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August 17, 2009, 06:57 |
Airfoil Pressure coefficients don't match!
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#1 |
New Member
Kappe
Join Date: Aug 2009
Posts: 8
Rep Power: 16 |
Hi,
I meshed a NACA0012, C-grid about 20K node points. Used K-Epsilon viscous model. Compared it with Abbott values. Doesn't match satisfactorily. Please suggest where i would've gone wrong. |
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August 18, 2009, 05:58 |
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#2 |
New Member
Kappe
Join Date: Aug 2009
Posts: 8
Rep Power: 16 |
I have also checked the y+ values which are between 30-60
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