void
SimpleCrossSection :: giveCharMaterialStiffnessMatrix(FloatMatrix &answer, MatResponseMode rMode, GaussPoint *gp, TimeStep *tStep)
{
MaterialMode mode = gp->giveMaterialMode();
if ( mode == _2dBeam ) {
this->give2dBeamStiffMtrx(answer, rMode, gp, tStep);
} else if ( mode == _3dBeam ) {
this->give3dBeamStiffMtrx(answer, rMode, gp, tStep);
} else if ( mode == _2dPlate ) {
this->give2dPlateStiffMtrx(answer, rMode, gp, tStep);
} else if ( mode == _3dShell ) {
this->give3dShellStiffMtrx(answer, rMode, gp, tStep);
} else {
StructuralMaterial *mat = dynamic_cast< StructuralMaterial * >( this->giveMaterial(gp) );
if ( mode == _3dMat ) {
mat->give3dMaterialStiffnessMatrix(answer, rMode, gp, tStep);
} else if ( mode == _PlaneStress ) {
mat->givePlaneStressStiffMtrx(answer, rMode, gp, tStep);
} else if ( mode == _PlaneStrain ) {
mat->givePlaneStrainStiffMtrx(answer, rMode, gp, tStep);
} else if ( mode == _1dMat ) {
mat->give1dStressStiffMtrx(answer, rMode, gp, tStep);
} else {
mat->giveStiffnessMatrix(answer, rMode, gp, tStep);
}
}
}
void
SimpleCrossSection :: give3dDegeneratedShellStiffMtrx(FloatMatrix &answer, MatResponseMode rMode, GaussPoint *gp, TimeStep *tStep)
{
StructuralMaterial *mat = dynamic_cast< StructuralMaterial * >( this->giveMaterial(gp) );
mat->give3dMaterialStiffnessMatrix(answer, rMode, gp, tStep);
answer.at(1, 1) -= answer.at(1, 3) * answer.at(3, 1) / answer.at(3, 3);
answer.at(2, 1) -= answer.at(2, 3) * answer.at(3, 1) / answer.at(3, 3);
answer.at(1, 2) -= answer.at(1, 3) * answer.at(3, 2) / answer.at(3, 3);
answer.at(2, 2) -= answer.at(2, 3) * answer.at(3, 2) / answer.at(3, 3);
answer.at(3, 1) = 0.0;
answer.at(3, 2) = 0.0;
answer.at(3, 3) = 0.0;
answer.at(2, 3) = 0.0;
answer.at(1, 3) = 0.0;
}
void StructuralMaterialEvaluator :: solveYourself()
{
Domain *d = this->giveDomain(1);
MaterialMode mode = _3dMat;
FloatArray initialStrain(6);
gps.clear();
gps.reserve(d->giveNumberOfMaterialModels());
for ( int i = 1; i <= d->giveNumberOfMaterialModels(); i++ ) {
std :: unique_ptr< GaussPoint > gp = std::make_unique<GaussPoint>(nullptr, i, FloatArray(0), 1, mode);
gps.emplace_back( std :: move(gp) );
// Initialize the strain vector;
StructuralMaterialStatus *status = static_cast< StructuralMaterialStatus * >( d->giveMaterial(i)->giveStatus( gps[i-1].get() ) );
status->letStrainVectorBe(initialStrain);
}
std :: string outname = this->giveOutputBaseFileName() + ".matdata";
this->outfile.open( outname.c_str() );
this->timer.startTimer(EngngModelTimer :: EMTT_AnalysisTimer);
TimeStep *tStep = giveNextStep();
// Note, strain == strain-rate (kept as strain for brevity)
int maxiter = 100; // User input?
FloatArray stressC, deltaStrain, strain, stress, res;
stressC.resize( sControl.giveSize() );
res.resize( sControl.giveSize() );
FloatMatrix tangent, reducedTangent;
for ( int istep = 1; istep <= this->numberOfSteps; ++istep ) {
this->timer.startTimer(EngngModelTimer :: EMTT_SolutionStepTimer);
for ( int imat = 1; imat <= d->giveNumberOfMaterialModels(); ++imat ) {
GaussPoint *gp = gps[imat-1].get();
StructuralMaterial *mat = static_cast< StructuralMaterial * >( d->giveMaterial(imat) );
StructuralMaterialStatus *status = static_cast< StructuralMaterialStatus * >( mat->giveStatus(gp) );
strain = status->giveStrainVector();
// Update the controlled parts
for ( int j = 1; j <= eControl.giveSize(); ++j ) {
int p = eControl.at(j);
strain.at(p) = d->giveFunction( cmpntFunctions.at(p) )->evaluateAtTime( tStep->giveIntrinsicTime() );
}
for ( int j = 1; j <= sControl.giveSize(); ++j ) {
int p = sControl.at(j);
stressC.at(j) = d->giveFunction( cmpntFunctions.at(p) )->evaluateAtTime( tStep->giveIntrinsicTime() );
}
//strain.add(-100, {6.27e-06, 6.27e-06, 6.27e-06, 0, 0, 0});
for ( int iter = 1; iter < maxiter; iter++ ) {
#if 0
// Debugging:
mat->give3dMaterialStiffnessMatrix(tangent, TangentStiffness, gp, tStep);
tangent.printYourself("# tangent");
strain.zero();
mat->giveRealStressVector_3d(stress, gp, strain, tStep);
FloatArray strain2;
tangent.solveForRhs(stress, strain2);
strain2.printYourself("# thermal expansion");
break;
#endif
strain.printYourself("Macro strain guess");
mat->giveRealStressVector_3d(stress, gp, strain, tStep);
for ( int j = 1; j <= sControl.giveSize(); ++j ) {
res.at(j) = stressC.at(j) - stress.at( sControl.at(j) );
}
OOFEM_LOG_INFO("*** Time step: %d (t = %.2e), Material %d, Iteration: %d, Residual = %e (tolerance %.2e)\n",
istep, tStep->giveIntrinsicTime(), imat, iter, res.computeNorm(), tolerance);
if ( res.computeNorm() <= tolerance ) {
break;
} else {
if ( tangent.giveNumberOfRows() == 0 || !keepTangent ) {
mat->give3dMaterialStiffnessMatrix(tangent, TangentStiffness, gp, tStep);
}
// Pick out the stress-controlled part;
reducedTangent.beSubMatrixOf(tangent, sControl, sControl);
// Update stress-controlled part of the strain
reducedTangent.solveForRhs(res, deltaStrain);
//deltaStrain.printYourself("deltaStrain");
for ( int j = 1; j <= sControl.giveSize(); ++j ) {
strain.at( sControl.at(j) ) += deltaStrain.at(j);
}
}
}
if ( res.computeNorm() > tolerance ) {
OOFEM_WARNING("Residual did not converge!");
}
// This material model has converged, so we update it and go on to the next.
gp->updateYourself(tStep);
}
this->timer.stopTimer(EngngModelTimer :: EMTT_SolutionStepTimer);
this->doStepOutput(tStep);
tStep = giveNextStep();
}
this->timer.stopTimer(EngngModelTimer :: EMTT_AnalysisTimer);
this->outfile.close();
}
void
SimpleCrossSection :: giveStiffnessMatrix_3d(FloatMatrix &answer, MatResponseMode rMode, GaussPoint *gp, TimeStep *tStep)
{
StructuralMaterial *mat = dynamic_cast< StructuralMaterial * >( this->giveMaterial(gp) );
mat->give3dMaterialStiffnessMatrix(answer, rMode, gp, tStep);
}