At the upstream of the shock wave, the air temperature and pressure are 14.85 C and 101,325

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At the upstream of the shock wave, the air temperature and pressure are 14.85 °C and 101,325 Pa, respectively; just downstream of the shock wave, the air temperature and pressure are 417 °C and 877,069.2 Pa, respectively. Calculate the changes in the enthalpy, internal energy, and entropy of the wave.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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