A wing of 2 percent camber, 5-in chord, and 30-in span is tested at a certain angle
Question:
(a) The angle of attack,
(b) The minimum drag of the wing and the angle of attack at which it occurs, and
(c) The maximum lift-to-drag ratio.
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Related Book For 
Fundamentals of Thermal-Fluid Sciences
ISBN: 978-0078027680
5th edition
Authors: Yunus A. Cengel, Robert H. Turner, John M. Cimbala
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