Adverse pressure gradient on an airfoil is found a. from the point of maximum thickness to the

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Adverse pressure gradient on an airfoil is found

a. from the point of maximum thickness to the trailing edge.

b. near the stagnation point at the leading edge.

c. from the point of minimum pressure to the trailing edge.

d. Both

(a) and (c).

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Flight Theory And Aerodynamics

ISBN: 9781119772415

4th Edition

Authors: Joseph R. Badick; Brian A. Johnson

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