As thickness of an airfoil is increased, the critical AOA a. is greater. b. is less. c.

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As thickness of an airfoil is increased, the critical AOA

a. is greater.

b. is less.

c. remains the same.

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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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