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The lift coefficient at this speed is 045 and the drag

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Reference no: EM13622359

An aircraft is in level flight at 225 km/hr through air at standard conditions. The lift coefficient at this speed is 0.45 and the drag coefficient is 0.065. The mass of the aircraft is 900 kg. Calculate the lift area for the craft, and the requried engine thrust and power.

Reference no: EM13622359

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