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A wing with an aspect ratio of 15 and a span efficiency of 0.88 uses an airfoil with a lift curve slope of 0.11/deg. Calculate
A wing with an aspect ratio of 15 and a span efficiency of 0.88 uses an airfoil with a lift curve slope of 0.11/deg. Calculate the wing lift curve slope.
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Fundamentals Of Aerodynamics
Authors: John Anderson
6th Edition
1259129918, 978-1259129919
