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openfoam/tutorials/mesh/snappyHexMesh/airfoilWithLayers/constant/transportProperties
2020-12-23 10:01:39 +01:00

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1.2 KiB
C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: v2012 |
| \\ / A nd | Website: www.openfoam.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Air temperature at standard atmospheric pressure = 540 R = 300 K
// See README.md
// c = 347.336 [m/s]
// Ma = UInf/c = 0.15
// UInf = 52.1004 [m/s]
// ReChord = 6e6 (per chord)
// Chord = 1 [m]
// ReChord = UInf*Chord/nuFluid
// nuFluid = UInf*Chord/ReChord = 8.6834e-06 [m2/s]
transportModel Newtonian;
nu 8.6834e-06;
// ************************************************************************* //