Consider a thin flat plate with an angle of attack of 5. Calculate: (a) the lift coefficient,

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Consider a thin flat plate with an angle of attack of 5°. Calculate:

(a) the lift coefficient,

(b) the moment coefficient about the leading edge,

(c) the moment coefficient about the 1/4 chord point, and

(d) the moment coefficient about the trailing edge.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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