void TwoStepPeriodicCondition<TDim>::GetDofList(DofsVectorType& rElementalDofList, ProcessInfo& rCurrentProcessInfo)
{
    KRATOS_TRY;

    switch ( rCurrentProcessInfo[FRACTIONAL_STEP] )
    {
    case 1:
    {
        this->GetVelocityDofList(rElementalDofList,rCurrentProcessInfo);
        break;
    }
    case 5:
    {
        this->GetPressureDofList(rElementalDofList,rCurrentProcessInfo);
        break;
    }
    case 6:
    {
        this->GetVelocityDofList(rElementalDofList,rCurrentProcessInfo);
        break;
    }
    default:
    {
        KRATOS_THROW_ERROR(std::logic_error,"Unexpected value for FRACTIONAL_STEP index: ",rCurrentProcessInfo[FRACTIONAL_STEP]);
    }
    }

    KRATOS_CATCH("");
}
//************************************************************************************
//************************************************************************************
// this subroutine calculates the nodal contributions for the explicit steps of the
// fractional step procedure
void UpdatedLagrangianFluid3Dinc::InitializeSolutionStep(ProcessInfo& CurrentProcessInfo)
{
    KRATOS_TRY
    //save original Area
    mA0 = GeometryUtils::CalculateVolume3D(GetGeometry());

    KRATOS_CATCH("");
}
int TwoStepPeriodicCondition<TDim>::Check(const ProcessInfo& rCurrentProcessInfo)
{
    KRATOS_TRY;

    return Condition::Check(rCurrentProcessInfo);

    KRATOS_CATCH("");
}
예제 #4
0
    boost::python::object AuxiliaryUtilities::GetIthSubModelPartName(ModelPart& rParentModelPart, const int& required_i){
        KRATOS_TRY;                             
        int current_i = 0;
        for (ModelPart::SubModelPartsContainerType::iterator sub_model_part = rParentModelPart.SubModelPartsBegin(); sub_model_part != rParentModelPart.SubModelPartsEnd(); ++sub_model_part) {

            if(current_i == required_i) {
                const std::string& name = (*sub_model_part).Name();
                return boost::python::object(name);
            }
            current_i++;
        }

        KRATOS_THROW_ERROR(std::runtime_error, "The function GetIthSubModelPartName required a position greater than the number of SubModelParts! The number of present submodelparts is ", rParentModelPart.NumberOfSubModelParts());
        
        KRATOS_CATCH("");  
    };
예제 #5
0
    boost::python::object AuxiliaryUtilities::GetIthSubModelPartIsForceIntegrationGroup(ModelPart& rParentModelPart, const int& required_i){
        KRATOS_TRY;                             
        int current_i = 0;
        for (ModelPart::SubModelPartsContainerType::iterator sub_model_part = rParentModelPart.SubModelPartsBegin(); sub_model_part != rParentModelPart.SubModelPartsEnd(); ++sub_model_part) {

            if(current_i == required_i) {
                const int is_force_integration_group = (*sub_model_part)[FORCE_INTEGRATION_GROUP];
                return boost::python::object( (bool) (is_force_integration_group) );
            }
            current_i++;
        }

        KRATOS_THROW_ERROR(std::runtime_error, "The function GetIthSubModelPartIsForceIntegrationGroup required a position greater than the number of SubModelParts! The number of present submodelparts is ", rParentModelPart.NumberOfSubModelParts());
        
        KRATOS_CATCH("");        
    };
예제 #6
0
//************************************************************************************
//************************************************************************************
void Monolithic2DNeumann::GetDofList(DofsVectorType& ElementalDofList,ProcessInfo& CurrentProcessInfo)
{
    KRATOS_TRY
    unsigned int number_of_nodes = GetGeometry().PointsNumber();
    unsigned int dim = 2;
    unsigned int node_size = dim;

    if(ElementalDofList.size() != number_of_nodes*node_size)
        ElementalDofList.resize(number_of_nodes*node_size);

    for (unsigned int i=0; i<number_of_nodes; i++)
    {
        ElementalDofList[i*node_size] = GetGeometry()[i].pGetDof(VELOCITY_X);
        ElementalDofList[i*node_size+1] = GetGeometry()[i].pGetDof(VELOCITY_Y);
    }
    KRATOS_CATCH("");
}
예제 #7
0
    ModelPart::NodesContainerType::Pointer AuxiliaryUtilities::GetIthSubModelPartNodes(ModelPart& rParentModelPart, const int& required_i){
        KRATOS_TRY; 
        
        int current_i = 0;
        for (ModelPart::SubModelPartsContainerType::iterator sub_model_part = rParentModelPart.SubModelPartsBegin(); sub_model_part != rParentModelPart.SubModelPartsEnd(); ++sub_model_part) {

            if(current_i == required_i) {
                return (*sub_model_part).pNodes();
            }
            
            current_i++;
        }

        KRATOS_THROW_ERROR(std::runtime_error, "The function GetIthSubModelPartNodes required a position greater than the number of SubModelParts! The number of present submodelparts is ", rParentModelPart.NumberOfSubModelParts());
        
