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  1. quibo

    high AoA in xfoil

    Hi, I want to use xfoil to get CL and CD data for all angles of attack, i.e. the full 360 degrees. This is for a NACA 4412 profile, Re = 0.708*10^6. Has anyone ever tried this? I'm beginning to think it's impossible as I get bombarded by "non convergence" and "no stagnation point found"...

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