rhoCentralFoam.C

Go to the documentation of this file.

/*---------------------------------------------------------------------------*\
  =========                 |
  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
   \\    /   O peration     |
    \\  /    A nd           | www.openfoam.com
     \\/     M anipulation  |
-------------------------------------------------------------------------------
    Copyright (C) 2011-2016 OpenFOAM Foundation
    Copyright (C) 2021-2025 OpenCFD Ltd.
-------------------------------------------------------------------------------
License
    This file is part of OpenFOAM.
 
    OpenFOAM is free software: you can redistribute it and/or modify it
    under the terms of the GNU General Public License as published by
    the Free Software Foundation, either version 3 of the License, or
    (at your option) any later version.
 
    OpenFOAM 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 General Public License
    for more details.
 
    You should have received a copy of the GNU General Public License
    along with OpenFOAM.  If not, see <http://www.gnu.org/licenses/>.
 
Application
    rhoCentralFoam
 
Group
    grpCompressibleSolvers
 
Description
    Density-based compressible flow solver based on
    central-upwind schemes of Kurganov and Tadmor with
    support for mesh-motion and topology changes.
 
\*---------------------------------------------------------------------------*/
 
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "psiThermo.H"
#include "turbulentFluidThermoModel.H"
#include "fixedRhoFvPatchScalarField.H"
#include "directionInterpolate.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"
 
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
int main(int argc, char *argv[])
{
    argList::addNote
    (
        "Density-based compressible flow solver based on"
        " central-upwind schemes of Kurganov and Tadmor with"
        " support for mesh-motion and topology changes."
    );
 
    #define NO_CONTROL
    #include "postProcess.H"
 
    #include "addCheckCaseOptions.H"
    #include "setRootCaseLists.H"
    #include "createTime.H"
    #include "createDynamicFvMesh.H"
    #include "createFields.H"
    #include "createFieldRefs.H"
    #include "createTimeControls.H"
 
    turbulence->validate();
 
    // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
    #include "readFluxScheme.H"
 
    const dimensionedScalar v_zero(dimVolume/dimTime, Zero);
 
    // Courant numbers used to adjust the time-step
    scalar CoNum = 0.0;
    scalar meanCoNum = 0.0;
    scalar minCoNum = 0.0;
 
    Info<< "\nStarting time loop\n" << endl;
 
    while (runTime.run())
    {
        #include "readTimeControls.H"
 
        if (!LTS)
        {
            #include "setDeltaT.H"
 
            ++runTime;
 
            // Do any mesh changes
            mesh.update();
        }
 
        // --- Directed interpolation of primitive fields onto faces
 
        surfaceScalarField rho_pos(interpolate(rho, pos));
        surfaceScalarField rho_neg(interpolate(rho, neg));
 
        surfaceVectorField rhoU_pos(interpolate(rhoU, pos, U.name()));
        surfaceVectorField rhoU_neg(interpolate(rhoU, neg, U.name()));
 
        volScalarField rPsi("rPsi", 1.0/psi);
        surfaceScalarField rPsi_pos(interpolate(rPsi, pos, T.name()));
        surfaceScalarField rPsi_neg(interpolate(rPsi, neg, T.name()));
 
        surfaceScalarField e_pos(interpolate(e, pos, T.name()));
        surfaceScalarField e_neg(interpolate(e, neg, T.name()));
 
        surfaceVectorField U_pos("U_pos", rhoU_pos/rho_pos);
        surfaceVectorField U_neg("U_neg", rhoU_neg/rho_neg);
 
        surfaceScalarField p_pos("p_pos", rho_pos*rPsi_pos);
        surfaceScalarField p_neg("p_neg", rho_neg*rPsi_neg);
 
        surfaceScalarField phiv_pos("phiv_pos", U_pos & mesh.Sf());
        // Note: extracted out the orientation so becomes unoriented
        phiv_pos.setOriented(false);
        surfaceScalarField phiv_neg("phiv_neg", U_neg & mesh.Sf());
        phiv_neg.setOriented(false);
 
        // Make fluxes relative to mesh-motion
        if (mesh.moving())
        {
            surfaceScalarField meshPhi(mesh.phi());
            meshPhi.setOriented(false);
            phiv_pos -= meshPhi;
            phiv_neg -= meshPhi;
        }
 
        volScalarField c("c", sqrt(thermo.Cp()/thermo.Cv()*rPsi));
        surfaceScalarField cSf_pos
        (
            "cSf_pos",
            interpolate(c, pos, T.name())*mesh.magSf()
        );
 
        surfaceScalarField cSf_neg
        (
            "cSf_neg",
            interpolate(c, neg, T.name())*mesh.magSf()
        );
 
