Two things an airfoil designer can change to increase C L(max) are a. thickness and wing area.

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Two things an airfoil designer can change to increase CL(max) are

a. thickness and wing area.

b. chord length and aspect ratio.

c. camber and wing span.

d. thickness and camber.

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Related Book For  book-img-for-question

Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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