Consider a finite wing with an aspect ratio of 8 and a taper ratio of 0.8. The

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Consider a finite wing with an aspect ratio of 8 and a taper ratio of 0.8. The airfoil profile is thin and symmetrical. Calculate the lift and induced drag coefficient of the wing at an angle of attack of 5°. Assume that δ = τ.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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Question Posted: Apr 29, 2024 06:00 AM

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Consider a finite wing with an aspect ratio of 8 and a taper ratio of 0.8. The

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Aerodynamics

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