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June 30, 2021, 21:41 |
OpenFOAM Aerofoil Performance Stats
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#1 |
New Member
Abdul
Join Date: Jun 2021
Posts: 1
Rep Power: 0 |
I'm a complete newbie when it comes to OpenFOAM, and I would like to obtain aerodynamic performance stats of a NACA 0012 at an AoA of 6 degrees. Can anyone advise me as to what code I need to input and where, as well as plotting lift + drag coefficients and forces?
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