Given the sweep angle 0 of the delta wing and the aspect ratio , try to prove

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Given the sweep angle χ0 of the delta wing and the aspect ratio λ, try to prove Given the sweep angle χ0 of the delta wing and the aspect ratio λ, try to prove from the geometric relationship that λ tanχ0 = 4.


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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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