        KRATOS_CATCH("");  
        
    }       
예제 #8
0
	void MonolithicPFEM22D::AddExplicitContribution(ProcessInfo& rCurrentProcessInfo)
	{
		KRATOS_TRY;

		switch ( rCurrentProcessInfo[FRACTIONAL_STEP] )
		{
			case 10: //calculating pressure projection. notthing returned. saving data in PRESS_PROJ, PRESS_PROJ_NO_RO , NODAL_MASS and NODAL_AREA
			{
				this->CalculatePressureProjection(rCurrentProcessInfo);
				break;
			}			
			default:
			{
				KRATOS_THROW_ERROR(std::logic_error,"Unexpected value for FRACTIONAL_STEP index: ",rCurrentProcessInfo[FRACTIONAL_STEP]);
			}
		}

		KRATOS_CATCH("");
	}
예제 #9
0
    void PillCluster3D::CalculateDampingMatrix(MatrixType& rDampingMatrix, ProcessInfo& r_process_info) {}

    //**************************************************************************************************************************************************
    //**************************************************************************************************************************************************

    void PillCluster3D::GetDofList(DofsVectorType& ElementalDofList, ProcessInfo& r_process_info) {}

    //**************************************************************************************************************************************************
    //**************************************************************************************************************************************************

    void PillCluster3D::InitializeSolutionStep(ProcessInfo& r_process_info) {
        
        KRATOS_TRY

        KRATOS_CATCH("")
        
    }

    //**************************************************************************************************************************************************
    //**************************************************************************************************************************************************

    void PillCluster3D::FinalizeSolutionStep(ProcessInfo& r_process_info) {}

    //**************************************************************************************************************************************************
    //**************************************************************************************************************************************************
    
    void PillCluster3D::Calculate(const Variable<double>& rVariable, double& Output, const ProcessInfo& r_process_info) {
          
        KRATOS_TRY
예제 #10
0
//************************************************************************************
//************************************************************************************
// this subroutine calculates the nodal contributions for the explicit steps of the
// fractional step procedure
void NDFluid2DCrankNicolson::InitializeSolutionStep(ProcessInfo& CurrentProcessInfo)
{
    KRATOS_TRY
    int FractionalStepNumber = CurrentProcessInfo[FRACTIONAL_STEP];

    //getting data for the given geometry
    double Area;
    GeometryUtils::CalculateGeometryData(GetGeometry(),msDN_DX,msN,Area);

    if(FractionalStepNumber  == 5) //calculation of stabilization terms
    {

        array_1d<double,3>& fv0 = GetGeometry()[0].FastGetSolutionStepValue(FRACT_VEL);
        array_1d<double,3>& w0 = GetGeometry()[0].FastGetSolutionStepValue(MESH_VELOCITY);
        array_1d<double,3>& press_proj0 = GetGeometry()[0].FastGetSolutionStepValue(PRESS_PROJ);
        array_1d<double,3>& conv_proj0 = GetGeometry()[0].FastGetSolutionStepValue(CONV_PROJ);
        double p0 = GetGeometry()[0].FastGetSolutionStepValue(PRESSURE);
        const double rho0 = GetGeometry()[0].FastGetSolutionStepValue(DENSITY);

        array_1d<double,3>& fv1 = GetGeometry()[1].FastGetSolutionStepValue(FRACT_VEL);
        array_1d<double,3>& w1 = GetGeometry()[1].FastGetSolutionStepValue(MESH_VELOCITY);
        array_1d<double,3>& press_proj1 = GetGeometry()[1].FastGetSolutionStepValue(PRESS_PROJ);
        array_1d<double,3>& conv_proj1 = GetGeometry()[1].FastGetSolutionStepValue(CONV_PROJ);
        double p1 = GetGeometry()[1].FastGetSolutionStepValue(PRESSURE);
        const double rho1 = GetGeometry()[1].FastGetSolutionStepValue(DENSITY);

        array_1d<double,3>& fv2 = GetGeometry()[2].FastGetSolutionStepValue(FRACT_VEL);
        array_1d<double,3>& w2 = GetGeometry()[2].FastGetSolutionStepValue(MESH_VELOCITY);
        array_1d<double,3>& press_proj2 = GetGeometry()[2].FastGetSolutionStepValue(PRESS_PROJ);
        array_1d<double,3>& conv_proj2 = GetGeometry()[2].FastGetSolutionStepValue(CONV_PROJ);
        double p2 = GetGeometry()[2].FastGetSolutionStepValue(PRESSURE);
        const double rho2 = GetGeometry()[2].FastGetSolutionStepValue(DENSITY);

        double density = 0.3333333333333333333333*(rho0 + rho1 + rho2 );

