A symmetrical double-cambered airfoil is placed in a supersonic flow, and the relative position of its focus

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A symmetrical double-cambered airfoil is placed in a supersonic flow, and the relative position of its focus (also its pressure center) is calculated by using the second-order approximate pressure coefficient formulaimage text in transcribedwhere

image text in transcribedis the negative value of a sectional area of a dimensional symmetric double-cambered airfoil.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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