During takeoff, the thrust from each of the two engines of a Boeing 737 is T = 95 kN. The mass center of the airplane is located at G, the horizontal distance between the main landing gear and G is d = 5.15 m, the horizontal distance between the front landing gear and the main landing gear is ℓ = 11.1 m, and the height of the mass center above the ground is h = 2.36 m. The mass of the plane is m = 74,200 kg, and the thrust from each engine is a distance δ = 1.15 m above the ground.
Assuming that the wings are the only surfaces generating lift during takeoff, determine the lift L generated by each wing when the normal force on the main landing gear is 25% of its initial takeoff value. The line of action of L goes through G.
Figure P7.16
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