tutorials/incompressible/simpleFoam/airFoil2D/system/fvSolution

   1 /*--------------------------------*- C++ -*----------------------------------*\
   2 | =========                 |                                                 |
   3 | \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
   4 |  \\    /   O peration     | Version:  1.6                                   |
   5 |   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
   6 |    \\/     M anipulation  |                                                 |
   7 \*---------------------------------------------------------------------------*/
   8 FoamFile
   9 {
  10     version     2.0;
  11     format      ascii;
  12     class       dictionary;
  13     location    "system";
  14     object      fvSolution;
  15 }
  16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
  17
  18 solvers
  19 {
  20     p
  21     {
  22         solver          GAMG;
  23         tolerance       1e-06;
  24         relTol          0.1;
  25         smoother        GaussSeidel;
  26         nPreSweeps      0;
  27         nPostSweeps     2;
  28         cacheAgglomeration true;
  29         nCellsInCoarsestLevel 10;
  30         agglomerator    faceAreaPair;
  31         mergeLevels     1;
  32     }
  33
  34     U
  35     {
  36         solver          smoothSolver;
  37         smoother        GaussSeidel;
  38         nSweeps         2;
  39         tolerance       1e-08;
  40         relTol          0.1;
  41     }
  42
  43     nuTilda
  44     {
  45         solver          smoothSolver;
  46         smoother        GaussSeidel;
  47         nSweeps         2;
  48         tolerance       1e-08;
  49         relTol          0.1;
  50     }
  51 }
  52
  53 SIMPLE
  54 {
  55     nNonOrthogonalCorrectors 0;
  56     pRefCell        0;
  57     pRefValue       0;
  58 }
  59
  60 relaxationFactors
  61 {
  62     default         0;
  63     p               0.3;
  64     U               0.7;
  65     nuTilda         0.7;
  66 }
  67
  68
  69 // ************************************************************************* //