Question: sent twis question before, please expert solve this question. Required information An aircraft has a wing area of 40m2, a lift coefficient of 0.45 at
Required information An aircraft has a wing area of 40m2, a lift coefficient of 0.45 at takeoff settings, and a total mass of 4300kg The density of standard air at sea level is =1.225kg/m3 Determine the required power to maintain a constant cruising speed of 330km/h for a cruising drag coefficient of 0.035 . The required power to maintain a constant cruising speed of 330km/h is kW
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