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August 9, 2021, 11:39 |
Checkerboarding problem_simpleFoam
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#1 |
New Member
Join Date: Jan 2021
Location: Norway
Posts: 22
Rep Power: 5 |
Hello Everyone,
I am working on very simple steady state solution (2D) of a channel flow using simpleFoam and having single cell along the flow direction (x). I have used periodic boundary condition for inlet and outlet, noSlip (for U) for the walls. I have tried different available fvSchemes. However, getting checkerboarding issue with p, Uy and Uz. Any suggestions to eliminate the issue will be highly appreciated. Thanks. Subho |
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August 9, 2021, 12:18 |
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#2 |
Senior Member
Uwe Pilz
Join Date: Feb 2017
Location: Leipzig, Germany
Posts: 744
Rep Power: 15 |
First: Periodic b.c. often lead to problems. You are in 2D. It may be much better stacking some of the geometries and avoid periodicity in b.c.
Second: Checkerboarding is an issue of Mesh, may be combined with schemes. Try using a finer mesh.
__________________
Uwe Pilz -- Die der Hauptbewegung überlagerte Schwankungsbewegung ist in ihren Einzelheiten so hoffnungslos kompliziert, daß ihre theoretische Berechnung aussichtslos erscheint. (Hermann Schlichting, 1950) |
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August 9, 2021, 13:18 |
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#3 |
New Member
Join Date: Jan 2021
Location: Norway
Posts: 22
Rep Power: 5 |
Many thanks for your reply Uwe. In my case, I have restrict to a 2D simulation. I have used fine mesh.
Subhojit |
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August 10, 2021, 00:58 |
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#4 |
Senior Member
Uwe Pilz
Join Date: Feb 2017
Location: Leipzig, Germany
Posts: 744
Rep Power: 15 |
In most cases, the main question is not
How may I get my simulation running but How do I change my real world problem into a simulation. > I have restrict to a 2D simulation Normally, there are no such restrictions. We have to select the simulation which gives the most reliable results. Often, this is the simplest one. If you want to stay your simulation, I recommend using more stable schemes and relaxation.
__________________
Uwe Pilz -- Die der Hauptbewegung überlagerte Schwankungsbewegung ist in ihren Einzelheiten so hoffnungslos kompliziert, daß ihre theoretische Berechnung aussichtslos erscheint. (Hermann Schlichting, 1950) |
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August 13, 2021, 11:17 |
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#5 | |
New Member
Join Date: Jan 2021
Location: Norway
Posts: 22
Rep Power: 5 |
Hello Uwe,
Thanks for your reply. I am using the following schemes Code:
ddtSchemes { default steadyState; } gradSchemes { default Gauss linear; //cellLimited Gauss linear 1; } divSchemes { default none; div(phi,U) bounded Gauss limitedLinearV 1;//bounded Gauss linearUpwind grad(U); div(phi,k) bounded Gauss limitedLinear 1; div(phi,epsilon) bounded Gauss limitedLinear 1; div((nuEff*dev2(T(grad(U))))) Gauss linear; div((nu*dev2(T(grad(U))))) Gauss linear;//For LRR, SSG div(phi,R) bounded Gauss limitedLinear 1; //For LRR, SSG div(R) Gauss linear; //For LRR, SSG } laplacianSchemes { //default Gauss linear corrected; default Gauss linear orthogonal; } interpolationSchemes { default linear; //interpolate(U) linear; } snGradSchemes { //default corrected; default orthogonal; } fluxRequired { default no; p; } wallDist { method meshWave; } for p 0.3 and for rest 0.7. I have also tried with lower/higher relaxations. But no noticeable improvements. Subhojit Quote:
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Tags |
checkerboarding, simplefoam convergence, steady state |
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