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January 8, 2020, 06:16 |
simpleFoam convergence issue
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#1 |
New Member
Gustavo Barahona
Join Date: Dec 2019
Location: Germany
Posts: 2
Rep Power: 0 |
Hi everybody!
I'm trying to simulate a flow trough an air Knife. At the inlet, the velocity should be approximate 20 m/s. The velocity at the outlet must be constant through the air knife. So I have to simulate various designs to reach this uniform velocity at the outlet. I tried with different b.c. combinations with simulation model k-omega-sst but my results are not reasonable. The residuals are oscillating too much and my case is not converging. I give you some information about my settings. My y+ is about 15 (that's why I set wallFunctions). I'd be very grateful for any help!! checkMesh.png residuals.png fvSchemes ddtSchemes { default steadyState; } gradSchemes { default cellLimited Gauss linear 1;//faceLimited leastSquares 0.5; //Gauss linear; //grad(U) cellLimited Gauss linear 1;// } divSchemes { default none; div(phi,U) bounded Gauss linearUpwind grad(U); div(phi,k) bounded Gauss linearUpwind grad(k);//limitedLinear 1; div(phi,omega) bounded Gauss linearUpwind grad(omega);//limitedLinear 1; div(div(phi,U)) Gauss linear; div((nuEff*dev2(T(grad(U))))) Gauss linear; } laplacianSchemes { default Gauss linear corrected;//limited 0.33;// } interpolationSchemes { default linear; } snGradSchemes { default corrected;//limited 0.33;// } wallDist { method meshWave; } fvSolutions p { solver GAMG; tolerance 1e-07; relTol 0.01; smoother GaussSeidel; } Phi { $p; } U { solver smoothSolver; smoother symGaussSeidel; tolerance 1e-07; relTol 0.01; } "(k|omega)" { solver smoothSolver; smoother symGaussSeidel; tolerance 1e-06; relTol 0.01; } } SIMPLE { nNonOrthogonalCorrectors 0; consistent yes; residualControl { p 1e-2; U 1e-3; "(k|omega)" 1e-3; } } potentialFlow { nNonOrthogonalCorrectors 10; } relaxationFactors fields {p 0.3;} equations { U 0.7; k 0.1; omega 0.1;} for U I defined: internalField uniform (0 0 0); fixedWalls type noSlip; inlet type fixedValue; value uniform (20 0 0); outlet type zeroGradient; for p : internalField uniform 0; fixedWalls type zeroGradient; inlet type zeroGradient; outlet type fixedValue; value uniform 0; for k: internalField uniform 0.84; inlet type fixedValue; value uniform 0.84; outlet type inletOutlet; inletValue $internalField; value $internalField; fixedWalls type kqRWallFunction; value uniform 0.84; for omega: uniform 434; inlet type fixedValue; outlet type inletOutlet; inletValue $internalField; value $internalField; fixedWalls type omegaWallFunction; value $internalField; Greetings Gustavo |
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