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![]() Quote:
http://www.google.com/search?q=Cruis...w=1920&bih=941 http://enpub.fulton.asu.edu/aero/mae...ingchapter.pdf "Maximum coefficient of lift" is the term for the CLmax a section can produce and defines the Angle of Attack the airfoil stalls. http://www.google.com/search?q=Cruis...0&bih=941&bs=1 |
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