Try to calculate the lift coefficient of a thin rectangular wing of = 5 with Ma

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Try to calculate the lift coefficient of a thin rectangular wing of λ = 5 with Ma∞ = 0.85 using Prandtl–Glauert rule and the affine combination parameter chart method.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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