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A small aircraft has a total mass of 1500 kg and a wing area of 45 m. The aircraft is cruising at an altitude

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A small aircraft has a total mass of 1500 kg and a wing area of 45 m. The aircraft is cruising at an altitude of 4000m at a constant speed of 280 km/h and generating 200 kW of power. The density of air at 4000m is 0.819 kg/m. a) Determine the drag coefficient for the aircraft. b) Determine the lift coefficient for the aircraft.

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