As camber of an airfoil is increased, its CL at any AOA a. is less. b. remains

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As camber of an airfoil is increased, its CL at any AOA

a. is less.

b. remains the same.

c. is greater.

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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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Question Posted: May 05, 2024 05:02 AM

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As camber of an airfoil is increased, its CL at any AOA a. is less. b. remains

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Flight Theory And Aerodynamics

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