RCROutflow.cpp

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///////////////////////////////////////////////////////////////////////////////
//
// File RCROutflow.cpp
//
// For more information, please see: http://www.nektar.info
//
// The MIT License
//
// Copyright (c) 2006 Division of Applied Mathematics, Brown University (USA),
// Department of Aeronautics, Imperial College London (UK), and Scientific
// Computing and Imaging Institute, University of Utah (USA).
//
// Permission is hereby granted, free of charge, to any person obtaining a
// copy of this software and associated documentation files (the "Software"),
// to deal in the Software without restriction, including without limitation
// the rights to use, copy, modify, merge, publish, distribute, sublicense,
// and/or sell copies of the Software, and to permit persons to whom the
// Software is furnished to do so, subject to the following conditions:
//
// The above copyright notice and this permission notice shall be included
// in all copies or substantial portions of the Software.
//
// THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS
// OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY,
// FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL
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// DEALINGS IN THE SOFTWARE.
//
// Description: 
//
///////////////////////////////////////////////////////////////////////////////

#include <PulseWaveSolver/EquationSystems/RCROutflow.h>
#include <SpatialDomains/MeshGraph.h>

using namespace std;

namespace Nektar
{

    std::string RCROutflow::className
    = GetBoundaryFactory().RegisterCreatorFunction(
        "RCR-terminal",
        RCROutflow::create,
        "RCR  outflow boundary condition");

    /**
     *
     */
    RCROutflow::RCROutflow(Array<OneD, MultiRegions::ExpListSharedPtr> pVessel, 
                           const LibUtilities::SessionReaderSharedPtr pSession,
                           PulseWavePressureAreaSharedPtr pressureArea)
        : PulseWaveBoundary(pVessel,pSession,pressureArea)
    {
        m_session->LoadParameter("TimeStep", m_timestep);
    }

    /**
     *
     */
    RCROutflow::~RCROutflow()
    {

    }

    void RCROutflow::v_DoBoundary(
        const Array<OneD,const Array<OneD, NekDouble> > &inarray,
        Array<OneD, Array<OneD, NekDouble> > &A_0,
        Array<OneD, Array<OneD, NekDouble> > &beta,
        const NekDouble time,
        int omega,int offset,int n)
    { 
    NekDouble A_r, u_r;
    NekDouble A_u, u_u;
        NekDouble A_l, u_l, c_0;

        Array<OneD, MultiRegions::ExpListSharedPtr> vessel(2);

        vessel[0] = m_vessels[2*omega];
        vessel[1] = m_vessels[2*omega+1];

        /* Find the terminal RCR boundary condition and calculates
           the updated velocity and area as well as the updated
           boundary conditions */

        NekDouble RT=((vessel[0]->GetBndCondExpansions())[n])->GetCoeffs()[0];
        NekDouble C=((vessel[1]->GetBndCondExpansions())[n])->GetCoeffs()[0];

        m_session->LoadParameter("pout", m_pout);

        NekDouble R1;
        NekDouble R2;
        NekDouble pout = m_pout;

        NekDouble rho = m_rho;
        int nq = vessel[0]->GetTotPoints(); 
                        
        A_l = inarray[0][offset+nq-1];
        u_l = inarray[1][offset+nq-1];

        // Goes through the first resistance Calculate c_0
        c_0 = sqrt(beta[omega][nq-1]/(2*m_rho))*sqrt(sqrt(A_0[omega][nq-1]));           
                        
        // Calculate R1 and R2, R1 being calculated so as
        // to eliminate reflections in the vessel
        R1 = rho*c_0/A_0[omega][nq-1];
        R2 = RT-R1;

        // Call the R RiemannSolver
        R_RiemannSolver(R1,A_l,u_l,A_0[omega][nq-1],beta[omega][nq-1],m_pc,A_u,u_u);
        A_r = A_l;
        u_r = 2*u_u-u_l;

        // Goes through the CR system, it consists in
        // updating the pressure pc
        m_pc = m_pc + m_timestep/C*(A_u*u_u-(m_pc-pout)/R2);

        // Store the updated values in the boundary condition
        (vessel[0]->UpdateBndCondExpansion(n))->UpdatePhys()[0] = A_r;
        (vessel[1]->UpdateBndCondExpansion(n))->UpdatePhys()[0] = u_r;
    }

    void RCROutflow::R_RiemannSolver(NekDouble R,NekDouble A_l,NekDouble u_l,NekDouble A_0, 
                                               NekDouble beta, NekDouble pout,
                                               NekDouble &A_u,NekDouble &u_u)
   {        
        NekDouble W1 = 0.0;
        NekDouble c_l = 0.0;
        NekDouble pext = m_pext;
        NekDouble A_calc = 0.0;
        NekDouble fa = 0.0;
        NekDouble dfa = 0.0;
        NekDouble delta_A_calc = 0.0;
        NekDouble rho = m_rho;
        
        int proceed = 1;
        int iter = 0;
        int MAX_ITER = 200;
        
        // Tolerances for the algorithm
        NekDouble Tol = 1.0e-10;
        
        // Calculate the wave speed
        c_l = sqrt(beta/(2*rho))*sqrt(sqrt(A_l));
    
        // Riemann invariant \f$W_1(Al,ul)\f$
        W1 = u_l + 4*c_l;
        
        // Newton Iteration (Area only)
        A_calc = A_l;
        while ((proceed) && (iter < MAX_ITER))
        {   
            iter =iter+1;
        
            fa = R*W1*A_calc-4*R*sqrt(beta/(2*rho))*A_calc*sqrt(sqrt(A_calc))-pext-beta*(sqrt(A_calc)-sqrt(A_0))+pout;
            dfa = R*W1-5*R*sqrt(beta/(2*rho))*sqrt(sqrt(A_calc))-beta/(2*sqrt(A_calc));
            delta_A_calc = fa/dfa;
            A_calc = A_calc - delta_A_calc;
            
            if (sqrt(delta_A_calc*delta_A_calc) < Tol)
                proceed = 0;
        }
        
    // Obtain u_u and A_u
    //u_u = W1 - 4*sqrt(beta/(2*rho))*(sqrt(sqrt(A_calc))); 
        u_u=(pext+beta*(sqrt(A_calc)-sqrt(A_0))-pout)/(R*A_calc);
        A_u = A_calc;
    }




}