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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