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Angle of attack problem.

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hrishikesh

Member
Joined
Aug 13, 2010
Messages
11
Location
Pune, Maharashtra, India
I have selected a NACA 4412 wing profile for my ultralight aircraft having flying weight 200 kgs powered by a 21 hp simonini engine (Thrust = 80 kg). Wing area = 9.27 sq.m. How do I decide the angle of attack and coefficient of lift ?
 
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