Air is flowing at Mach 2 at a temperature and pressure of 100 kPa and 0°C down a duct. One wall of this duct turns through an angle of 5° away from the flow lead- ing to the formation of an expansion wave. This expansion wave is reflected off the flat opposite wall of the duct. Find the pressure and temperature behind the reflected wave.

Elements Of Electromagnetics
7th Edition
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Author:Sadiku, Matthew N. O.
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3. Air is flowing at Mach 2 at a temperature and pressure of 100 kPa and 0°C down a
duct. One wall of this duct turns through an angle of 5° away from the flow lead-
ing to the formation of an expansion wave. This expansion wave is reflected off
the flat opposite wall of the duct. Find the pressure and temperature behind the
reflected wave.
Transcribed Image Text:3. Air is flowing at Mach 2 at a temperature and pressure of 100 kPa and 0°C down a duct. One wall of this duct turns through an angle of 5° away from the flow lead- ing to the formation of an expansion wave. This expansion wave is reflected off the flat opposite wall of the duct. Find the pressure and temperature behind the reflected wave.
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