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An airplane has a rectangular-platform wing that has an

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Reference no: EM13627019

An airplane has a rectangular-platform wing that has an elleiptical spanwise lift distribution. the airplane has a mass of 1200 kg, a wing area of 20 m^2, and a wingspan of 14 m, and it is flying at 60 m/s at 3000 m altitude in a standard atmosphere. if the form drag coefficient is .01, calculate the total drag on the wing and the power (p=FV) necessary to overcome the drag.

Reference no: EM13627019

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