An airplane powered by a single turbojet engine loses its only engine at an alti...
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An airplane powered by a single turbojet engine loses its only engine at an altitude h = 2000 m above sea level, and the pilot decides to glide the maximum possible horizontal distance. How far will it glide if the mass is m = 4000 kg, the parasitic drag coefficient is CD0 = 0.065, the Oswald factor is e = 0.90 and the wing aspect ratio is AR=20?
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