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A small airplane has a total mass of 1850kg and a wing area of 42m2. Determine the lift and drag coefficients of this airplane while

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A small airplane has a total mass of 1850kg and a wing area of 42m2. Determine the lift and drag coefficients of this airplane while cruising at an altitude of 4000m at a constant speed of 280km/h and generating 190kW of power. The density of standard air at an altitude of 4000m is =0.819kg/m3. The drag coefficient of the aircraft is The lift coefficient of the aircraft is

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