/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 1.2 | | \\ / A nd | Web: http://www.openfoam.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; } // ************************************************************************* //