A small aircraft has a wing area of 28 m2, a lift
Chapter 11, Problem 92P(choose chapter or problem)
Problem 92P
A small aircraft has a wing area of 28 m2, a lift coefficient of 0.45 at takeoff settings, and a total mass of 2500 kg. Determine(a) the takeoff speed of this aircraft at sea level at standard atmospheric conditions,(b) the wing loading, and (c) the required power to maintain a constant cruising speed of 300 km/h for a cruising drag coefficient of 0.035.
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