Engineering, 11.07.2019 02:40 josephcarriveau
An untwisted wing with aspect ratio of 7 and span of 10m. the wing is an ellitical planform with elliptical lift distribution. the wing load is 900n/m2. when the aircraft is flying at 41.61m/s at seea level conditions. determine the induced drag, the induced angle of attack, the effective angle of attack, the absolute angle of attack and the power needed to overcome the induced drag,
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An untwisted wing with aspect ratio of 7 and span of 10m. the wing is an ellitical planform with ell...
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