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v2-f turbulent model for 2D square cylinder application |
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December 17, 2018, 18:07 |
v2-f turbulent model for 2D square cylinder application
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#1 |
New Member
Nayan Levaux
Join Date: Dec 2018
Posts: 3
Rep Power: 7 |
Dear All,
I'm new to OpenFOAM and as a lot of new users, I'm struggling with my problem. I'm trying to simulate the unsteady turbulent 2D incompressible flow past a square cylinder. To this aim, after investigating the SST model, I've tried the model to hopefully better capture separation of the flow and get results more in adequacy with experiments. To do so, I've changed the turbulenceProperties file, modified the fvSchemes and fvSolution, and finally added to the 0 folder two files for the boundary conditions of and . Note as a final remark I'm not using the wall functions, my first grid points give a of 3.5. With all these inputs, OpenFOAM launches the computation but when it comes to analyze the results, I see is remained equal to its initial conditions during the whole simulation. Thus, there is clearly one (several?) bug in my input files. I've tried to change the initial conditions (there is maybe too many constraints on ?) and also numerical schemes but whatever changes I made, I remain with this constant field... Even after researches on forums, I cannot manage this issue. Therefore, I'm here hoping someone could help me fix this issue. Thanks in advance for any reply! PS: Please find my input files hereafter: turbulenceProperties: Code:
simulationType RAS; RAS { turbulence on; RASModel v2f; printCoeffs on; } Code:
ddtSchemes { default backward; } gradSchemes { default Gauss linear; } divSchemes { // From the thesis default none; div(phi,U) bounded Gauss linearUpwind Grad(U); div(phi,k) bounded Gauss upwind; div(phi,epsilon) bounded Gauss upwind; div(phi,omega) bounded Gauss upwind; div(phi,R) Gauss upwind; div(R) Gauss linear; div(phi,nuTilda) Gauss upwind; div((nuEff*dev2(T(grad(U))))) Gauss linear; div(phi,v2) bounded Gauss linearUpwind Grad(v2); div(phi,f) bounded Gauss linearUpwind Grad(f); } laplacianSchemes { default Gauss linear corrected; } interpolationSchemes { default linear; } snGradSchemes { default corrected; } wallDist { method meshWave; } Code:
solvers { p { solver PCG; preconditioner DIC; tolerance 1e-05; relTol 0; } pFinal { solver PCG; preconditioner DIC; tolerance 1e-05; relTol 0; } "(k|epsilon|omega|R|nuTilda|v2)" { solver PBiCG; preconditioner DILU; tolerance 1e-5; relTol 0; } f { solver PCG; preconditioner DIC; tolerance 1e-5; relTol 0; } U { solver PBiCG; preconditioner DILU; tolerance 1e-05; relTol 0; }; } PISO { nCorrectors 2; nNonOrthogonalCorrectors 0; pRefCell 0; pRefValue 0; } Code:
dimensions [0 2 -2 0 0 0 0]; internalField uniform 0.000294; boundaryField { inlet { type fixedValue; value uniform 0.000294; } outlet { type zeroGradient; } noSlipWall { type fixedValue; value uniform 1e-10; } slipWall { type symmetry; } frontAndBack { type empty; } } Code:
dimensions [0 2 -3 0 0 0 0]; internalField uniform 0.0773; boundaryField { inlet { type fixedValue; value uniform 0.0773; } outlet { type zeroGradient; } noSlipWall { type fixedValue; value uniform 1083.794774319; } slipWall { type symmetry; } frontAndBack { type empty; } } Code:
dimensions [0 0 -1 0 0 0 0]; internalField uniform 1e-10; boundaryField { inlet { type zeroGradient; } outlet { type zeroGradient; } noSlipWall { type fixedValue; value uniform 1e-10; } slipWall { type symmetry; } frontAndBack { type empty; } } Code:
dimensions [0 2 -2 0 0 0 0]; internalField uniform 0.000196; boundaryField { inlet { type fixedValue; value uniform 0.000196; } outlet { type zeroGradient; } noSlipWall { type fixedValue; value uniform 1e-10; } slipWall { type symmetry; } frontAndBack { type empty; } } Code:
dimensions [0 2 -1 0 0 0 0]; internalField uniform 0; boundaryField { inlet { type calculated; value uniform 0; } outlet { type calculated; value uniform 0; } noSlipWall { type calculated; value uniform 0; } slipWall { type symmetry; } frontAndBack { type empty; } } |
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December 24, 2018, 06:19 |
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#2 |
Senior Member
Fumiya Nozaki
Join Date: Jun 2010
Location: Yokohama, Japan
Posts: 266
Blog Entries: 1
Rep Power: 19 |
Could you upload the log file of your simulation with v2f model?
Best regards, Fumiya
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December 24, 2018, 12:34 |
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#3 |
New Member
Nayan Levaux
Join Date: Dec 2018
Posts: 3
Rep Power: 7 |
Hi Fumiya,
Thank you for your reply! You will find in attachment the compressed log file as you demand. Have a nice day, Nayan Levaux |
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December 24, 2018, 17:15 |
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#4 | |
Senior Member
Fumiya Nozaki
Join Date: Jun 2010
Location: Yokohama, Japan
Posts: 266
Blog Entries: 1
Rep Power: 19 |
Hi Nayan,
The initial residuals of k and v2 fields become smaller than the tolerance specified in fvSolution file and these fields are not solved and updated from t = 0.000125. Quote:
Best regards, Fumiya
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December 28, 2018, 06:32 |
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#5 |
New Member
Nayan Levaux
Join Date: Dec 2018
Posts: 3
Rep Power: 7 |
Hi Fumiya,
I've followed your advice, but unfortunately, this only postpones the moment et become steady. As I said in the description of the issue, these two quantities should vary in time due to the unsteadyness of the problem at hand. By changing the numerical scheme used to discretize the divergence of (I used bounded Gauss linearUpwind instead of bounded Gauss upwind, like for ), I achieved to have a change in the solution compared to the initial conditions I impose: I was able to see an increase of around the corners of the square. However, at some point, the solution doesn't change anymore like in the first test. So I imagine I should try other schemes, maybe one would give the solution I hope... Do you have any idea of schemes which are better to use with the model? Thank you for the attention you give to my issue! Nayan |
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December 29, 2018, 10:41 |
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#6 |
Senior Member
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Hi,
In fvSolution you can add an entry Code:
"(k|epsilon|omega|R|nuTilda|v2)" { solver PBiCG; preconditioner DILU; tolerance 1e-5; relTol 0; minIter 1; } Tom Last edited by tomf; December 29, 2018 at 10:41. Reason: alignment |
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