Consider a finite wing with an aspect ratio of 6. Suppose the lift is distributed in an

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Consider a finite wing with an aspect ratio of 6. Suppose the lift is distributed in an elliptical shape. The lift slope of the airfoil profile is 0.1/degree. Calculate and compare the lift coefficients of

(a) straight wing and

(b) swept-back wing, the half-chord sweep angle is 45°.

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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 6. Suppose the lift is distributed in an

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Aerodynamics

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