A 32000 kg airplane begins to climb at an angle of 3

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Reference no: EM13630178

A 32,000 kg airplane begins to climb at an angle of 3 degrees. Its initial speed is 150 m/s, and after one minute its speed has increased to 170 m/s. The airplane experiences an aerodynamic drag force D that opposes its velocity. The lift, drag, and thrust forces can be decomposed as shown, where L = Lb2,D = - Db1, and T = Tb1. Using linear impulse concepts and |D| = 12,000 N, determine the constant thrust T (developed by the engines) that is needed to offset both the aerodynamic drag and gravitational force and allow the airplane to increase its speed as described above.

Reference no: EM13630178

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