Kindly don't just copy paste from chegg. EXAMPLE 5: Just downstream of a normal shock in air, the pressure, temperature and velocityare 270 kPa, 150°C and 190 m/s respectively.1- Calculate the pressure, temperature and velocity prior to the shock wave.2- Determine if the continuity equation is respected downstream and up-stream of the normalshock wave.Take k = 1.4 and R = 287 J/(kg.K)

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Answered: 1- Calculate the pressure, temperature…

1- Calculate the pressure, temperature and velocity prior to the shock wave. 2- Determine if the continuity equation is respected downstream and up-stream of the normal shock wave.

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.68P

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Kindly don't just copy paste from chegg.

EXAMPLE 5: Just downstream of a normal shock in air, the pressure, temperature and velocity
are 270 kPa, 150°C and 190 m/s respectively.
1- Calculate the pressure, temperature and velocity prior to the shock wave.
2- Determine if the continuity equation is respected downstream and up-stream of the normal
shock wave.
Take k = 1.4 and R = 287 J/(kg.K)

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