76 lines
2 KiB
C++
76 lines
2 KiB
C++
/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | foam-extend: Open Source CFD |
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| \\ / O peration | Version: 3.2 |
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| \\ / A nd | Web: http://www.foam-extend.org |
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| \\/ M anipulation | |
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\*---------------------------------------------------------------------------*/
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FoamFile
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{
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version 2.0;
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format ascii;
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class dictionary;
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object fvSchemes;
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}
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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ddtSchemes
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{
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default steadyState;
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}
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gradSchemes
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{
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default Gauss linear;
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grad(p) Gauss linear;
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grad(U) Gauss linear;
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}
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divSchemes
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{
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default none;
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div(phi,U) Gauss limitedLinearV 1;
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div(phi,k) Gauss limitedLinear 1;
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div(phi,epsilon) Gauss limitedLinear 1;
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div((nuEff*dev(T(grad(U))))) Gauss linear;
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}
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laplacianSchemes
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{
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default none;
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laplacian(nuEff,U) Gauss linear corrected;
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laplacian((1|A(U)),p) Gauss linear corrected;
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laplacian(DkEff,k) Gauss linear corrected;
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laplacian(DepsilonEff,epsilon) Gauss linear corrected;
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}
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interpolationSchemes
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{
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default linear;
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interpolate(U) linear;
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}
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snGradSchemes
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{
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default corrected;
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}
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fluxRequired
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{
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default no;
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p;
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}
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mixingPlane
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{
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default areaAveraging;
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U areaAveraging;
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p areaAveraging;
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k fluxAveraging; //Transported variable
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epsilon fluxAveraging; //Transported variable
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//NOTE: Ideally, tangential velocity components should also be
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//fluxAveraged, while keeping areaAveraging for normal velocity
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//component (to preserve perfect mass conservation)
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}
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// ************************************************************************* //
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