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Showing results 1 to 1 of 1 Search took 0.00 seconds. Search: Posts Made By: wrb

Forum: ANSYS March 1, 2018, 10:23

Replies: 1 Analysing Lift for NACA0012 through range of angles of attack. Views: 995 Posted By wrb Analysing Lift for NACA0012 through range of angles of attack. I am currently trying to find coefficients of lift for a NACA 0012 (2D) airfoil operating at a Reynolds number of 6million, mach number of 0.3 and with a chord length of 1m through a range of angles...

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