What is coefficient of lift cl of an airplane weighing 2200
What is coefficient of lift (CL) of an airplane weighing 2200 lbs with wing surface area of 150 ft2, in steady level flight, at sea level density (0.0023 slugs/ft3), flying at 160 kts?
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what is coefficient of lift cl of an airplane weighing 2200 lbs with wing surface area of 150 ft2 in steady level
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