tutorials/incompressible/MRFSimpleFoam/axialTurbine_mixingPlane/system/fvSchemes

   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
   9 {
  10     version     2.0;
  11     format      ascii;
  12     class       dictionary;
  13     object      fvSchemes;
  14 }
  15 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
  16
  17 ddtSchemes
  18 {
  19     default steadyState;
  20 }
  21
  22 gradSchemes
  23 {
  24     default         Gauss linear;
  25     grad(p)         Gauss linear;
  26     grad(U)         Gauss linear;
  27 }
  28
  29 divSchemes
  30 {
  31     default         none;
  32     div(phi,U)      Gauss limitedLinearV 1;
  33     div(phi,k)      Gauss limitedLinear 1;
  34     div(phi,epsilon) Gauss limitedLinear 1;
  35     div((nuEff*dev(grad(U).T()))) Gauss linear;
  36 }
  37
  38 laplacianSchemes
  39 {
  40     default         none;
  41     laplacian(nuEff,U) Gauss linear corrected;
  42     laplacian((1|A(U)),p) Gauss linear corrected;
  43     laplacian(DkEff,k) Gauss linear corrected;
  44     laplacian(DepsilonEff,epsilon) Gauss linear corrected;
  45 }
  46
  47 interpolationSchemes
  48 {
  49     default         linear;
  50     interpolate(U)  linear;
  51 }
  52
  53 snGradSchemes
  54 {
  55     default         corrected;
  56 }
  57
  58 fluxRequired
  59 {
  60     default         no;
  61     p;
  62 }
  63
  64 mixingPlane
  65 {
  66     default         areaAveraging;
  67     U               areaAveraging;
  68     p               areaAveraging;
  69     k               fluxAveraging; //Transported variable
  70     epsilon         fluxAveraging; //Transported variable
  71     //NOTE: Ideally, tangential velocity components should also be
  72     //fluxAveraged, while keeping areaAveraging for normal velocity
  73     //component (to preserve perfect mass conservation)
  74 }
  75
  76 // ************************************************************************* //