Try to calculate the lift line slope of a rectangular wing with aspect ratio = 10

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Try to calculate the lift line slope of a rectangular wing with aspect ratio λ = 10 in the condition of Ma∞ = 0.6 and compare it with the image text in transcribedof the same wing in incompressible flow.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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