Q5: Air is flowing over a flat wall. The Mach number, pressure and temperature in the air stream are 3, 50kpa, and 253K respectively. If the wall turns through an angle 4° leading to formation of an oblique shock wave, find the Mach number, the pressure and the temperature in the flow behind the shock wave. (Assume weak shock)

Q5: Air is flowing over a flat wall. The Mach number, pressure and temperature in the air stream are 3, 50kpa, and 253K respectively. If the wall turns through an angle 4° leading to formation of an oblique shock wave, find the Mach number, the pressure and the temperature in the flow behind the shock wave. (Assume weak shock)

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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