        //calculation of the pressure gradient (saved in ms_vel_gauss)
        ms_vel_gauss[0] = msDN_DX(0,0)*(p0) + msDN_DX(1,0)*(p1) + msDN_DX(2,0)*(p2);
        ms_vel_gauss[1] = msDN_DX(0,1)*(p0) + msDN_DX(1,1)*(p1) + msDN_DX(2,1)*(p2);
        ms_vel_gauss *= Area;

        //press_proj += G*p
        press_proj0[0] += msN[0]*ms_vel_gauss[0];
        press_proj0[1] += msN[0]*ms_vel_gauss[1];

        press_proj1[0] += msN[1]*ms_vel_gauss[0];
        press_proj1[1] += msN[1]*ms_vel_gauss[1];

        press_proj2[0] += msN[2]*ms_vel_gauss[0];
        press_proj2[1] += msN[2]*ms_vel_gauss[1];

        // vel_gauss = sum( N[i]*(vel[i]-mesh_vel[i]), i=0, number_of_points) (note that the fractional step vel is used)
        ms_vel_gauss[0] =  msN[0]*(fv0[0]-w0[0]) + msN[1]*(fv1[0]-w1[0]) +  msN[2]*(fv2[0]-w2[0]);
        ms_vel_gauss[1] =  msN[0]*(fv0[1]-w0[1]) + msN[1]*(fv1[1]-w1[1]) +  msN[2]*(fv2[1]-w2[1]);

        //calculating convective auxiliary vector
        noalias(ms_u_DN) = prod(msDN_DX , ms_vel_gauss);

        //attention changing the meaning of ms_vel_gauss!!
        ms_vel_gauss[0] = ms_u_DN[0] * fv0[0] + ms_u_DN[1] * fv1[0] + ms_u_DN[2] * fv2[0];
        ms_vel_gauss[1] = ms_u_DN[0] * fv0[1] + ms_u_DN[1] * fv1[1] + ms_u_DN[2] * fv2[1];
        ms_vel_gauss *= Area * density;

        // conv_proj += C*u
        conv_proj0[0] += msN[0]*ms_vel_gauss[0];
        conv_proj0[1] += msN[0]*ms_vel_gauss[1];

        conv_proj1[0] += msN[1]*ms_vel_gauss[0];
        conv_proj1[1] += msN[1]*ms_vel_gauss[1];

        conv_proj2[0] += msN[2]*ms_vel_gauss[0];
        conv_proj2[1] += msN[2]*ms_vel_gauss[1];
    }
    else if(FractionalStepNumber == 6) //calculation of velocities
    {
        //outside of the element it is performed a loop on the elements in which it is considered nodally
        //v = vfrac - Dt/Mnodal * G*(p-pold)
        // the term G*(p-pold) needs to be assembled by element. the contribution is thus directly added to the nodal contrib

        double p0 = GetGeometry()[0].FastGetSolutionStepValue(PRESSURE);
        double p0old = GetGeometry()[0].FastGetSolutionStepValue(PRESSURE_OLD_IT);
        array_1d<double,3>& fv0 = GetGeometry()[0].FastGetSolutionStepValue(FRACT_VEL);
// 			const double rho0 = GetGeometry()[0].FastGetSolutionStepValue(DENSITY);
// 			const double eps0 = GetGeometry()[0].FastGetSolutionStepValue(POROSITY);

        double p1 = GetGeometry()[1].FastGetSolutionStepValue(PRESSURE);
        double p1old = GetGeometry()[1].FastGetSolutionStepValue(PRESSURE_OLD_IT);
        array_1d<double,3>& fv1 = GetGeometry()[1].FastGetSolutionStepValue(FRACT_VEL);
// 			const double rho1 = GetGeometry()[1].FastGetSolutionStepValue(DENSITY);
// 			const double eps1 = GetGeometry()[1].FastGetSolutionStepValue(POROSITY);


        double p2 = GetGeometry()[2].FastGetSolutionStepValue(PRESSURE);
        double p2old = GetGeometry()[2].FastGetSolutionStepValue(PRESSURE_OLD_IT);
        array_1d<double,3>& fv2 = GetGeometry()[2].FastGetSolutionStepValue(FRACT_VEL);
// 			const double rho2 = GetGeometry()[2].FastGetSolutionStepValue(DENSITY);
// 			const double eps2 = GetGeometry()[2].FastGetSolutionStepValue(POROSITY);

// 			double density = 0.33333333333333333333333*(rho0 + rho1 + rho2);
// 			double eps = 0.33333333333333333333333*(eps0 + eps1 + eps2);


        double p_avg =	msN[0]*(p0 - p0old)
                        + msN[1]*(p1 - p1old)
                        + msN[2]*(p2 - p2old) ;
        p_avg *= Area;
// 			KRATOS_WATCH(p_avg);
// 			KRATOS_WATCH(eps);
        fv0[0] += msDN_DX(0,0)*p_avg;
        fv0[1] += msDN_DX(0,1)*p_avg;
        fv1[0] += msDN_DX(1,0)*p_avg;
        fv1[1] += msDN_DX(1,1)*p_avg;
        fv2[0] += msDN_DX(2,0)*p_avg;
        fv2[1] += msDN_DX(2,1)*p_avg;




