Adverse pressure gradient on an airfoil is found a. from the point of maximum thickness to the
Question:
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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Related Book For
Flight Theory And Aerodynamics
ISBN: 9781119772415
4th Edition
Authors: Joseph R. Badick; Brian A. Johnson
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