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May 17, 2013, 02:48 |
Airfoil Validation
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#1 |
New Member
Manjunatha S
Join Date: Nov 2012
Location: Bangalore
Posts: 3
Rep Power: 13 |
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..
Thanks in Advance |
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