Physics, 10.03.2020 00:17 augustusj48
An airplane has a total mass of 35,000 kg and a wing planform area of 65. The airplane is cruising at 10,000 m altitude with a velocity of 1100 km/h. The density of air on cruising altitude is 0.414. The lift force is the weight of the airplane. The lift coefficient of this airplane at the cruising altitude is .
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