Consider a light plane that has a total weight of 15,000N
Chapter 11, Problem 95P(choose chapter or problem)
Problem 95P
Consider a light plane that has a total weight of 15,000N and a wing area of 46 m2 and whose wings resemble the NACA 23012 airfoil with no flaps. Using data from Fig. 15-45, determine the takeoff speed at an angle of attack of 5° at sea level. Also determine the stall speed.
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