Wing span= 15.3
wing area= 27.3 m^2
takeoff gross mass= 3900 kg
Oswald efficiency factor= 0.9
zero-lift drag coefficient= 0.03
maximum power for each engine (twin engine)= 280 kW at sea level
propellers efficency= 0.84
Calculate the maximum rate of climb at sea level and at 4.5 km altitude.
Calculate the maximum rate of climb at sea level and at 4.5 km altitude.
Wing span= 15.3 wing area= 27.3 m^2 takeoff gross mass= 3900 kg Oswald efficiency factor= 0.9 zero-lift drag coefficient
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answerhappygod
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Wing span= 15.3 wing area= 27.3 m^2 takeoff gross mass= 3900 kg Oswald efficiency factor= 0.9 zero-lift drag coefficient
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