dnsFoam.C

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/*---------------------------------------------------------------------------*\
  =========                 |
  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
   \\    /   O peration     |
    \\  /    A nd           | www.openfoam.com
     \\/     M anipulation  |
-------------------------------------------------------------------------------
    Copyright (C) 2011-2016 OpenFOAM Foundation
-------------------------------------------------------------------------------
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
    dnsFoam
 
Group
    grpDNSSolvers
 
Description
    Direct numerical simulation solver for boxes of isotropic turbulence.
 
\*---------------------------------------------------------------------------*/
 
#include "fvCFD.H"
#include "Kmesh.H"
#include "UOprocess.H"
#include "fft.H"
#include "calcEk.H"
#include "graph.H"
#include "pisoControl.H"
 
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
int main(int argc, char *argv[])
{
    argList::addNote
    (
        "Direct numerical simulation for boxes of isotropic turbulence."
    );
 
    #include "postProcess.H"
 
    #include "setRootCaseLists.H"
    #include "createTime.H"
    #include "createMeshNoClear.H"
    #include "createControl.H"
    #include "createFields.H"
    #include "initContinuityErrs.H"
 
    // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
 
    label ntot = 1;
    forAll(K.nn(), idim)
    {
        ntot *= K.nn()[idim];
    }
    const scalar recRootN = 1.0/Foam::sqrt(scalar(ntot));
 
    Info<< nl << "Starting time loop" << endl;
 
    while (runTime.loop())
    {
        Info<< "Time = " << runTime.timeName() << nl << endl;
 
        force.primitiveFieldRef() = ReImSum
        (
            fft::reverseTransform
            (
                K/(mag(K) + 1.0e-6) ^ forceGen.newField(), K.nn()
            )*recRootN
        );
 
        #include "globalProperties.H"
 
        fvVectorMatrix UEqn
        (
            fvm::ddt(U)
          + fvm::div(phi, U)
          - fvm::laplacian(nu, U)
         ==
            force
        );
 
        solve(UEqn == -fvc::grad(p));
 
 
        // --- PISO loop
        while (piso.correct())
        {
            volScalarField rAU(1.0/UEqn.A());
            surfaceScalarField rAUf("rAUf", fvc::interpolate(rAU));
            volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
            surfaceScalarField phiHbyA
            (
                "phiHbyA",
                fvc::flux(HbyA)
              + rAUf*fvc::ddtCorr(U, phi)
            );
 
            // Update the pressure BCs to ensure flux consistency
            constrainPressure(p, U, phiHbyA, rAUf);
 
            fvScalarMatrix pEqn
            (
                fvm::laplacian(rAUf, p) == fvc::div(phiHbyA)
            );
 
            pEqn.solve(mesh.solver(p.select(piso.finalInnerIter())));
 
            phi = phiHbyA - pEqn.flux();
 
            #include "continuityErrs.H"
 
            U = HbyA - rAU*fvc::grad(p);
            U.correctBoundaryConditions();
        }
 
        runTime.write();
 
        if (runTime.writeTime())
        {
            calcEk(U, K).write
            (
                runTime.path()/"graphs"/runTime.timeName(),
                "Ek",
                runTime.graphFormat()
            );
        }
 
        runTime.printExecutionTime(Info);
    }
 
    Info<< "End\n" << endl;
 
    return 0;
}
 
 
// ************************************************************************* //