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foam-extend4.1-coherent-io/tutorials/lesInterFoam/nozzleFlow2D/constant/transportProperties

68 lines
2.2 KiB
C++

/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
twoPhase
{
transportModel twoPhase;
phase1 phase1;
phase2 phase2;
}
phase1
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 5.952e-06;
rho rho [1 -3 0 0 0 0 0] 840;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
m m [0 0 1 0 0 0 0] 1;
n n [0 0 0 0 0 0 0] 0;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 0.0142515;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
k k [0 0 1 0 0 0 0] 99.6;
n n [0 0 0 0 0 0 0] 0.1003;
}
}
phase2
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 8.5e-07;
rho rho [1 -3 0 0 0 0 0] 20;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
m m [0 0 1 0 0 0 0] 1;
n n [0 0 0 0 0 0 0] 0;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 0.0142515;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
k k [0 0 1 0 0 0 0] 99.6;
n n [0 0 0 0 0 0 0] 0.1003;
}
}
sigma sigma [1 0 -2 0 0 0 0] 0.0261;
// ************************************************************************* //