108 lines
2.1 KiB
Text
108 lines
2.1 KiB
Text
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/*--------------------------------*- C++ -*----------------------------------*\
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| ========= | |
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| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
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| \\ / O peration | Version: 1.2 |
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| \\ / A nd | Web: http://www.openfoam.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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// ddt(rho,U) steadyInertial phi rho 0.25;
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ddt(rho,h) steadyState;
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ddt(rho,i) steadyState;
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// ddt(rho,h) steadyInertial phi rho 0.25;
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ddt(psi,p) steadyInertial phi rho 1;
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// ddt(psi,p) steadyState;
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ddt(rho,k) steadyState;
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ddt(rho,epsilon) steadyState;
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U steadyState;
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T steadyState;
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p 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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}
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divSchemes
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{
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default none;
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div(phi,U) Gauss upwind;
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div(phi,h) Gauss upwind;
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div(phi,i) Gauss upwind;
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div(phid,p) Gauss upwind;
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div(phi,k) Gauss upwind;
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div(phi,epsilon) Gauss upwind;
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div((muEff*dev2(T(grad(U))))) Gauss linear;
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div((nuEff*dev(T(grad(U))))) Gauss linear;
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div(U,p) Gauss upwind;
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}
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laplacianSchemes
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{
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default Gauss linear limited 0.5;
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}
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interpolationSchemes
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{
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default linear;
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}
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snGradSchemes
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{
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default limited 0.5;
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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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k fluxAveraging;
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omega areaAveraging;
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}
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// ************************************************************************* //
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