    }


    KRATOS_CATCH("");
}
예제 #11
0
//************************************************************************************
//************************************************************************************
//calculation by component of the fractional step velocity corresponding to the first stage
void NDFluid2DCrankNicolson::Stage2(MatrixType& rLeftHandSideMatrix, VectorType& rRightHandSideVector,
                                    ProcessInfo& rCurrentProcessInfo)
{
    KRATOS_TRY;

    unsigned int number_of_points = 3;

    if(rLeftHandSideMatrix.size1() != number_of_points)
        rLeftHandSideMatrix.resize(number_of_points,number_of_points,false);

    if(rRightHandSideVector.size() != number_of_points)
        rRightHandSideVector.resize(number_of_points,false);

    //getting data for the given geometry
    double Area;
    GeometryUtils::CalculateGeometryData(GetGeometry(),msDN_DX,msN,Area);


    const array_1d<double,3>& fv0 = GetGeometry()[0].FastGetSolutionStepValue(FRACT_VEL);
    const array_1d<double,3>& w0 = GetGeometry()[0].FastGetSolutionStepValue(MESH_VELOCITY);
    const array_1d<double,3>& proj0 = GetGeometry()[0].FastGetSolutionStepValue(PRESS_PROJ);
    double p0 = GetGeometry()[0].FastGetSolutionStepValue(PRESSURE);
    double p0old = GetGeometry()[0].FastGetSolutionStepValue(PRESSURE_OLD_IT);
    const double nu0 = GetGeometry()[0].FastGetSolutionStepValue(VISCOSITY);
    const double rho0 = GetGeometry()[0].FastGetSolutionStepValue(DENSITY);
    const double eps0 = GetGeometry()[0].FastGetSolutionStepValue(POROSITY);


    const array_1d<double,3>& fv1 = GetGeometry()[1].FastGetSolutionStepValue(FRACT_VEL);
    const array_1d<double,3>& w1 = GetGeometry()[1].FastGetSolutionStepValue(MESH_VELOCITY);
    const array_1d<double,3>& proj1 = GetGeometry()[1].FastGetSolutionStepValue(PRESS_PROJ);
    double p1 = GetGeometry()[1].FastGetSolutionStepValue(PRESSURE);
    double p1old = GetGeometry()[1].FastGetSolutionStepValue(PRESSURE_OLD_IT);
    const double nu1 = GetGeometry()[1].FastGetSolutionStepValue(VISCOSITY);
    const double rho1 = GetGeometry()[1].FastGetSolutionStepValue(DENSITY);
    const double eps1 = GetGeometry()[1].FastGetSolutionStepValue(POROSITY);


    const array_1d<double,3>& fv2 = GetGeometry()[2].FastGetSolutionStepValue(FRACT_VEL);
    const array_1d<double,3>& w2 = GetGeometry()[2].FastGetSolutionStepValue(MESH_VELOCITY);
    const array_1d<double,3>& proj2 = GetGeometry()[2].FastGetSolutionStepValue(PRESS_PROJ);
    double p2 = GetGeometry()[2].FastGetSolutionStepValue(PRESSURE);
    double p2old = GetGeometry()[2].FastGetSolutionStepValue(PRESSURE_OLD_IT);
    const double nu2 = GetGeometry()[2].FastGetSolutionStepValue(VISCOSITY);
    const double rho2 = GetGeometry()[2].FastGetSolutionStepValue(DENSITY);
    const double eps2 = GetGeometry()[2].FastGetSolutionStepValue(POROSITY);

//3PG-------------
//ms_vel_gauss
//3PG-------------


    // vel_gauss = sum( N[i]*(vel[i]-mesh_vel[i]), i=0, number_of_points) (note that the fractional step vel is used)
    ms_vel_gauss[0] =  msN[0]*(fv0[0]-w0[0]) + msN[1]*(fv1[0]-w1[0]) +  msN[2]*(fv2[0]-w2[0]);
    ms_vel_gauss[1] =  msN[0]*(fv0[1]-w0[1]) + msN[1]*(fv1[1]-w1[1]) +  msN[2]*(fv2[1]-w2[1]);

    //calculating convective auxiliary vector
//3PG-------------
//ms_u_DN
//3PG-------------
    noalias(ms_u_DN) = prod(msDN_DX , ms_vel_gauss);

    //calculating average density and viscosity
    double nu = 0.33333333333333*(nu0 + nu1 + nu2 );
    double density = 0.33333333333333*(rho0 + rho1 + rho2 );

