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Old   May 17, 2013, 02:48
Default Airfoil Validation
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Manjunatha S
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I am simulating incompressible flow over NACA0012 airfoil using CFX. i used upwind scheme, SST turbulence model , Computational results are well matching with experimental results at low angles but i am not getting stall for any higher angles. can anybody please help me in this reg..

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