tutorials/multiphase/cavitatingFoam/ras/throttle/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              Euler;
  20 }
  21
  22 interpolationSchemes
  23 {
  24     default              linear;
  25 }
  26
  27 divSchemes
  28 {
  29     default              none;
  30     div(phiv,rho)        Gauss limitedLinear 0.2;
  31     div(phi,U)           Gauss limitedLinearV 0.2;
  32     div(phiv,omega)      Gauss upwind;
  33     div(phiv,k)          Gauss upwind;
  34 }
  35
  36 gradSchemes
  37 {
  38     default              Gauss linear;
  39 }
  40
  41 laplacianSchemes
  42 {
  43     default none;
  44
  45     laplacian(nuf,rhoU)  Gauss linear corrected;
  46     laplacian(muEff,U)  Gauss linear corrected;
  47     laplacian(rrhoUAf,p) Gauss linear corrected;
  48     laplacian(rUAf,p)    Gauss linear corrected;
  49     laplacian(DomegaEff,omega) Gauss linear corrected;
  50     laplacian(DkEff,k)   Gauss linear corrected;
  51
  52     laplacian(1,p)       Gauss linear corrected;
  53 }
  54
  55 snGradSchemes
  56 {
  57     default         none;
  58     snGrad(p)       corrected;
  59 }
  60
  61 fluxRequired
  62 {
  63     default        none;
  64     p;
  65     rho;
  66 }
  67
  68 // ************************************************************************* //