Q3:-The velocity, pressure and temperature of air flow upstream of a normal shock are 500 m/s, 100 kPa and 300 K. Determine the velocity, pressure and temperature just behind the shock and the increase of entropy caused by the shock.

Q3:-The velocity, pressure and temperature of air flow upstream of a normal shock are 500 m/s, 100 kPa and 300 K. Determine the velocity, pressure and temperature just behind the shock and the increase of entropy caused by the 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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Q3:-The velocity, pressure and temperature of air flow upstream of a normal shock are
500 m/s, 100 kPa and 300 K. Determine the velocity, pressure and temperature just behind
the shock and the increase of entropy caused by the shock.

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