file structuralmaterial.C.

References oofem::FloatArray::at(), and oofem::FloatMatrix::at().

Referenced by oofem::RCM2Material::giveRealPrincipalStressVector3d().

transformStrainVectorTo()

FloatArrayF< 6 > oofem::StructuralMaterial::transformStrainVectorTo ( const FloatMatrixF< 3, 3 > & base, const FloatArrayF< 6 > & strain, bool transpose = false )

static

Transforms 3d strain vector into another coordinate system.

Parameters

answer	Transformed strain vector
base	Transformation matrix. There are on each column stored unit vectors of coordinate system (so called base vectors) to which we do transformation. These vectors must be expressed in the same coordinate system as source strainVector.
strainVector	3d strain.
transpose	Determines if we transpose matrix before transforming.

Definition at line 1889 of file structuralmaterial.C.

References oofem::dot(), giveStrainVectorTranformationMtrx(), and oofem::transpose().

Referenced by giveIPValue(), oofem::MITC4Shell::giveMidplaneIPValue(), and oofem::CompoDamageMat::giveRealStressVector().

transformStressVectorTo()

FloatArrayF< 6 > oofem::StructuralMaterial::transformStressVectorTo ( const FloatMatrixF< 3, 3 > & base, const FloatArrayF< 6 > & stress, bool transpose = false )

static

Transforms 3d stress vector into another coordinate system.

Parameters

answer	Transformed stress vector.
base	Transformation matrix. There are on each column stored unit vectors of coordinate system (so called base vectors) to which we do transformation. These vectors must be expressed in the same coordinate system as source stressVector.
stressVector	Transformed 3d strain.
transpose	Determines if we transpose matrix before transforming.

Definition at line 1906 of file structuralmaterial.C.

References oofem::dot(), giveStressVectorTranformationMtrx(), and oofem::transpose().

Referenced by oofem::ConcreteDPM2::computeAlpha(), giveIPValue(), oofem::MITC4Shell::giveMidplaneIPValue(), oofem::CompoDamageMat::giveRealStressVector(), oofem::RCM2Material::giveRealStressVector(), oofem::RCSDEMaterial::giveRealStressVector(), oofem::RCSDMaterial::giveRealStressVector(), oofem::ConcreteDPM2::performRegularReturn(), and oofem::ConcreteDPM::performRegularReturn().

Friends And Related Symbol Documentation

CrossSection

friend class CrossSection

friend

Definition at line 699 of file structuralmaterial.h.

References CrossSection.

Referenced by CrossSection.

LayeredCrossSection

friend class LayeredCrossSection

friend

Definition at line 702 of file structuralmaterial.h.

References LayeredCrossSection.

Referenced by LayeredCrossSection.

SimpleCrossSection

friend class SimpleCrossSection

friend

Definition at line 701 of file structuralmaterial.h.

References SimpleCrossSection.

Referenced by SimpleCrossSection.

StructuralCrossSection

friend class StructuralCrossSection

friend

Definition at line 700 of file structuralmaterial.h.

References StructuralCrossSection.

Referenced by oofem::PerfectlyPlasticMaterial::computePlasticStiffnessAt(), oofem::PerfectlyPlasticMaterial::giveRealStressVector(), oofem::PerfectlyPlasticMaterial::GiveStressCorrectionBackToYieldSurface(), and StructuralCrossSection.

Member Data Documentation

referenceTemperature

double oofem::StructuralMaterial::referenceTemperature = 0.

protected

Reference temperature (temperature, when material has been built into structure).

Definition at line 124 of file structuralmaterial.h.

Referenced by computeStressIndependentStrainVector(), computeStressIndependentStrainVector_3d(), giveInputRecord(), giveReferenceTemperature(), and initializeFrom().

SCAbsTol

double oofem::StructuralMaterial::SCAbsTol = 1.e-12

protected

absolute stress tolerance for stress control

Definition at line 130 of file structuralmaterial.h.

Referenced by giveInputRecord(), and initializeFrom().

SCMaxiter

int oofem::StructuralMaterial::SCMaxiter = 100000

protected

maximum iterations for stress-control

Definition at line 132 of file structuralmaterial.h.

Referenced by giveFirstPKStressVector_StressControl(), giveRealStressVector_ShellStressControl(), giveRealStressVector_StressControl(), and initializeFrom().

SCRelTol

double oofem::StructuralMaterial::SCRelTol = 1.e-3

protected

relative tolerance for stress control

Definition at line 128 of file structuralmaterial.h.

Referenced by giveInputRecord(), and initializeFrom().

SCStiffMode

MatResponseMode oofem::StructuralMaterial::SCStiffMode = TangentStiffness

protected

stifness mode used in stress control

Definition at line 126 of file structuralmaterial.h.

Referenced by giveInputRecord(), giveRealStressVector_ShellStressControl(), giveRealStressVector_StressControl(), and initializeFrom().

svIndex

std::array< std::array< int, 3 >, 3 > oofem::StructuralMaterial::svIndex

static

Initial value:

= {{
    {1, 6, 5},
    {6, 2, 4},
    {5, 4, 3}
}}

Symmetric Voigt index map.

Definition at line 139 of file structuralmaterial.h.

Referenced by giveSymVI().

vIindex

std::array< std::array< int, 3 >, 3 > oofem::StructuralMaterial::vIindex

static

Initial value:

= {{
  {1, 6, 5},
  {9, 2, 4},
  {8, 7, 3}
}}

Voigt index map.

Definition at line 136 of file structuralmaterial.h.

Referenced by giveVI().

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The documentation for this class was generated from the following files:

• structuralmaterial.h
• structuralmaterial.C