CompressibleSteadyNS.H

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/*---------------------------------------------------------------------------*\
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 * In real Time Highly Advanced Computational Applications for Finite Volumes
 * Copyright (C) 2017 by the ITHACA-FV authors
-------------------------------------------------------------------------------
License
    This file is part of ITHACA-FV
    ITHACA-FV is free software: you can redistribute it and/or modify
    it under the terms of the GNU Lesser General Public License as published by
    the Free Software Foundation, either version 3 of the License, or
    (at your option) any later version.
    ITHACA-FV is distributed in the hope that it will be useful,
    but WITHOUT ANY WARRANTY; without even the implied warranty of
    MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
    GNU Lesser General Public License for more details.
    You should have received a copy of the GNU Lesser General Public License
    along with ITHACA-FV. If not, see <http://www.gnu.org/licenses/>.
Class
    steadyNS
Description
    Reduction class for a Stationary Navier-Stokes problem.
SourceFiles
    steadyNS.C
\*---------------------------------------------------------------------------*/

 
#ifndef CompressibleSteadyNS_H
#define CompressibleSteadyNS_H
#include "fvCFD.H"
#include "fluidThermo.H"
#include "turbulentFluidThermoModel.H"
#include "simpleControl.H"
#include "pressureControl.H"
#include "fvOptions.H"
#include "steadyNS.H"
#include "SteadyNSTurb.H"
#include "SteadyNSSimple.H"
#include "reductionProblem.H"
#include "ITHACAstream.H"
#include "ITHACAparameters.H"
#include "ITHACAforces.H"
#include "volFields.H"
#include <iostream>
 
 
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
/*---------------------------------------------------------------------------*\
                        Class SteadyNS Declaration
\*---------------------------------------------------------------------------*/


class CompressibleSteadyNS: public SteadyNSTurb
{
    public:
        // Constructors
        CompressibleSteadyNS();

        CompressibleSteadyNS(int argc, char* argv[]);
        ~CompressibleSteadyNS() {};
 
        // Functions
 
        //--------------------------------------------------------------------------
        //void truthSolve(List<scalar> mu_now);
        void truthSolve(word folder);
 
        // Momuntum equation terms
        fvVectorMatrix getUmatrix(volVectorField& U);//, Vector<double>& uresidual_v);
        fvVectorMatrix getNLTerm(volVectorField& U);
        fvVectorMatrix getViscTerm(volVectorField& U);
        volVectorField getGradP(volScalarField& p);
 
        // Energy equation terms
        fvScalarMatrix getEmatrix(volVectorField& U,
                                  volScalarField& p);//, scalar& eresidual);
        fvScalarMatrix getFluxTerm();
        volScalarField getKinEnTerm(volVectorField& U, volScalarField& p);
        fvScalarMatrix getDiffTerm();
 
        // Pressure equation terms
        fvScalarMatrix getPmatrix(fvVectorMatrix& Ueqn, volVectorField& U,
                                  volScalarField& p);
        surfaceScalarField getPhiHbyA(fvVectorMatrix& Ueqn, volVectorField& U,
                                      volScalarField& p);
        volScalarField getDivPhiHbyA(fvVectorMatrix& Ueqn, volVectorField& U,
                                     volScalarField& p);
        surfaceScalarField getRhorAUf(fvVectorMatrix& Ueqn);
        fvScalarMatrix getPoissonTerm(fvVectorMatrix& Ueqn, volScalarField& p);
 
        //--------------------------------------------------------------------------
        void changeViscosity(double mu_new);
 
        //--------------------------------------------------------------------------
        void restart();
 
        autoPtr<fluidThermo> pThermo;
 
        autoPtr<volScalarField> _rho;
 
        autoPtr<volScalarField> _p;
 
        autoPtr<pressureControl> _pressureControl;
 
        autoPtr<compressible::turbulenceModel> turbulence;
 
        autoPtr<dimensionedScalar> _initialMass;
 
        autoPtr<volScalarField> _psi;
 
        autoPtr<volScalarField> _E;


        autoPtr<volScalarField> _p0;

        autoPtr<volScalarField> _E0;

        autoPtr<volVectorField> _U0;

        autoPtr<volScalarField> _rho0;

        autoPtr<surfaceScalarField> _phi0;
 

        PtrList<volScalarField> Efield;

        volScalarModes Emodes;
 
        autoPtr<fvVectorMatrix> Ueqn_global;
 
        autoPtr<fvScalarMatrix> Peqn_global;
 
        autoPtr<fvScalarMatrix> Eeqn_global;
 
        autoPtr<surfaceScalarField> phiHbyA;
 
        autoPtr<surfaceScalarField> rhorAUf;
 
        autoPtr<volVectorField> HbyA;

        scalar tolerance;

        scalar maxIter;

        label middleStep;
        //label middleStepInit;

        bool middleExport;
 
 
 
};
 
#endif