overBuoyantPimpleDyMFoam.C

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/*---------------------------------------------------------------------------*\
  =========                 |
  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
   \\    /   O peration     |
    \\  /    A nd           | www.openfoam.com
     \\/     M anipulation  |
-------------------------------------------------------------------------------
    Copyright (C) 2019 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
    overBuoyantPimpleDymFoam
 
Group
    grpHeatTransferSolvers
 
Description
    Transient solver for buoyant, turbulent flow of compressible fluids for
    ventilation and heat-transfer with overset feature
 
    Turbulence is modelled using a run-time selectable compressible RAS or
    LES model.
 
\*---------------------------------------------------------------------------*/
 
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "rhoThermo.H"
#include "turbulentFluidThermoModel.H"
#include "radiationModel.H"
#include "fvOptions.H"
#include "pimpleControl.H"
#include "pressureControl.H"
 
#include "CorrectPhi.H"
#include "cellCellStencilObject.H"
#include "localMin.H"
 
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
int main(int argc, char *argv[])
{
    argList::addNote
    (
        "Transient solver for buoyant, turbulent fluid flow"
        " of compressible fluids, including radiation."
    );
 
    #include "postProcess.H"
 
    #include "addCheckCaseOptions.H"
    #include "setRootCaseLists.H"
    #include "createTime.H"
    #include "createDynamicFvMesh.H"
    #include "createDyMControls.H"
    #include "createFields.H"
    #include "createFieldRefs.H"
    #include "initContinuityErrs.H"
 
    #include "createRhoUfIfPresent.H"
    #include "createControls.H"
 
    #include "compressibleCourantNo.H"
    #include "setInitialDeltaT.H"
 
    turbulence->validate();
 
    // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
    Info<< "\nStarting time loop\n" << endl;
 
    while (runTime.run())
    {
        #include "readTimeControls.H"
 
        #include "readControls.H"
        #include "readDyMControls.H"
 
        #include "compressibleCourantNo.H"
        #include "setDeltaT.H"
 
        // Store divrhoU from the previous mesh so that it can be mapped
        // and used in correctPhi to ensure the corrected phi has the
        // same divergence
        autoPtr<volScalarField> divrhoU;
        if (correctPhi)
        {
            divrhoU.reset
            (
                new volScalarField
                (
                    "divrhoU",
                    fvc::div(fvc::absolute(phi, rho, U))
                )
            );
        }
 
 
        ++runTime;
 
        Info<< "Time = " << runTime.timeName() << nl << endl;
 
        // --- Pressure-velocity PIMPLE corrector loop
        while (pimple.loop())
        {
            if (pimple.firstIter() || moveMeshOuterCorrectors)
            {
                // Do any mesh changes
                mesh.update();
 
                if (mesh.changing())
                {
                    MRF.update();
 
                    #include "setCellMask.H"
 
                    const surfaceScalarField faceMaskOld
                    (
                        localMin<scalar>(mesh).interpolate(cellMask.oldTime())
                    );
 
                    // Zero Uf on old faceMask (H-I)
                    rhoUf() *= faceMaskOld;
 
                    //fvc::correctRhoUf(rhoUfint, rho, U, phi);
                    surfaceVectorField rhoUfint(fvc::interpolate(rho*U));
 
                    // Update Uf and phi on new C-I faces
                    rhoUf() += (1-faceMaskOld)*rhoUfint;
 
                    // Update Uf boundary
                    forAll(rhoUf().boundaryField(), patchI)
                    {
                        rhoUf().boundaryFieldRef()[patchI] =
                            rhoUfint.boundaryField()[patchI];
                    }
 
                    // Calculate absolute flux from the mapped surface velocity
                    phi = mesh.Sf() & rhoUf();
 
                    if (correctPhi)
                    {
                        #include "correctPhi.H"
                    }
 
                    // Zero phi on current H-I
                    const surfaceScalarField faceMask
                    (
                        localMin<scalar>(mesh).interpolate(cellMask)
                    );
 
                    phi *= faceMask;
                    U   *= cellMask;
 
                     // Make the fluxes relative to the mesh-motion
                    fvc::makeRelative(phi, rho, U);
                }
 
                if (checkMeshCourantNo)
                {
                    #include "meshCourantNo.H"
                }
            }
 
            if (pimple.firstIter())
            {
                #include "rhoEqn.H"
            }
 
            #include "UEqn.H"
            #include "EEqn.H"
 
            // --- Pressure corrector loop
            while (pimple.correct())
            {
                #include "pEqn.H"
            }
 
            if (pimple.turbCorr())
            {
                turbulence->correct();
            }
        }
 
        rho = thermo.rho();
 
        runTime.write();
 
        runTime.printExecutionTime(Info);
    }
 
    Info<< "End\n" << endl;
 
    return 0;
}
 
 
// ************************************************************************* //