Пример #1
0
void
MisesMat :: give1dStressStiffMtrx(FloatMatrix &answer,
                                  MatResponseMode mode,
                                  GaussPoint *gp,
                                  TimeStep *tStep)
{
    this->giveLinearElasticMaterial()->give1dStressStiffMtrx(answer, mode, gp, tStep);
    MisesMatStatus *status = static_cast< MisesMatStatus * >( this->giveStatus(gp) );
    double kappa = status->giveCumulativePlasticStrain();
    // increment of cumulative plastic strain as an indicator of plastic loading
    double tempKappa = status->giveTempCumulativePlasticStrain();
    double omega = status->giveTempDamage();
    double E = answer.at(1, 1);
    if ( mode != TangentStiffness ) {
        return;
    }


    if ( tempKappa <= kappa ) { // elastic loading - elastic stiffness plays the role of tangent stiffness
        answer.times(1 - omega);
        return;
    }


    // === plastic loading ===
    const FloatArray &stressVector = status->giveTempEffectiveStress();
    double stress = stressVector.at(1);
    answer.resize(1, 1);
    answer.at(1, 1) = ( 1 - omega ) * E * H / ( E + H ) - computeDamageParamPrime(tempKappa) * E / ( E + H ) * stress * signum(stress);
}
Пример #2
0
void
MisesMatGrad :: give3dGprime(FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep)
{
    MisesMatGradStatus *status = static_cast< MisesMatGradStatus * >( this->giveStatus(gp) );
    answer.resize(6, 1);
    answer.zero();
    double damage, tempDamage;
    double nlKappa, kappa;
    double gPrime;
    double tempKappa = status->giveTempCumulativePlasticStrain();
    damage = status->giveDamage();
    tempDamage = status->giveTempDamage();
    nlKappa =  status->giveNonlocalCumulatedStrain();
    kappa = mParam * nlKappa + ( 1. - mParam ) * tempKappa;
    if ( ( tempDamage - damage ) > 0 ) {
        const FloatArray &tempEffStress = status->giveTempEffectiveStress();
        for ( int i = 1; i <= 6; i++ ) {
            answer.at(i, 1) = tempEffStress.at(i);
        }

        gPrime = computeDamageParamPrime(kappa);
        answer.times(gPrime * mParam);
    } else {
        answer.zero();
    }
}
Пример #3
0
void
MisesMatNl :: give1dStressStiffMtrx(FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep)
{
    answer.resize(1, 1);
    answer.zero();
    LinearElasticMaterial *lmat = this->giveLinearElasticMaterial();
    double E = lmat->give('E', gp);
    double nlKappa;
    MisesMatNlStatus *status = static_cast< MisesMatNlStatus * >( this->giveStatus(gp) );
    double kappa = status->giveCumulativePlasticStrain();
    double tempKappa = status->giveTempCumulativePlasticStrain();
    double tempDamage = status->giveTempDamage();
    double damage = status->giveDamage();
    answer.at(1, 1) = ( 1 - tempDamage ) * E;
    if ( mode != TangentStiffness ) {
        return;
    }

    if ( tempKappa <= kappa ) { // elastic loading - elastic stiffness plays the role of tangent stiffness
        return;
    }

    // === plastic loading ===
    const FloatArray &stressVector = status->giveTempEffectiveStress();
    double stress = stressVector.at(1);
    answer.at(1, 1) = ( 1. - tempDamage ) * E * H / ( E + H );
    if ( tempDamage > damage ) {
        this->computeCumPlasticStrain(nlKappa, gp, tStep);
        answer.at(1, 1) = answer.at(1, 1) - ( 1 - mm ) * computeDamageParamPrime(nlKappa) * E / ( E + H ) * stress * sgn(stress);
    }
}
Пример #4
0
int
MisesMatNl :: giveLocalNonlocalStiffnessContribution(GaussPoint *gp, IntArray &loc, const UnknownNumberingScheme &s,
        FloatArray &lcontrib, TimeStep *atTime)
{
    int nrows, nsize, i, j;
    double sum, nlKappa, damage, tempDamage, dDamF;
    MisesMatNlStatus *status = ( MisesMatNlStatus * ) this->giveStatus(gp);
    StructuralElement *elem = ( StructuralElement * )( gp->giveElement() );
    FloatMatrix b;
    FloatArray stress;

    this->computeCumPlasticStrain(nlKappa, gp, atTime);
    damage = status->giveDamage();
    tempDamage = status->giveTempDamage();
    if ( ( tempDamage - damage ) > 0 ) {
        elem->giveLocationArray(loc, EID_MomentumBalance, s);
        status->giveTempEffectiveStress(stress);
        elem->computeBmatrixAt(gp, b);
        dDamF = computeDamageParamPrime(nlKappa);
        nrows = b.giveNumberOfColumns();
        nsize = stress.giveSize();
        lcontrib.resize(nrows);

