/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: dev | | \\ / A nd | Web: http://www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class dictionary; object transportProperties; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // phase1 { transportModel Newtonian; nu nu [0 2 -1 0 0 0 0] 1e-06; rho rho [1 -3 0 0 0 0 0] 1000; 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] 1.48e-05; rho rho [1 -3 0 0 0 0 0] 1; 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] 0.07; // ************************************************************************* //