foam-extend4.1-coherent-io/tutorials/compressible/sonicFoam/ras/nacaAirfoil/system/fvSchemes

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM Extend Project: Open Source CFD        |
|  \\    /   O peration     | Version:  1.6-ext                               |
|   \\  /    A nd           | Web:      www.extend-project.de                 |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    location    "system";
    object      fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

ddtSchemes
{
    default         Euler;
}

gradSchemes
{
    default         Gauss linear;
}

divSchemes
{
    default         none;
    div(phi,U)      Gauss limitedLinearV 1;
    div(phi,k)      Gauss upwind;
    div(phi,epsilon) Gauss upwind;
    div(phi,R)      Gauss upwind;
    div(R)          Gauss linear;
    div(phid,p)     Gauss limitedLinear 1;
    div(phiU,p)     Gauss limitedLinear 1;
    div(phi,e)      Gauss limitedLinear 1;
    div((muEff*dev2(grad(U).T()))) Gauss linear;
}

laplacianSchemes
{
    default         none;
    laplacian(muEff,U) Gauss linear limited 0.5;
    laplacian(DkEff,k) Gauss linear limited 0.5;
    laplacian(DREff,R) Gauss linear limited 0.5;
    laplacian(DepsilonEff,epsilon) Gauss linear limited 0.5;
    laplacian((rho*(1|A(U))),p) Gauss linear limited 0.5;
    laplacian(alphaEff,e) Gauss linear limited 0.5;
}

interpolationSchemes
{
    default         linear;
}

snGradSchemes
{
    default         corrected;
}

fluxRequired
{
    default         no;
    p;
}

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