        for ( i = 1; i <= nrows; i++ ) {
            sum = 0.0;
            for ( j = 1; j <= nsize; j++ ) {
                sum += b.at(j, i) * stress.at(j);
            }

            lcontrib.at(i) = sum * mm * dDamF;
        }
    }

    return 1;
}
Пример #5
0
// returns the consistent (algorithmic) tangent stiffness matrix
void
MisesMat :: give3dSSMaterialStiffnessMatrix(FloatMatrix &answer,
                                            MatResponseMode mode,
                                            GaussPoint *gp,
                                            TimeStep *atTime)
{
    // start from the elastic stiffness
    this->giveLinearElasticMaterial()->give3dMaterialStiffnessMatrix(answer, mode, gp, atTime);
    if ( mode != TangentStiffness ) {
        return;
    }

    MisesMatStatus *status = static_cast< MisesMatStatus * >( this->giveStatus(gp) );
    double kappa = status->giveCumulativePlasticStrain();
    double tempKappa = status->giveTempCumulativePlasticStrain();
    // increment of cumulative plastic strain as an indicator of plastic loading
    double dKappa = tempKappa - kappa;

    if ( dKappa <= 0.0 ) { // elastic loading - elastic stiffness plays the role of tangent stiffness
        return;
    }

    // === plastic loading ===

    // yield stress at the beginning of the step
    double sigmaY = sig0 + H * kappa;

    // trial deviatoric stress and its norm
    StressVector trialStressDev(_3dMat);
    double trialStressVol;
    status->giveTrialStressVol(trialStressVol);
    status->giveTrialStressDev(trialStressDev);
    double trialS = trialStressDev.computeStressNorm();

    // one correction term
    FloatMatrix stiffnessCorrection(6, 6);
    stiffnessCorrection.beDyadicProductOf(trialStressDev, trialStressDev);
    double factor = -2. * sqrt(6.) * G * G / trialS;
    double factor1 = factor * sigmaY / ( ( H + 3. * G ) * trialS * trialS );
    stiffnessCorrection.times(factor1);
    answer.add(stiffnessCorrection);

    // another correction term
    stiffnessCorrection.bePinvID();
    double factor2 = factor * dKappa;
    stiffnessCorrection.times(factor2);
    answer.add(stiffnessCorrection);

    //influence of damage
    //    double omega = computeDamageParam(tempKappa);
    double omega = status->giveTempDamage();
    answer.times(1. - omega);
    FloatArray effStress;
    status->giveTempEffectiveStress(effStress);
    double omegaPrime = computeDamageParamPrime(tempKappa);
    double scalar = -omegaPrime *sqrt(6.) * G / ( 3. * G + H ) / trialS;
    stiffnessCorrection.beDyadicProductOf(effStress, trialStressDev);
    stiffnessCorrection.times(scalar);
    answer.add(stiffnessCorrection);
}
Пример #6
0
void
MisesMatGrad :: givePlaneStrainStiffMtrx(FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep)
{
    this->giveLinearElasticMaterial()->giveStiffnessMatrix(answer, mode, gp, tStep);
    if ( mode != TangentStiffness ) {
        return;
    }

    MisesMatGradStatus *status = static_cast< MisesMatGradStatus * >( this->giveStatus(gp) );
    double tempKappa = status->giveTempCumulativePlasticStrain();
    double kappa = status->giveCumulativePlasticStrain();
    double dKappa = tempKappa - kappa;
    double tempDamage = status->giveTempDamage();
    double damage = status->giveDamage();

    if ( dKappa <= 0.0 ) { // elastic loading - elastic stiffness plays the role of tangent stiffness
        return;
    }

