Consider a light plane that has a total weight of 11,000 N and a wing area of 39 m2 and
Chapter 11, Problem 11-94(choose chapter or problem)
Consider a light plane that has a total weight of 11,000 N and a wing area of 39 m2 and whose wings resemble the NACA 23012 airfoil with no flaps. Using data from Fig. 1145, determine the takeoff speed at an angle of attack of 58 at sea level. Also determine the stall speed.
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