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You are here: home->com_plt->H300->2.5.1.5.8.A.1

5158
Lift on a wing is most properly defined as the
A) differential pressure acting perpendicular to the chord of the wing.
B) reduced pressure resulting from a laminar flow over the upper camber of an airfoil, which acts perpendicular to the mean camber.
*C) force acting perpendicular to the relative wind.

 

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