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Physics, 14.09.2019 11:30, payshencec21
An aircraft is in a steady level turn at a flight speed of 200 ft/s and a turn rate about the local vertical of 5 deg/s. thrust frm the engine is along the flight direction. given the weight of the aircraft as 50,000 lb and l/d of 10, determine the lift, drag and thrust required for the given equilibrium flight. assume g = 32.2 ft/s
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An aircraft is in a steady level turn at a flight speed of 200 ft/s and a turn rate about the local...
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