Removed unnecessary return statement
[foam-extend-3.2.git] / tutorials / compressible / steadyCompressibleMRFFoam / simpleRotorStator / system / fvSchemes
blob1bb70c9eea9f67e0728111ad767aa2eb6ca7107d
1 /*--------------------------------*- C++ -*----------------------------------*\
2 | =========                 |                                                 |
3 | \\      /  F ield         | foam-extend: Open Source CFD                    |
4 |  \\    /   O peration     | Version:     3.2                                |
5 |   \\  /    A nd           | Web:         http://www.foam-extend.org         |
6 |    \\/     M anipulation  |                                                 |
7 \*---------------------------------------------------------------------------*/
8 FoamFile
10     version     2.0;
11     format      ascii;
12     class       dictionary;
13     object      fvSchemes;
15 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
17 ddtSchemes
19     default         none;
21     ddt(rho,U)      steadyState;
22     ddt(rho,i)      steadyState;
23     ddt(psi,p)      steadyInertial phi rho 0.25;
25     ddt(rho,k)        steadyState;
26     ddt(rho,epsilon)  steadyState;
28     U               steadyState;
29     T               steadyState;
30     p               steadyState;
33 gradSchemes
35     default         Gauss linear;
38 divSchemes
40     default          none;
41     div(phi,U)       Gauss upwind;
42     div(phi,i)       Gauss upwind;
43     div(phid,p)      Gauss upwind;
45     div(phi,k)       Gauss upwind;
46     div(phi,epsilon) Gauss upwind;
47     div((muEff*dev2(grad(U).T()))) Gauss linear;
49     div(U,p)       Gauss linear;
52 laplacianSchemes
54     default         Gauss linear corrected;
57 interpolationSchemes
59     default         linear;
62 snGradSchemes
64     default         corrected;
67 fluxRequired
69     default         no;
70     p;
73 // ************************************************************************* //