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Physics, 18.02.2020 05:31 autumperry682

On its takeoff roll, the airplane starts from rest and accelerates according to a = a0 − kv2 , where a0 is the constant acceleration resulting from the engine thrust and −kv2 is the acceleration due to aerodynamic drag. If a0 = 2 m/s2 , k = 0.00004 m−1, and v is in meters per second, determine the design length of runway required for the airplane to reach the takeoff speed of 250 km /h if the drag term is (a) excluded and (b) included.

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On its takeoff roll, the airplane starts from rest and accelerates according to a = a0 − kv2 , where...
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