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Physics, 30.11.2021 22:20 vjmfghhh

A light aircraft with a wing area of 200 ft2 and a weight of 2000 lbf has a lift coefficient of 0.40 and a drag coefficient of 0.05. Determine the power (in horsepower) required to maintain level flight.

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A light aircraft with a wing area of 200 ft2 and a weight of 2000 lbf has a lift coefficient of 0.40...
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