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An airplane weighing 5000 lb is flying at standard sea

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An airplane weighing 5000 lb is flying at standard sea level with a velocity of 200 mph. At this velocity, the L/D ratio is a maximum. The wing area and aspect ratio are 200 and 8.5, respectively. The Oswald efficiency factor is 0.93. Calculate the total drag on the airplane.

Reference no: EM13626194

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