    // === plastic loading ===
    // yield stress at the beginning of the step
    double sigmaY = sig0 + H * kappa;
    // trial deviatoric stress and its norm
    StressVector trialStressDev(status->giveTrialStressDev(), _PlaneStrain);
    double trialS = trialStressDev.computeStressNorm();
    // volumetric stress
    //double trialStressVol = status->giveTrialStressVol();
    // one correction term
    FloatMatrix stiffnessCorrection(4, 4);
    stiffnessCorrection.beDyadicProductOf(trialStressDev, trialStressDev);
    double factor = -2. * sqrt(6.) * G * G / trialS;
    double factor1 = factor * sigmaY / ( ( H + 3. * G ) * trialS * trialS );
    stiffnessCorrection.times(factor1);
    answer.add(stiffnessCorrection);
    // another correction term
    stiffnessCorrection.zero();
    stiffnessCorrection.at(1, 1) = stiffnessCorrection.at(2, 2) = stiffnessCorrection.at(3, 3) = 2. / 3.;
    stiffnessCorrection.at(1, 2) = stiffnessCorrection.at(1, 3) = stiffnessCorrection.at(2, 1) = -1. / 3.;
    stiffnessCorrection.at(2, 3) = stiffnessCorrection.at(3, 1) = stiffnessCorrection.at(3, 2) = -1. / 3.;
    stiffnessCorrection.at(4, 4) = 0.5;
    double factor2 = factor * dKappa;
    stiffnessCorrection.times(factor2);
    answer.add(stiffnessCorrection);
    //influence of damage
    answer.times(1 - tempDamage);
    if ( tempDamage > damage ) {
        const FloatArray &effStress = status->giveTempEffectiveStress();
        double nlKappa = status->giveNonlocalCumulatedStrain();
        kappa = mParam * nlKappa + ( 1. - mParam ) * tempKappa;
        double omegaPrime = computeDamageParamPrime(kappa);
        double scalar = -omegaPrime *sqrt(6.) * G / ( 3. * G + H ) / trialS;
        stiffnessCorrection.beDyadicProductOf(effStress, trialStressDev);
        stiffnessCorrection.times( scalar * ( 1. - mParam ) );
        answer.add(stiffnessCorrection);
    }
}
Пример #7
0
void
MisesMatGrad :: give3dMaterialStiffnessMatrix(FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep)
{
    MisesMatGradStatus *status = static_cast< MisesMatGradStatus * >( this->giveStatus(gp) );
    this->giveLinearElasticMaterial()->give3dMaterialStiffnessMatrix(answer, mode, gp, tStep);
    // start from the elastic stiffness
    if ( mode != TangentStiffness ) {
        return;
    }

    double tempKappa = status->giveTempCumulativePlasticStrain();
    double kappa = status->giveCumulativePlasticStrain();
    double dKappa = tempKappa - kappa;

    if ( dKappa > 0.0 ) {
        double tempDamage = status->giveTempDamage();
        double damage = status->giveDamage();
        double sigmaY = sig0 + H * kappa;
        // trial deviatoric stress and its norm
        StressVector trialStressDev(status->giveTrialStressDev(), _3dMat);
        /*****************************************************/
        //double trialStressVol = status->giveTrialStressVol();
        /****************************************************/
        double trialS = trialStressDev.computeStressNorm();
        // one correction term
        FloatMatrix stiffnessCorrection(6, 6);
        stiffnessCorrection.beDyadicProductOf(trialStressDev, trialStressDev);
        double factor = -2. * sqrt(6.) * G * G / trialS;
        double factor1 = factor * sigmaY / ( ( H + 3. * G ) * trialS * trialS );
        stiffnessCorrection.times(factor1);
        answer.add(stiffnessCorrection);
        // another correction term
        stiffnessCorrection.bePinvID();
        double factor2 = factor * dKappa;
        stiffnessCorrection.times(factor2);
        answer.add(stiffnessCorrection);
        //influence of damage
        answer.times(1. - tempDamage);
        if ( tempDamage > damage ) {
            const FloatArray &effStress = status->giveTempEffectiveStress();
            double nlKappa =  status->giveNonlocalCumulatedStrain();
            kappa = mParam * nlKappa + ( 1. - mParam ) * tempKappa;
            double omegaPrime = computeDamageParamPrime(kappa);
            double scalar = -omegaPrime *sqrt(6.) * G / ( 3. * G + H ) / trialS;
            stiffnessCorrection.beDyadicProductOf(effStress, trialStressDev);
            stiffnessCorrection.times( scalar * ( 1. - mParam ) );
            answer.add(stiffnessCorrection);
        }
    }
}
Пример #8
0
// computes m*gprime*Btransposed*sigmaeff for the given Gauss point
// and returns 0 of damage is not growing, 1 if it is growing
// (if damage is not growing, the contribution is not considered at all)
int
RankineMatNl :: giveLocalNonlocalStiffnessContribution(GaussPoint *gp, IntArray &loc, const UnknownNumberingScheme &s,
                                                       FloatArray &lcontrib, TimeStep *atTime)
{
    int nrows, nsize, i, j;
    double sum, nlKappa, damage, tempDamage;
    RankineMatNlStatus *status = ( RankineMatNlStatus * ) this->giveStatus(gp);
    StructuralElement *elem = ( StructuralElement * )( gp->giveElement() );
    FloatMatrix b;
    FloatArray stress;

    damage = status->giveDamage();
    tempDamage = status->giveTempDamage();
    if ( tempDamage <= damage ) {
        return 0; // no contribution if damage is not growing
    }

