A subsonic inlet diffuser of area ratio 3 is employed in a Mach-2 jet engine. A normal shock is formed just upstream of the inlet. The free stream pressure and temperature are 10 kPa and 300 K. Determine the Mach number, pressure and temperature at the diffuser exit. [Ans. M. = 0.16, P. = 55.4 kPa, T. = 537.8 K]

A subsonic inlet diffuser of area ratio 3 is employed in a Mach-2 jet engine. A normal shock is formed just upstream of the inlet. The free stream pressure and temperature are 10 kPa and 300 K. Determine the Mach number, pressure and temperature at the diffuser exit. [Ans. M. = 0.16, P. = 55.4 kPa, T. = 537.8 K]

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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