Consider the isentropic compression surface drawn in the figure. The Mach number and upstream pressure of the

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Consider the isentropic compression surface drawn in the figure. The Mach number and upstream pressure of the wave are M1 = 10 and p1 = 1atm (1atm = 101325 Pa), respectively. The water flows through an angle of 15°. Calculate the Mach number and pressure in the 2 zone after the compression wave.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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