If the airplane of Problem 1–38 weighs 1450 lbf, estimate the lift force produced by the airplane’s wings (in lbf and newtons) when flying at 70.0 m/s.

Data from Problem 38

An airplane flies horizontally at 70 m/s. Its propeller delivers 1500 N of thrust (forward force) to overcome aerodynamic drag (backward force). Using dimensional reasoning and unity converstion ratios, calculate the useful power delivered by the propeller in units of kW and horsepower.