tutorials/incompressible/MRFSimpleFoam/axialTurbine_mixingPlane/system/fvSolution

   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      fvSolution;
  14 }
  15 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
  16
  17 solvers
  18 {
  19     // For meshes with
  20     // disparities in angle span across the mixingPlane interface, a
  21     // solver for asymmetrical matrices is required, like BiCGStab. When
  22     // in doubt, just select a solver for asymmetrical matrices for p.
  23     p
  24     {
  25         solver           BiCGStab;
  26         preconditioner   DILU;
  27         tolerance        1e-08;
  28         relTol           0.05;
  29     };
  30     U
  31     {
  32         solver           BiCGStab;
  33         preconditioner   DILU;
  34         tolerance        1e-07;
  35         relTol           0.1;
  36     };
  37     k
  38     {
  39         solver           BiCGStab;
  40         preconditioner   DILU;
  41         tolerance        1e-07;
  42         relTol           0.1;
  43     };
  44     epsilon
  45     {
  46         solver           BiCGStab;
  47         preconditioner   DILU;
  48         tolerance        1e-07;
  49         relTol           0.1;
  50     };
  51 }
  52
  53 SIMPLE
  54 {
  55     nNonOrthogonalCorrectors 0;
  56 }
  57
  58 relaxationFactors
  59 {
  60     p               0.3;
  61     U               0.7;
  62     k               0.7;
  63     epsilon         0.7;
  64 }
  65
  66 // ************************************************************************* //