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You are here: home->sp_inst->H300->Z.0.0.0.7.A.1

0007
An aircraft wing is designed to produce lift resulting from
A) negative air pressure below the wing's surface and positive air pressure above the wing's surface.
*B) positive air pressure below the wing's surface and negative air pressure above the wing's surface.
C) a larger center of pressure above the wing's surface and a lower center of pressure below the wing's surface.

 

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