    //DIAMETER of the element
    //double dp = 0.33333333333333*(d0+d1+d2)
    //POROSITY of the element: average value of the porosity
    double eps = 0.3333333333333333333333*(eps0 + eps1 + eps2 );

    //Getting delta time value for the restriction over tau.
    double Dt = rCurrentProcessInfo[DELTA_TIME];

    //calculating parameter tau (saved internally to each element)
    double h = sqrt(2.00*Area);
    double norm_u = ms_vel_gauss[0]*ms_vel_gauss[0] + ms_vel_gauss[1]*ms_vel_gauss[1];
    norm_u = sqrt(norm_u);
    double tau = 1.00 / ( 4.00*nu/(h*h) + 2.00*norm_u/h );

    //tau = min{tau; Dt}
    if(tau > Dt)
    {
        tau = Dt;
    }

    //getting the BDF2 coefficients (not fixed to allow variable time step)
    //the coefficients INCLUDE the time step
    const Vector& BDFcoeffs = rCurrentProcessInfo[BDF_COEFFICIENTS];

    //CALCULATION OF THE LEFT HAND SIDE
    //laplacian term	       L = Dt * gradN  *eps * trans(gradN);
    //stabilization term       Spp = tau * gradN * eps * trans(gradN);
    noalias(rLeftHandSideMatrix) = ((1.00/BDFcoeffs[0] + tau)/density*eps) * prod(msDN_DX,trans(msDN_DX));

    //calculation of the RHS
    // RHS = -G*vfrac
    double Gaux;
    Gaux =  msDN_DX(0,0)*fv0[0] + msDN_DX(0,1)*fv0[1];
    Gaux += msDN_DX(1,0)*fv1[0] + msDN_DX(1,1)*fv1[1];
    Gaux += msDN_DX(2,0)*fv2[0] + msDN_DX(2,1)*fv2[1];
    rRightHandSideVector[0] = - Gaux * msN[0];
    rRightHandSideVector[1] = - Gaux * msN[1];
    rRightHandSideVector[2] = - Gaux * msN[2];

    //attention!! changing the meaning of ms_vel_gauss
    //Inserting the influence of POROSITY!
    // RHS += Sz * proj*eps
    //contrib of Spy*proj
    ms_vel_gauss[0] = msN[0]*proj0[0] + msN[1]*proj1[0] + msN[2]*proj2[0];
    ms_vel_gauss[1] = msN[0]*proj0[1] + msN[1]*proj1[1] + msN[2]*proj2[1];
    ms_vel_gauss *= tau*eps;
    noalias(rRightHandSideVector) += prod(msDN_DX , ms_vel_gauss);

    //dirichlet contribution
    ms_temp_vec_np[0] = p0;
    ms_temp_vec_np[1] = p1;
    ms_temp_vec_np[2] = p2;
    noalias(rRightHandSideVector) -= prod(rLeftHandSideMatrix,ms_temp_vec_np);

    // RHS += dt * L *eps* pold
    ms_temp_vec_np[0] = p0old;
    ms_temp_vec_np[1] = p1old;
    ms_temp_vec_np[2] = p2old;
    noalias(ms_vel_gauss) = prod(trans(msDN_DX),ms_temp_vec_np);
    noalias(rRightHandSideVector) += (1.00/BDFcoeffs[0]/density*eps) * prod(msDN_DX,ms_vel_gauss);

    //multiplicating by the area
    rLeftHandSideMatrix *= Area;
    rRightHandSideVector *= Area;

    //adding contributions to nodal areas following the corresponding lumping term
    double nodal_contrib = 0.333333333333333333333333333 * Area*density;
    GetGeometry()[0].FastGetSolutionStepValue(NODAL_MASS) += nodal_contrib;
    GetGeometry()[1].FastGetSolutionStepValue(NODAL_MASS) += nodal_contrib;
    GetGeometry()[2].FastGetSolutionStepValue(NODAL_MASS) += nodal_contrib;

    KRATOS_CATCH("");
}
예제 #12
0
//************************************************************************************
//************************************************************************************
//calculation by component of the fractional step velocity corresponding to the first stage
void NDFluid2DCrankNicolson::Stage1(MatrixType& rLeftHandSideMatrix, VectorType& rRightHandSideVector,
                                    ProcessInfo& rCurrentProcessInfo, unsigned int ComponentIndex)
{
    KRATOS_TRY;

    const unsigned int number_of_points = 3;

    if(rLeftHandSideMatrix.size1() != number_of_points)
        rLeftHandSideMatrix.resize(number_of_points,number_of_points,false); //false says not to preserve existing storage!!

    if(rRightHandSideVector.size() != number_of_points)
        rRightHandSideVector.resize(number_of_points,false); //false says not to preserve existing storage!!

