tutorials/solidMechanics/elasticOrthoSolidFoam/orthotropicBlock/0/U

   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       volVectorField;
  13     location    "0";
  14     object      U;
  15 }
  16 // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
  17
  18 dimensions      [0 1 0 0 0 0 0];
  19
  20 internalField   uniform (0 0 0);
  21
  22 boundaryField
  23 {
  24     top
  25       {
  26         type            solidTraction;
  27         traction        uniform ( 0 2e7 0 );
  28         pressure        uniform 0;
  29         orthotropic     yes;
  30         value           uniform (0 0 0);
  31       }
  32
  33     bottom
  34       {
  35         type            symmetryPlane;
  36       }
  37
  38     left
  39       {
  40         type            symmetryPlane;
  41       }
  42
  43     back
  44       {
  45         type            symmetryPlane;
  46       }
  47
  48     right
  49       {
  50         type            solidTraction;
  51         traction        uniform ( 0 0 0 );
  52         pressure        uniform 0;
  53         orthotropic     yes;
  54         value           uniform (0 0 0);
  55       }
  56
  57     front
  58       {
  59         type            solidTraction;
  60         traction        uniform ( 0 0 0 );
  61         pressure        uniform 0;
  62         orthotropic     yes;
  63         value           uniform (0 0 0);
  64       }
  65 }
  66
  67 // ************************************************************************* //