MPPICInterFoam.C

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/*---------------------------------------------------------------------------*\
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    Copyright (C) 2016-2020 OpenCFD Ltd.
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License
    This file is part of OpenFOAM.

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Application
    MPPICInterFoam

Description
    Solver for two incompressible, isothermal immiscible fluids using a VOF
    (volume of fluid) phase-fraction based interface capturing approach.
    The momentum and other fluid properties are of the "mixture" and a single
    momentum equation is solved.

    It includes MRF and an MPPIC cloud.

    Turbulence modelling is generic, i.e. laminar, RAS or LES may be selected.

\*---------------------------------------------------------------------------*/

#include "fvCFD.H"
#include "CMULES.H"
#include "EulerDdtScheme.H"
#include "localEulerDdtScheme.H"
#include "CrankNicolsonDdtScheme.H"
#include "subCycle.H"

#include "immiscibleIncompressibleTwoPhaseMixture.H"
#include "PhaseCompressibleTurbulenceModel.H"
#include "pimpleControl.H"
#include "fvOptions.H"
#include "CorrectPhi.H"
#include "fvcSmooth.H"

#include "basicKinematicCloud.H"

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

int main(int argc, char *argv[])
{
    argList::addNote
    (
        "Solver for two incompressible, isothermal immiscible fluids using"
        " VOF phase-fraction based interface capturing.\n"
        "Includes MRF and an MPPIC cloud."
    );

    #include "postProcess.H"

    #include "addCheckCaseOptions.H"
    #include "setRootCaseLists.H"
    #include "createTime.H"
    #include "createMesh.H"
    #include "createControl.H"
    #include "createTimeControls.H"
    #include "initContinuityErrs.H"
    #include "createFields.H"
    #include "createAlphaFluxes.H"
    #include "createFvOptions.H"
    #include "correctPhi.H"

    turbulence->validate();

    if (!LTS)
    {
        #include "readTimeControls.H"
        #include "CourantNo.H"
        #include "setInitialDeltaT.H"
    }

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

    Info<< "\nStarting time loop\n" << endl;

    while (runTime.run())
    {
        #include "readTimeControls.H"

        if (LTS)
        {
            #include "setRDeltaT.H"
        }
        else
        {
            #include "CourantNo.H"
            #include "alphaCourantNo.H"
            #include "setDeltaT.H"
        }

        ++runTime;

        Info<< "Time = " << runTime.timeName() << nl << endl;

        Info<< "Evolving " << kinematicCloud.name() << endl;

        kinematicCloud.evolve();

        // Update continuous phase volume fraction field
        alphac = max(1.0 - kinematicCloud.theta(), alphacMin);
        alphac.correctBoundaryConditions();

         Info<< "Continuous phase-1 volume fraction = "
            << alphac.weightedAverage(mesh.Vsc()).value()
            << "  Min(alphac) = " << min(alphac).value()
            << "  Max(alphac) = " << max(alphac).value()
            << endl;

        alphacf = fvc::interpolate(alphac);
        alphaRhoPhic = alphacf*rhoPhi;
        alphaPhic = alphacf*phi;
        alphacRho = alphac*rho;

        fvVectorMatrix cloudSU(kinematicCloud.SU(U));
        volVectorField cloudVolSUSu
        (
            IOobject
            (
                "cloudVolSUSu",
                runTime.timeName(),
                mesh
            ),
            mesh,
            dimensionedVector(cloudSU.dimensions()/dimVolume, Zero),
            fvPatchFieldBase::zeroGradientType()
        );

        cloudVolSUSu.primitiveFieldRef() = -cloudSU.source()/mesh.V();
        cloudVolSUSu.correctBoundaryConditions();

        cloudSU.source() = vector::zero;

        // --- Pressure-velocity PIMPLE corrector loop
        while (pimple.loop())
        {
            #include "alphaControls.H"
            #include "alphaEqnSubCycle.H"

            mixture.correct();

            #include "UEqn.H"

            // --- Pressure corrector loop
            while (pimple.correct())
            {
                #include "pEqn.H"
            }

            if (pimple.turbCorr())
            {
                turbulence->correct();
            }
        }

        runTime.write();

        runTime.printExecutionTime(Info);
    }

    Info<< "End\n" << endl;

    return 0;
}


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