Example #1
0
volScalarField dynOneEqEddy::ck
(
    const volSymmTensorField& D,
    const volScalarField& KK
) const
{
    const volSymmTensorField LL
    (
        simpleFilter_(dev(filter_(sqr(U())) - (sqr(filter_(U())))))
    );

    const volSymmTensorField MM
    (
        simpleFilter_(-2.0*delta()*sqrt(KK)*filter_(D))
    );

    const volScalarField ck
    (
        simpleFilter_(0.5*(LL && MM))
       /(
            simpleFilter_(magSqr(MM))
          + dimensionedScalar("small", sqr(MM.dimensions()), VSMALL)
        )
    );

    tmp<volScalarField> tfld = 0.5*(mag(ck) + ck);
    return tfld();
}
Example #2
0
volScalarField dynamicKEqn<BasicTurbulenceModel>::Ck
(
    const volSymmTensorField& D,
    const volScalarField& KK
) const
{
    const volSymmTensorField LL
    (
        simpleFilter_(dev(filter_(sqr(this->U_)) - (sqr(filter_(this->U_)))))
    );

    const volSymmTensorField MM
    (
        simpleFilter_(-2.0*this->delta()*sqrt(KK)*filter_(D))
    );

    const volScalarField Ck
    (
        simpleFilter_(0.5*(LL && MM))
       /(
            simpleFilter_(magSqr(MM))
          + dimensionedScalar("small", sqr(MM.dimensions()), VSMALL)
        )
    );

    tmp<volScalarField> tfld = 0.5*(mag(Ck) + Ck);
    return tfld();
}
void Foam::functionObjects::wallShearStress::calcShearStress
(
    const volSymmTensorField& Reff,
    volVectorField& shearStress
)
{
    shearStress.dimensions().reset(Reff.dimensions());

    forAllConstIter(labelHashSet, patchSet_, iter)
    {
        label patchi = iter.key();

        vectorField& ssp = shearStress.boundaryFieldRef()[patchi];
        const vectorField& Sfp = mesh_.Sf().boundaryField()[patchi];
        const scalarField& magSfp = mesh_.magSf().boundaryField()[patchi];
        const symmTensorField& Reffp = Reff.boundaryField()[patchi];

        ssp = (-Sfp/magSfp) & Reffp;
    }
int main(int argc, char *argv[])
{
    timeSelector::addOptions();

    #include "setRootCase.H"
    #include "createTime.H"

    instantList timeDirs = timeSelector::select0(runTime, args);

    #include "createMesh.H"
    #include "createFields.H"

    forAll(timeDirs, timeI)
    {
        runTime.setTime(timeDirs[timeI], timeI);

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

        // Cache the turbulence fields

        Info<< "\nRetrieving field k from turbulence model" << endl;
        const volScalarField k = RASModel->k();

        Info<< "\nRetrieving field epsilon from turbulence model" << endl;
        const volScalarField epsilon = RASModel->epsilon();

        Info<< "\nRetrieving field R from turbulence model" << endl;
        const volSymmTensorField R = RASModel->R();

        // Check availability of tubulence fields

        if (!IOobject("k", runTime.timeName(), mesh).headerOk())
        {
            Info<< "\nWriting turbulence field k" << endl;
            k.write();
        }
        else
        {
            Info<< "\nTurbulence k field already exists" << endl;
        }

        if (!IOobject("epsilon", runTime.timeName(), mesh).headerOk())
        {
            Info<< "\nWriting turbulence field epsilon" << endl;
            epsilon.write();
        }
        else
        {
            Info<< "\nTurbulence epsilon field already exists" << endl;
        }

        if (!IOobject("R", runTime.timeName(), mesh).headerOk())
        {
            Info<< "\nWriting turbulence field R" << endl;
            R.write();
        }
        else
        {
            Info<< "\nTurbulence R field already exists" << endl;
        }

        if (!IOobject("omega", runTime.timeName(), mesh).headerOk())
        {
            const scalar Cmu = 0.09;

            Info<< "creating omega" << endl;
            volScalarField omega
            (
                IOobject
                (
                    "omega",
                    runTime.timeName(),
                    mesh
                ),
                epsilon/(Cmu*k),
                epsilon.boundaryField().types()
            );
            Info<< "\nWriting turbulence field omega" << endl;
            omega.write();
        }
        else
        {
            Info<< "\nTurbulence omega field already exists" << endl;
        }
    }
tmp<fvVectorMatrix> surfaceShearForce::correct(volVectorField& U)
{
    // local reference to film model
    const kinematicSingleLayer& film =
        static_cast<const kinematicSingleLayer&>(owner_);

    // local references to film fields
    const volScalarField& mu = film.mu();
    const volVectorField& Uw = film.Uw();
    const volScalarField& delta = film.delta();
    const volVectorField& Up = film.UPrimary();

    // film surface linear coeff to apply to velocity
    tmp<volScalarField> tCs;

    typedef compressible::turbulenceModel turbModel;
    if (film.primaryMesh().foundObject<turbModel>("turbulenceProperties"))
    {
        // local reference to turbulence model
        const turbModel& turb =
            film.primaryMesh().lookupObject<turbModel>("turbulenceProperties");

        // calculate and store the stress on the primary region
        const volSymmTensorField primaryReff(turb.devRhoReff());

        // create stress field on film
        // - note boundary condition types (mapped)
        // - to map, the field name must be the same as the field on the
        //   primary region
        volSymmTensorField Reff
        (
            IOobject
            (
                primaryReff.name(),
                film.regionMesh().time().timeName(),
                film.regionMesh(),
                IOobject::NO_READ,
                IOobject::NO_WRITE
            ),
            film.regionMesh(),
            dimensionedSymmTensor
            (
                "zero",
                primaryReff.dimensions(),
                symmTensor::zero
            ),
            film.mappedFieldAndInternalPatchTypes<symmTensor>()
        );

        // map stress from primary region to film region
        Reff.correctBoundaryConditions();

        dimensionedScalar U0("SMALL", U.dimensions(), SMALL);
        tCs = Cf_*mag(-film.nHat() & Reff)/(mag(Up - U) + U0);
    }
    else
    {
        // laminar case - employ simple coeff-based model
        const volScalarField& rho = film.rho();
        tCs = Cf_*rho*mag(Up - U);
    }

    dimensionedScalar d0("SMALL", delta.dimensions(), SMALL);

    // linear coeffs to apply to velocity
    const volScalarField& Cs = tCs();
    volScalarField Cw("Cw", mu/(0.3333*(delta + d0)));
    Cw.min(1.0e+06);

    return
    (
       - fvm::Sp(Cs, U) + Cs*Up // surface contribution
       - fvm::Sp(Cw, U) + Cw*Uw // wall contribution
    );
}