Question: sent twis question before, please expert solve this question. A small airplane has a total mass of 1820kg and a wing area of 42m2. Determine

sent twis question before, please expert solve this question.

A small airplane has a total mass of 1820kg and a wing area of 42m2. Determine the lift and drag coefficients of this airplane while cruising at an alutude of 4000m at a constant speed of 280km/h and generating 190kW of power. The density of standard air at an alitude of 4000m is =0.819kg/m3 The drag coefficient of the aircraft is The lift coefficient of the aircraft is A small airplane has a total mass of 1820kg and a wing area of 42m2. Determine the lift and drag coefficients of this airplane while cruising at an alutude of 4000m at a constant speed of 280km/h and generating 190kW of power. The density of standard air at an alitude of 4000m is =0.819kg/m3 The drag coefficient of the aircraft is The lift coefficient of the aircraft is

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