foam-extend4.1-coherent-io/tutorials/compressible/steadyUniversalMRFFoam/axialTurbineGgiJump/system/fvSchemes

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | foam-extend: Open Source CFD                    |
|  \\    /   O peration     | Version:     4.1                                |
|   \\  /    A nd           | Web:         http://www.foam-extend.org         |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/

FoamFile
{
    version         2.0;
    format          ascii;
    class           dictionary;
    object          fvSchemes;
}

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

ddtSchemes
{
    default           steadyState;

//    ddt(rho,U)     steadyInertial phi rho 0.25;
    ddt(rho,h)        steadyState;
    ddt(rho,i)        steadyState;
//     ddt(rho,h)      steadyInertial phi rho 0.25;
    ddt(psi,p)        steadyInertial phi rho 1;
//     ddt(psi,p)        steadyState;

    ddt(rho,k)        steadyState;
    ddt(rho,epsilon)  steadyState;

    U              steadyState;
    T              steadyState;
    p              steadyState;
}
gradSchemes
{
    default           Gauss linear;
}

divSchemes
{
    default           none;
    div(phi,U)        Gauss upwind;
    div(phi,h)        Gauss upwind;
    div(phi,i)        Gauss upwind;
    div(phid,p)       Gauss upwind;

    div(phi,k)        Gauss upwind;
    div(phi,epsilon)  Gauss upwind;


    div((muEff*dev2(T(grad(U))))) Gauss linear;
    div((nuEff*dev(T(grad(U)))))  Gauss linear;
    div(U,p)    Gauss upwind;

}

laplacianSchemes
{
    default           Gauss linear limited 0.5;
}

interpolationSchemes
{
    default           linear;
}

snGradSchemes
{
    default           limited 0.5;
}

mixingPlane
{
    default  areaAveraging;
    U        areaAveraging;
    k        fluxAveraging;
    omega    areaAveraging;
}

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