Wing span= 15.3 wing area= 27.3 m^2 takeoff gross mass= 3900 kg Oswald efficiency factor= 0.9 zero-lift drag coefficient
Posted: Mon May 02, 2022 3:21 pm
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 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.