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Required information An aircraft has a wing area of 40m2, a fift coefficient of 0.45 at takeoff settings, and a total mass of 4250kg. The

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Required information An aircraft has a wing area of 40m2, a fift coefficient of 0.45 at takeoff settings, and a total mass of 4250kg. The density of standard aif at sea level is =1.225kg3. Determine the required power to maintain a constant cruising speed of 345km/h for a cruising drag coetticient of 0.035 . The required power to maintain a constant cruising speed of 345km/h is kW

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