Lift and Drag A small aircraft has a wing area of 35 m², a lift coefficient of 0.45 at take-off settings, and a total ma
Posted: Fri Jul 08, 2022 5:48 am
Lift and Drag A small aircraft has a wing area of 35 m², a lift coefficient of 0.45 at take-off settings, and a total mass of 4000 kg. Determine a) the take-off speed of this aircraft at sea level at standard atmospheric conditions b) the wing loading, and c) the required power to maintain a constant cruising speed of 300 km/h for a cruising drag coefficient of 0.035.