    elem->giveLocationArray(loc, EID_MomentumBalance, s);
    status->giveTempEffectiveStress(stress);
    elem->computeBmatrixAt(gp, b);
    this->computeCumPlasticStrain(nlKappa, gp, atTime);
    double factor = computeDamageParamPrime(nlKappa);
    factor *= mm; // this factor is m*gprime
    nrows = b.giveNumberOfColumns();
    nsize = stress.giveSize();
    lcontrib.resize(nrows);
    // compute the product Btransposed*stress and multiply by factor
    for ( i = 1; i <= nrows; i++ ) {
        sum = 0.0;
        for ( j = 1; j <= nsize; j++ ) {
            sum += b.at(j, i) * stress.at(j);
        }

        lcontrib.at(i) = sum * factor;
    }

    return 1; // contribution will be considered
}
Пример #9
0
int
MisesMatNl :: giveLocalNonlocalStiffnessContribution(GaussPoint *gp, IntArray &loc, const UnknownNumberingScheme &s,
                                                     FloatArray &lcontrib, TimeStep *tStep)
{
    double nlKappa, damage, tempDamage, dDamF;
    MisesMatNlStatus *status = static_cast< MisesMatNlStatus * >( this->giveStatus(gp) );
    StructuralElement *elem = static_cast< StructuralElement * >( gp->giveElement() );
    FloatMatrix b;

    this->computeCumPlasticStrain(nlKappa, gp, tStep);
    damage = status->giveDamage();
    tempDamage = status->giveTempDamage();
    if ( ( tempDamage - damage ) > 0 ) {
        const FloatArray &stress = status->giveTempEffectiveStress();
        elem->giveLocationArray(loc, s);
        elem->computeBmatrixAt(gp, b);
        dDamF = computeDamageParamPrime(nlKappa);
        lcontrib.clear();
        lcontrib.plusProduct(b, stress, mm * dDamF);
    }

    return 1;
}
Пример #10
0
void
MisesMatGrad :: give1dStressStiffMtrx(FloatMatrix &answer, MatResponseMode mode, GaussPoint *gp, TimeStep *tStep)
{
    answer.resize(1, 1);
    LinearElasticMaterial *lmat = this->giveLinearElasticMaterial();
    double E = lmat->give('E', gp);
    answer.at(1, 1) = E;
    if ( mode != TangentStiffness ) {
        return;
    }

    MisesMatGradStatus *status = static_cast< MisesMatGradStatus * >( this->giveStatus(gp) );
    double tempKappa = status->giveTempCumulativePlasticStrain();
    // increment of cumulative plastic strain as an indicator of plastic loading
    double dKappa = ( tempKappa - status->giveCumulativePlasticStrain() );
    /********************************************************************/
    double tempDamage = status->giveTempDamage();
    double damage = status->giveDamage();
    /*********************************************************************/
    double nlKappa =  status->giveNonlocalCumulatedStrain();
    double kappa = mParam * nlKappa + ( 1. - mParam ) * tempKappa;
    if ( dKappa <= 0.0 ) {
        answer.at(1, 1) = ( 1. - tempDamage ) * E;
        return;
    }


    // === plastic loading ===
    const FloatArray &stressVector = status->giveTempEffectiveStress();
    double stress = stressVector.at(1);

    answer.at(1, 1) = ( 1. - tempDamage ) * E * H / ( E + H );
    if ( ( tempDamage - damage ) > 0 ) {
        answer.at(1, 1) = answer.at(1, 1) - ( 1. - mParam ) * computeDamageParamPrime(kappa) * E / ( E + H ) * signum(stress) * stress;
    }
}
Пример #11
0
void
RankineMatNl :: givePlaneStressStiffMtrx(FloatMatrix &answer, MatResponseForm form, MatResponseMode mode, GaussPoint *gp, TimeStep *atTime)
{
    if ( mode == ElasticStiffness ) {
        this->giveLinearElasticMaterial()->giveCharacteristicMatrix(answer, form, mode, gp, atTime);
        return;
    }

    RankineMatNlStatus *status = ( RankineMatNlStatus * ) this->giveStatus(gp);

    if ( mode == SecantStiffness ) {
        this->giveLinearElasticMaterial()->giveCharacteristicMatrix(answer, form, mode, gp, atTime);
        double damage = status->giveTempDamage();
        answer.times(1. - damage);
        return;
    }

    if ( mode == TangentStiffness ) {
        double tempDamage = status->giveTempDamage();
        double damage = status->giveDamage();
        double gprime;
        if ( tempDamage <= damage ) { // unloading
            gprime = 0.;
        } else { // loading
            double kappa;
            computeCumPlasticStrain(kappa, gp, atTime);
            gprime = computeDamageParamPrime(kappa);
            gprime *= ( 1. - mm );
        }

        evaluatePlaneStressStiffMtrx(answer, form, mode, gp, atTime, gprime);
        return;
    }

    _error("RankineMatNl :: givePlaneStressStiffMtrx ... unknown type of stiffness\n");
}