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boundaryFoam, axisymmetry and turbulence models |
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May 12, 2011, 14:05 |
boundaryFoam, axisymmetry and turbulence models
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Thomas Toulorge
Join Date: May 2011
Posts: 1
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Hello,
I am trying to obtain a fully developed velocity profile in a duct at low Reynolds number (Re ~ 6000) by using an axisymmetric geometry with boundaryFoam. I would like to use the k-omega SST turbulence model, but I get a strange error that seems to occur at initialization of the turbulence model object: Code:
/*---------------------------------------------------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 1.7.x | | \\ / A nd | Web: www.OpenFOAM.com | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ Build : 1.7.x-3776603e4c6c Exec : /opt/openfoam171/applications/bin/linux64GccDPOpt/boundaryFoam Date : May 12 2011 Time : 18:34:16 Host : PMA-08-003 PID : 10174 Case : /home/u0056407/DG/Tests/SideCavity/CFD/Duct/Duct_Test nProcs : 1 SigFpe : Enabling floating point exception trapping (FOAM_SIGFPE). // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Create time Create mesh for time = 0 Reading field U Creating face flux Selecting incompressible transport model Newtonian Selecting RAS turbulence model kOmegaSST --> FOAM FATAL ERROR: Maximum number of iterations reached. Increase maxIter. maxIter:20 nChangedCells:0 nChangedFaces:4 From function FaceCellWave<Type>::FaceCellWave(const polyMesh&, const labelList&, const List<Type>, UList<Type>&, UList<Type>&, const label maxIter) in file /home/opencfd/OpenFOAM/OpenFOAM-1.7.x/src/OpenFOAM/lnInclude/FaceCellWave.C at line 862. FOAM exiting Am I doing something wrong? Is it even possible at all to use boundaryFoam in an axisymmetric setting? The files are attached. Thanks in advance! Thomas. |
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