        surfaceScalarField ap
        (
            "ap",
            max(max(phiv_pos + cSf_pos, phiv_neg + cSf_neg), v_zero)
        );
 
        surfaceScalarField am
        (
            "am",
            min(min(phiv_pos - cSf_pos, phiv_neg - cSf_neg), v_zero)
        );
 
        surfaceScalarField a_pos("a_pos", ap/(ap - am));
 
        surfaceScalarField amaxSf("amaxSf", max(mag(am), mag(ap)));
 
        surfaceScalarField aSf("aSf", am*a_pos);
 
        if (fluxScheme == "Tadmor")
        {
            aSf = -0.5*amaxSf;
            a_pos = 0.5;
        }
 
        surfaceScalarField a_neg("a_neg", 1.0 - a_pos);
 
        phiv_pos *= a_pos;
        phiv_neg *= a_neg;
 
        surfaceScalarField aphiv_pos("aphiv_pos", phiv_pos - aSf);
        surfaceScalarField aphiv_neg("aphiv_neg", phiv_neg + aSf);
 
        // Reuse amaxSf for the maximum positive and negative fluxes
        // estimated by the central scheme
        amaxSf = max(mag(aphiv_pos), mag(aphiv_neg));
 
        if (LTS)
        {
            #include "setRDeltaT.H"
 
            ++runTime;
        }
 
        #include "centralCourantNo.H"
 
        Info<< "Time = " << runTime.timeName() << nl << endl;
 
        phi = aphiv_pos*rho_pos + aphiv_neg*rho_neg;
 
        surfaceVectorField phiU(aphiv_pos*rhoU_pos + aphiv_neg*rhoU_neg);
        // Note: reassembled orientation from the pos and neg parts so becomes
        // oriented
        phiU.setOriented(true);
 
        surfaceVectorField phiUp(phiU + (a_pos*p_pos + a_neg*p_neg)*mesh.Sf());
 
        surfaceScalarField phiEp
        (
            "phiEp",
            aphiv_pos*(rho_pos*(e_pos + 0.5*magSqr(U_pos)) + p_pos)
          + aphiv_neg*(rho_neg*(e_neg + 0.5*magSqr(U_neg)) + p_neg)
          + aSf*p_pos - aSf*p_neg
        );
 
        // Make flux for pressure-work absolute
        if (mesh.moving())
        {
            surfaceScalarField meshPhi(mesh.phi());
            meshPhi.setOriented(false);
            phiEp += meshPhi*(a_pos*p_pos + a_neg*p_neg);
        }
 
        volScalarField muEff("muEff", turbulence->muEff());
        volTensorField tauMC("tauMC", muEff*dev2(Foam::T(fvc::grad(U))));
 
        // --- Solve density
        solve(fvm::ddt(rho) + fvc::div(phi));
 
        // --- Solve momentum
        solve(fvm::ddt(rhoU) + fvc::div(phiUp));
 
        U.ref() =
            rhoU()
           /rho();
        U.correctBoundaryConditions();
        rhoU.boundaryFieldRef() == rho.boundaryField()*U.boundaryField();
 
        if (!inviscid)
        {
            solve
            (
                fvm::ddt(rho, U) - fvc::ddt(rho, U)
              - fvm::laplacian(muEff, U)
              - fvc::div(tauMC)
            );
            rhoU = rho*U;
        }
 
        // --- Solve energy
        surfaceScalarField sigmaDotU
        (
            "sigmaDotU",
            (
                fvc::interpolate(muEff)*mesh.magSf()*fvc::snGrad(U)
              + fvc::dotInterpolate(mesh.Sf(), tauMC)
            )
          & (a_pos*U_pos + a_neg*U_neg)
        );
 
        solve
        (
            fvm::ddt(rhoE)
          + fvc::div(phiEp)
          - fvc::div(sigmaDotU)
        );
 
        e = rhoE/rho - 0.5*magSqr(U);
        e.correctBoundaryConditions();
        thermo.correct();
        rhoE.boundaryFieldRef() ==
            rho.boundaryField()*
            (
                e.boundaryField() + 0.5*magSqr(U.boundaryField())
            );
 
        if (!inviscid)
        {
            solve
            (
                fvm::ddt(rho, e) - fvc::ddt(rho, e)
              - fvm::laplacian(turbulence->alphaEff(), e)
            );
            thermo.correct();
            rhoE = rho*(e + 0.5*magSqr(U));
        }
 
        p.ref() =
            rho()
           /psi();
        p.correctBoundaryConditions();
        rho.boundaryFieldRef() == psi.boundaryField()*p.boundaryField();
 
        turbulence->correct();
 
        runTime.write();
 
        runTime.printExecutionTime(Info);
    }
 
    Info<< "End\n" << endl;
 
    return 0;
}
 
// ************************************************************************* //