16. Air is expanded through a convergent-divergent nozzle from a large chamber in which the pressure and temperature are 200 kPa and 310 K, respectively. A normal shock wave occurs at a point in the nozzle where the Mach number is 2.5. The air is then brought to rest in a second large chamber. Find the pressure and temperature in this second chamber. Clearly state the assumptions you have made in arriving at the solution.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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16. Air is expanded through a convergent-divergent nozzle from a large chamber in
which the pressure and temperature are 200 kPa and 310 K, respectively. A normal
shock wave occurs at a point in the nozzle where the Mach number is 2.5. The air is
then brought to rest in a second large chamber. Find the pressure and temperature
in this second chamber. Clearly state the assumptions you have made in arriving
at the solution.
Transcribed Image Text:16. Air is expanded through a convergent-divergent nozzle from a large chamber in which the pressure and temperature are 200 kPa and 310 K, respectively. A normal shock wave occurs at a point in the nozzle where the Mach number is 2.5. The air is then brought to rest in a second large chamber. Find the pressure and temperature in this second chamber. Clearly state the assumptions you have made in arriving at the solution.
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