    //getting data for the given geometry
    double Area;
    GeometryUtils::CalculateGeometryData(GetGeometry(),msDN_DX,msN,Area);

    //getting the velocity vector on the nodes

    //getting the velocity on the nodes
    const array_1d<double,3>& fv0 = GetGeometry()[0].FastGetSolutionStepValue(FRACT_VEL,0);
    const array_1d<double,3>& fv0_old = GetGeometry()[0].FastGetSolutionStepValue(VELOCITY,1);
    const array_1d<double,3>& w0 = GetGeometry()[0].FastGetSolutionStepValue(MESH_VELOCITY);
    const array_1d<double,3>& w0_old = GetGeometry()[0].FastGetSolutionStepValue(MESH_VELOCITY,1);
    const array_1d<double,3>& proj0 = GetGeometry()[0].FastGetSolutionStepValue(CONV_PROJ);
    const array_1d<double,3>& proj0_old = GetGeometry()[0].FastGetSolutionStepValue(CONV_PROJ,1);
    double p0old = GetGeometry()[0].FastGetSolutionStepValue(PRESSURE_OLD_IT);
    const double nu0 = GetGeometry()[0].FastGetSolutionStepValue(VISCOSITY);
    const double rho0 = GetGeometry()[0].FastGetSolutionStepValue(DENSITY);
    const double fcomp0 = GetGeometry()[0].FastGetSolutionStepValue(BODY_FORCE)[ComponentIndex];
    const double eps0 = GetGeometry()[0].FastGetSolutionStepValue(POROSITY);
    const double dp0 = GetGeometry()[0].FastGetSolutionStepValue(DIAMETER);


    const array_1d<double,3>& fv1 = GetGeometry()[1].FastGetSolutionStepValue(FRACT_VEL);
    const array_1d<double,3>& fv1_old = GetGeometry()[1].FastGetSolutionStepValue(VELOCITY,1);
    const array_1d<double,3>& w1 = GetGeometry()[1].FastGetSolutionStepValue(MESH_VELOCITY);
    const array_1d<double,3>& w1_old = GetGeometry()[1].FastGetSolutionStepValue(MESH_VELOCITY,1);
    const array_1d<double,3>& proj1 = GetGeometry()[1].FastGetSolutionStepValue(CONV_PROJ);
    double p1old = GetGeometry()[1].FastGetSolutionStepValue(PRESSURE_OLD_IT);
    const array_1d<double,3>& proj1_old = GetGeometry()[1].FastGetSolutionStepValue(CONV_PROJ,1);
    const double nu1 = GetGeometry()[1].FastGetSolutionStepValue(VISCOSITY);
    const double rho1 = GetGeometry()[1].FastGetSolutionStepValue(DENSITY);
    const double fcomp1 = GetGeometry()[1].FastGetSolutionStepValue(BODY_FORCE)[ComponentIndex];
    const double eps1 = GetGeometry()[1].FastGetSolutionStepValue(POROSITY);
    const double dp1 = GetGeometry()[1].FastGetSolutionStepValue(DIAMETER);


    const array_1d<double,3>& fv2 = GetGeometry()[2].FastGetSolutionStepValue(FRACT_VEL);
    const array_1d<double,3>& fv2_old = GetGeometry()[2].FastGetSolutionStepValue(VELOCITY,1);
    const array_1d<double,3>& w2 = GetGeometry()[2].FastGetSolutionStepValue(MESH_VELOCITY);
    const array_1d<double,3>& w2_old = GetGeometry()[2].FastGetSolutionStepValue(MESH_VELOCITY,1);
    const array_1d<double,3>& proj2 = GetGeometry()[2].FastGetSolutionStepValue(CONV_PROJ);
    const array_1d<double,3>& proj2_old = GetGeometry()[2].FastGetSolutionStepValue(CONV_PROJ,1);
    double p2old = GetGeometry()[2].FastGetSolutionStepValue(PRESSURE_OLD_IT);
    const double nu2 = GetGeometry()[2].FastGetSolutionStepValue(VISCOSITY);
    const double rho2 = GetGeometry()[2].FastGetSolutionStepValue(DENSITY);
    const double fcomp2 = GetGeometry()[2].FastGetSolutionStepValue(BODY_FORCE)[ComponentIndex];
    const double eps2 = GetGeometry()[2].FastGetSolutionStepValue(POROSITY);
    const double dp2 = GetGeometry()[2].FastGetSolutionStepValue(DIAMETER);


    //
    // vel_gauss = sum( N[i]*(vel[i]-mesh_vel[i]), i=0, number_of_points) (note that the fractional step vel is used)
    ms_vel_gauss[0] =  msN[0]*(fv0[0]-w0[0]) + msN[1]*(fv1[0]-w1[0]) +  msN[2]*(fv2[0]-w2[0]);
    ms_vel_gauss[1] =  msN[0]*(fv0[1]-w0[1]) + msN[1]*(fv1[1]-w1[1]) +  msN[2]*(fv2[1]-w2[1]);

