tutorials/compressible/sonicFoam/ras/nacaAirfoil/0/U

   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       volVectorField;
  13     object      U;
  14 }
  15 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
  16
  17 dimensions      [0 1 -1 0 0 0 0];
  18
  19 internalField   uniform (600 148.16 0);
  20
  21 boundaryField
  22 {
  23     INLE1
  24     {
  25         type            supersonicFreestream;
  26         pInf            100000;
  27         TInf            300;
  28         UInf            (600 148.16 0);
  29         gamma           1.4;
  30         value           uniform (600 148.16 0);
  31     }
  32
  33     OUTL2
  34     {
  35         type            inletOutlet;
  36         inletValue      uniform (600 148.16 0);
  37         value           uniform (600 148.16 0);
  38     }
  39
  40     SYMP3
  41     {
  42         type            empty;
  43     }
  44
  45     WALL10
  46     {
  47         type            fixedValue;
  48         value           uniform (0 0 0);
  49     }
  50 }
  51
  52 // ************************************************************************* //