Aerospace Engineering > GATE 2021 > Jet Engines
A jet aircraft weighing 10,000 kg has an elliptic wing with a span of 10 m and area 30 m2. The CD0 for the aircraft is 0.025. The maximum speed of the aircraft in steady and level flight at sea level is 100 m/s. The density of air at sea level is 1.225 kg/m3 and take g = 10 m/s2. The maximum thrust developed by the engine at sea level is _______ N. (round off to two decimal places)
Correct : 9735 to 9797
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