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June 30, 2021, 21:41
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OpenFOAM Aerofoil Performance Stats
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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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July 1, 2021, 16:28
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#2 |
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Senior Member
Herpes Free Engineer
Join Date: Sep 2019
Location: The Home Under The Ground with the Lost Boys
Posts: 932
Rep Power: 12 |
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