tutorials/compressible/sonicFoam/ras/nacaAirfoil/system/controlDict

   1 /*--------------------------------*- C++ -*----------------------------------*\
   2 | =========                 |                                                 |
   3 | \\      /  F ield         | foam-extend: Open Source CFD                    |
   4 |  \\    /   O peration     | Version:     3.0                                |
   5 |   \\  /    A nd           | Web:         http://www.extend-project.de       |
   6 |    \\/     M anipulation  |                                                 |
   7 \*---------------------------------------------------------------------------*/
   8 FoamFile
   9 {
  10     version     2.0;
  11     format      ascii;
  12     class       dictionary;
  13     location    "system";
  14     object      controlDict;
  15 }
  16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
  17
  18 application     sonicFoam;
  19
  20 startFrom       latestTime;
  21
  22 startTime       0;
  23
  24 stopAt          endTime;
  25
  26 endTime         0.01;
  27
  28 deltaT          4e-08;
  29
  30 writeControl    runTime;
  31
  32 writeInterval   2e-04;
  33
  34 purgeWrite      0;
  35
  36 writeFormat     ascii;
  37
  38 writePrecision  6;
  39
  40 writeCompression compressed;
  41
  42 timeFormat      general;
  43
  44 timePrecision   6;
  45
  46 runTimeModifiable yes;
  47
  48 functions
  49 {
  50     forces
  51     {
  52         type        forceCoeffs;
  53         functionObjectLibs ( "libforces.so" );
  54         outputControl timeStep;
  55         outputInterval 1;
  56         patches
  57         (
  58             WALL10
  59         );
  60         pName       p;
  61         UName       U;
  62         log         true;
  63         rhoInf      1;
  64         CofR        ( 0 0 0 );
  65         liftDir     ( -0.239733 0.970839 0 );
  66         dragDir     ( 0.970839 0.239733 0 );
  67         pitchAxis   ( 0 0 1 );
  68         magUInf     618.022;
  69         lRef        1;
  70         Aref        1;
  71     }
  72 }
  73
  74 // ************************************************************************* //