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Stalling problem with simpleFoam on a NACA0012 |
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March 2, 2010, 05:13
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Stalling problem with simpleFoam on a NACA0012
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#1 |
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New Member
Damien Guénot
Join Date: Mar 2009
Location: France
Posts: 1
Rep Power: 0  |
Hello,
I have a problem with a simpleFoam computation : I tried to compute a 2D NACA0012 at Re=100000 (Mach~0.17) but the stalling effect on drag and lift coefficient is underestimated, as can be seen on the following curves. I am using Spalart-Allmaras model. This mesh is the one used by Strelets (STRELETS, M., 2001, Detached eddy simulation of massively separated flows, AIAA Paper 2001-0879). It is a O shaped fine mesh (no wall function) expanding at 15 chords around the wing. I already used this mesh with an other solver and I didn't face this problem If someone has an idea, he would be welcome. Thank you Damien |
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March 3, 2010, 08:46
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#2 |
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Senior Member
maddalena
Join Date: Mar 2009
Posts: 436
Rep Power: 23 |
Hello Damien,
welcome to the OpenFoam community! I had similar problems some time ago. Maybe this thread can help you: http://www.cfd-online.com/Forums/ope...omparison.html Good luck! maddalena |
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