    //vel_gauss = sum( N[i]*(vel[i]-mesh_vel[i]), i=0, number_of_points) (note that the fractional step vel is used)
    ms_vel_gauss_old[0] =  msN[0]*(fv0_old[0]-w0_old[0]) + msN[1]*(fv1_old[0]-w1_old[0]) +  msN[2]*(fv2_old[0]-w2_old[0]);
    ms_vel_gauss_old[1] =  msN[0]*(fv0_old[1]-w0_old[1]) + msN[1]*(fv1_old[1]-w1_old[1]) +  msN[2]*(fv2_old[1]-w2_old[1]);


    //ms_vel_gauss = v at (n+1)/2;
    ms_vel_gauss[0] += ms_vel_gauss_old[0];
    ms_vel_gauss[0] *= 0.5;
    ms_vel_gauss[1] += ms_vel_gauss_old[1];
    ms_vel_gauss[1] *= 0.5;

    //calculating viscosity
    double nu = 0.333333333333333333333333*(nu0 + nu1 + nu2 );
    double density = 0.3333333333333333333333*(rho0 + rho1 + rho2 );

    //DIAMETER of the element
    double dp = 0.3333333333333333333333*(dp0 + dp1 + dp2);
    //POROSITY of the element: average value of the porosity
    double eps = 0.3333333333333333333333*(eps0 + eps1 + eps2 );

    //1/PERMEABILITY of the element: average value of the porosity
    double kinv = 0.0;

    //Calculate the elemental Kinv in function of the nodal K of each element.

    //Version 1: we can calculate the elemental kinv from the nodal kinv;
    //THERE IS AN ERROR: IN THE INTERPHASE ELEMENTS A WATER NODE HAS TO BE ''MORE IMPORTANT'' THAN A POROUS ONE!!!
// 		if(kinv0 != 0.0 || kinv1 != 0.0 || kinv2 != 0.0) //if it is a fluid element
// 		{	double k0 = 0.0;
// 			double k1 = 0.0;
// 			double k2 = 0.0;
// 			if(kinv0 != 0.0)
// 				k0 = 1.0/kinv0;
// 			if(kinv1 != 0.0)
// 				k1 = 1.0/kinv1;
// 			if(kinv2 != 0.0)
// 				k2 = 1.0/kinv2;
// 			kinv = 3.0/(k0 + k1 + k2 );
// 		}
//
    //Calculate kinv = 1/ k(eps_elem);
// if(rLeftHandSideMatrix.size1() != number_of_points)
// 			rLeftHandSideMatrix.resize(number_of_points,number_of_points,false);

    //Version 2:we can calculate the elemental kinv from the already calculate elemental eps;
    if( (eps0 != 1) | (eps1 != 1) | (eps2 != 1) )
        kinv = 150*(1-eps)*(1-eps)/(eps*eps*eps*dp*dp);

    //getting the BDF2 coefficients (not fixed to allow variable time step)
    //the coefficients INCLUDE the time step
    //const Vector& BDFcoeffs = rCurrentProcessInfo[BDF_COEFFICIENTS];


    //Getting delta time value for the restriction over tau.
    double Dt = rCurrentProcessInfo[DELTA_TIME];

    array_1d<double,2> BDFcoeffs = ZeroVector(2);
    BDFcoeffs[0]= 1.0 / Dt; 		//coeff for step n+1;
    BDFcoeffs[1]= -1.0 / Dt;		//coeff for step n;




    //calculating parameter tau (saved internally to each element)
    double c1 = 4.00;
    double c2 = 2.00;
    double h = sqrt(2.00*Area);

    double norm_u = ms_vel_gauss[0]*ms_vel_gauss[0] + ms_vel_gauss[1]*ms_vel_gauss[1];
    norm_u = sqrt(norm_u); //norm_u calculated at (n+1)/2;//
    double tau = 1.00 / ( c1*nu/(h*h) + c2*norm_u/h );




    // *****************************************
    //CALCULATION OF THE LHS

    //CONVECTIVE CONTRIBUTION TO THE STIFFNESS MATRIX
    noalias(ms_u_DN) =  prod(msDN_DX , ms_vel_gauss);
    noalias(rLeftHandSideMatrix) = 0.5 * outer_prod(msN,ms_u_DN)/(eps*eps);

    //CONVECTION STABILIZING CONTRIBUTION (Suu)
    noalias(rLeftHandSideMatrix) += 0.5 * tau/(eps*eps) * outer_prod(ms_u_DN,ms_u_DN);

    //VISCOUS CONTRIBUTION TO THE STIFFNESS MATRIX
    // rLeftHandSideMatrix += Laplacian * nu;
    noalias(rLeftHandSideMatrix) += 0.5 * nu/eps * prod(msDN_DX,trans(msDN_DX));

    //INERTIA CONTRIBUTION
    //  rLeftHandSideMatrix += M/Dt
    noalias(rLeftHandSideMatrix) += BDFcoeffs[0] * msMassFactors/eps;

