At a given point on the surface of the wing of the airplane in Prob. 3.6, the

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At a given point on the surface of the wing of the airplane in Prob. 3.6, the flow velocity is 130 m/s. Calculate the pressure coefficient at this point.

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Fundamentals of Aerodynamics

ISBN: 978-0070016798

2nd Edition

Authors: J. Anderson

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Question Posted: Dec 09, 2010 03:24 AM

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At a given point on the surface of the wing of the airplane in Prob. 3.6, the

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Fundamentals of Aerodynamics

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