The pressure upstream of a normal shock wave is 1 atm. The pressureand temperature downstream of the wave are 10.33 atm and 1390 ◦R,respectively. Calculate the Mach number and temperature upstream of thewave and the total temperature and total pressure downstream of the wave.

The pressure upstream of a normal shock wave is 1 atm. The pressureand temperature downstream of the wave are 10.33 atm and 1390 ◦R,respectively. Calculate the Mach number and temperature upstream of thewave and the total temperature and total pressure downstream of the 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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Question

The pressure upstream of a normal shock wave is 1 atm. The pressure
and temperature downstream of the wave are 10.33 atm and 1390 ^◦R,
respectively. Calculate the Mach number and temperature upstream of the
wave and the total temperature and total pressure downstream of the wave.

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