Question #146092

A 40,000 kg airplane is provided with 130,000N of thrust by its engines as it takes of at an angle of 25 degrees above the horizontal. If the velocity of the airplane is constant, how much upward force on it is provided by its vertical component?

Expert's answer

Fy=Fsin25°=130000⋅0.423≈55000NF_y=Fsin25°=130000\cdot 0.423\approx55000 N


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