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laminar pipe flow with buoyantSimpleRadiationFoam and janafThermo crashes |
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September 28, 2010, 16:01 |
laminar pipe flow with buoyantSimpleRadiationFoam and janafThermo crashes
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#1 |
New Member
Fabian Hampp
Join Date: Dec 2009
Location: Abu Dhabi
Posts: 8
Rep Power: 17 |
Hi all,
I try to simulate a laminar (Re~ 200) pipe flow with constant wall temperature. I planned to use buoyantSimpleRadiationFoam, since I want to activate later on a radiation model. So far my mesh is not axis symmetric yet; it is just a pretty fine 2D gambit mesh which I translated via fluentMeshToFoam. Later on I want to use makeAxialMesh to simulate axis symmetry. Anyhow, since I have high temperature gradients (1000K at the wall and inflow temperature of 300K), I want to use janafThermo to calculate cp as a function of T. My calculation fails with the message: Foam Fatal Error: attempt to use janafThermo<equationOfState> out of temperature range 200->6000; T = 137.957 I also tried to set the wall temperature to 300K - same result. anybody have a clue, why this occurs? Maybe wrong Janaf parameter? I used a parameter set from an oxidizer with MW like air, which I found in one of the combustion tutorials. Also, my velocity field looks really weird for a laminar pipe flow. The folder constant/ contains following files: g: dimensions [0 1 -2 0 0 0 0]; value (9.81 0 0 ); RASProperties: RASModel laminar; turbulence on; printCoeffs on; thermophysicalProperties: thermoType hPsiThermo<pureMixture<sutherlandTransport<specieT hermo<janafThermo<perfectGas>>>>>; mixture air 1 28.8504 200 6000 1000 pRef 101325; radiationProperties: standard file from corresponding tutorial case The folder system/ contains following files: controlDict: application buoyantSimpleRadiationFoam; startFrom latestTime; startTime 0; stopAt endTime; endTime 1; deltaT 1e-05; writeControl timeStep; writeInterval 50; purgeWrite 0; writeFormat ascii; writePrecision 6; writeCompression uncompressed; timeFormat general; timePrecision 6; runTimeModifiable yes; fvSchemes: ddtSchemes { default steadyState; } gradSchemes { default Gauss linear; } divSchemes { default none; div(phi,U) Gauss upwind; div(phi,h) Gauss upwind; div((muEff*dev2(grad(U).T()))) Gauss linear; } laplacianSchemes { default none; laplacian(muEff,U) Gauss linear corrected; laplacian((rho*(1|A(U))),p) Gauss linear corrected; laplacian(alphaEff,h) Gauss linear corrected; laplacian(gammaRad,G) Gauss linear corrected; } interpolationSchemes { default linear; } snGradSchemes { default corrected; } fluxRequired { default no; p; } fvSolution: solvers { p { solver PCG; preconditioner DIC; tolerance 1e-08; relTol 0; } U { solver PBiCG; preconditioner DILU; tolerance 1e-05; relTol 0; } h { solver PBiCG; preconditioner DILU; tolerance 1e-05; relTol 0; } rho { solver PCG; preconditioner DIC; tolerance 1e-08; relTol 0; } G { solver PCG; preconditioner DIC; tolerance 1e-08; relTol 0; } } SIMPLE { nNonOrthogonalCorrectors 0; pRefCell 0; pRefValue 0; } relaxationFactors { rho 0.7; p 0.2; U 0.7; h 0.5; G 0.7; } Boundary Conditions: Temperature: dimensions [0 0 0 1 0 0 0]; internalField uniform 300; boundaryField { wall { type fixedValue; value uniform 1000.0; } axis { type symmetryPlane; } outlet { type zeroGradient; } inlet { type fixedValue; value uniform 300.0; } frontAndBackPlanes { type empty; } } alphat: dimensions [1 -1 -1 0 0 0 0]; internalField uniform 2.8739e-05; boundaryField { wall { type zeroGradient; } axis { type symmetryPlane; } outlet { type zeroGradient; } inlet { type fixedValue; value uniform 2.8739e-05; } frontAndBackPlanes { type empty; } } mut: dimensions [1 -1 -1 0 0 0 0]; internalField uniform 1.983e-05; boundaryField { wall { type zeroGradient; } axis { type symmetryPlane; } outlet { type zeroGradient; } inlet { type fixedValue; value uniform 1.983e-05; } frontAndBackPlanes { type empty; } } Velocity: dimensions [0 1 -1 0 0 0 0]; internalField uniform (0.081 0 0); boundaryField { wall { type fixedValue; value uniform (0 0 0); } axis { type symmetryPlane; } outlet { type zeroGradient; } inlet { type fixedValue; value uniform (0.081 0 0); } frontAndBackPlanes { type empty; } } Pressure: dimensions [1 -1 -2 0 0 0 0]; internalField uniform 0; boundaryField { wall { type zeroGradient; } axis { type symmetryPlane; } outlet { type fixedGradient; gradient uniform -1.2; } inlet { type fixedValue; value uniform 101325; } frontAndBackPlanes { type empty; } } |
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September 29, 2010, 12:38 |
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#2 |
New Member
Fabian Hampp
Join Date: Dec 2009
Location: Abu Dhabi
Posts: 8
Rep Power: 17 |
Sorry, I forgot to mention that I am using OpenFOAM 1.6
best, Fabian |
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Thread | Thread Starter | Forum | Replies | Last Post |
laminar pipe flow with buoyantSimpleRadiationFoam and janafThermo crashes | Fabian | OpenFOAM Pre-Processing | 0 | September 27, 2010 16:38 |