A light aircraft with a wing area of 200 ft2 has a lift


A light aircraft with a wing area of 200 ft2 has a lift coefficient of 0.4 and a drag coefficient of 0.05. the power required to maintain level flight is 66hp. determine the weight of the airplane. recall power is force in the direction of velocity, times velocity. the density of air is 2.38 E-3 slug/ft3

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Mechanical Engineering: A light aircraft with a wing area of 200 ft2 has a lift
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