Air is expanded from a larger reservoir in which the pressure and temperature are 500 kPa and 35°C through a variable area duct. A normal shock occurs at a point in the duct where the Mach number is 2.5. Find the pressure and temperature in the flow just downstream of the shock wave. Downstream of the shock wave, the flow is brought to rest in another large reservoir. Find the pressure and tempera- ture in this reservoir. Assume that the flow is one-dimensional and isentropic everywhere except through the shock wave.
Air is expanded from a larger reservoir in which the pressure and temperature are 500 kPa and 35°C through a variable area duct. A normal shock occurs at a point in the duct where the Mach number is 2.5. Find the pressure and temperature in the flow just downstream of the shock wave. Downstream of the shock wave, the flow is brought to rest in another large reservoir. Find the pressure and tempera- ture in this reservoir. Assume that the flow is one-dimensional and isentropic everywhere except through the shock wave.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Transcribed Image Text:Example 4
Air is expanded from a larger reservoir in which the pressure and temperature are
500 kPa and 35°C through a variable area duct. A normal shock occurs at a point
in the duct where the Mach number is 2.5. Find the pressure and temperature in
the flow just downstream of the shock wave. Downstream of the shock wave, the
flow is brought to rest in another large reservoir. Find the pressure and tempera-
ture in this reservoir. Assume that the flow is one-dimensional and isentropic
everywhere except through the shock wave.
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