    //DARCY linear CONTRIBUTION
    //  rLeftHandSideMatrix -= nu/permeability (using the cinematic viscosity it is already divided for density: then we are going to multiplicate for density again);
    noalias(rLeftHandSideMatrix) -= 0.5 * nu*msMassFactors*kinv;

    //DARCY non linear CONTRIBUTION (brinkmann)
    //rLeftHandSideMatrix -= 1.75*|u(n+1/2)|/[(150*k)^0.5*eps^(3/2)]
    noalias(rLeftHandSideMatrix) -= 0.5 * msMassFactors*norm_u*1.75*sqrt(kinv)/12.2474487/sqrt(eps*eps*eps);

    //multiplication by the area
    rLeftHandSideMatrix *= (Area * density);


    // *****************************************
    //CALCULATION OF THE RHS

    //external forces (component)
    double force_component = 0.3333333333333333*(fcomp0 + fcomp1 + fcomp2);

// 		KRATOS_WATCH(force_component);
// 		KRATOS_WATCH(p0old);
// 		KRATOS_WATCH(p1old);
// 		KRATOS_WATCH(p2old);

    //adding pressure gradient (integrated by parts)
    noalias(rRightHandSideVector) = (force_component )*msN;

//3PG-------------
//p_avg turn out to be p0_avg p1_avg and p2_avg
//3PG-------------

    double p_avg = msN[0]*p0old + msN[1]*p1old + msN[2]*p2old;
    p_avg /= density;

// 		KRATOS_WATCH(p_avg);

    rRightHandSideVector[0] += msDN_DX(0,ComponentIndex)*p_avg;
    rRightHandSideVector[1] += msDN_DX(1,ComponentIndex)*p_avg;
    rRightHandSideVector[2] += msDN_DX(2,ComponentIndex)*p_avg;

// 		KRATOS_WATCH(rRightHandSideVector);
    //adding the inertia terms
    // RHS += M*vhistory
    //calculating the historical velocity
    noalias(ms_temp_vec_np) = ZeroVector(3);

    for(int iii = 0; iii<3; iii++)
    {
        const array_1d<double,3>& v = (GetGeometry()[iii].FastGetSolutionStepValue(VELOCITY,1) );
        ms_temp_vec_np[iii] = BDFcoeffs[1]*v[ComponentIndex];
    }

    noalias(rRightHandSideVector) -= prod(msMassFactors,ms_temp_vec_np)/eps ;
// 		KRATOS_WATCH(prod(msMassFactors,ms_temp_vec_np)/eps);

//3PG-------------
//proj_component calculated on the 3 gauss points
//3PG-------------


    //RHS += Suy * proj[component]
    double proj_component = msN[0]*proj0[ComponentIndex]
                            + msN[1]*proj1[ComponentIndex]
                            + msN[2]*proj2[ComponentIndex];
    double proj_old_component = msN[0]*proj0_old[ComponentIndex]
                                + msN[1]*proj1_old[ComponentIndex]
                                + msN[2]*proj2_old[ComponentIndex];
    proj_component += proj_old_component;
    proj_component *= 0.5;    //proj_component calculate in t_n+1/2;
    noalias(rRightHandSideVector) += (tau*proj_component)/(eps*eps)*ms_u_DN;

    //multiplying by area
    rRightHandSideVector  *= (Area * density);


    ms_temp_vec_np[0] = fv0_old[ComponentIndex];
    ms_temp_vec_np[1] = fv1_old[ComponentIndex];
    ms_temp_vec_np[2] = fv2_old[ComponentIndex];


    //there is a part of the lhs which is already included;
    for(int iii = 0; iii<3; iii++)
    {
        ms_temp_vec_np[iii] *= BDFcoeffs[0];
    }

    noalias(rRightHandSideVector) +=  (Area * density)*prod(msMassFactors,ms_temp_vec_np)/eps ;
// 		KRATOS_WATCH((Area * density)*prod(msMassFactors,ms_temp_vec_np)/eps);

    //suubtracting the dirichlet term
    // RHS -= LHS*FracVel
    ms_temp_vec_np[0] = fv0[ComponentIndex] + fv0_old[ComponentIndex];
    ms_temp_vec_np[1] = fv1[ComponentIndex] + fv1_old[ComponentIndex];
    ms_temp_vec_np[2] = fv2[ComponentIndex] + fv2_old[ComponentIndex];

    noalias(rRightHandSideVector) -= prod(rLeftHandSideMatrix,ms_temp_vec_np);

// 		KRATOS_WATCH(prod(rLeftHandSideMatrix,ms_temp_vec_np));
//
// 		KRATOS_WATCH(fv0);
// 		KRATOS_WATCH(fv1);
// 		KRATOS_WATCH(fv2);
// 		KRATOS_WATCH(fv0_old);
// 		KRATOS_WATCH(fv1_old);
// 		KRATOS_WATCH(fv2_old);


// 		KRATOS_WATCH(rRightHandSideVector);

    KRATOS_CATCH("");
}