Try to find the ratio of the lift force of a slender cylindrical fuselage and triangular flat

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Try to find the ratio of the lift force of a slender cylindrical fuselage and triangular flat wing with small aspect ratio in the case of image text in transcribedto the lift force of which at the angle of attack image text in transcribedin the case of image text in transcribed

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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