For a cambered airfoil, the center of pressure (CP) a. moves to the rear of the wing

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For a cambered airfoil, the center of pressure (CP)

a. moves to the rear of the wing at low AOA.

b. moves backward as AOA increases.

c. moves forward as AOA increases.

d. Both

(a) and (c).

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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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