A supersonic flow at M = 3, T1 = 295 K, and pi = 3 atm is deflected upward through a compression corner with e = 30.6° and then is subsequently expanded around a corner of the same angle such that the flow direction is the same as its original direction. Calculate M3, p3, and T3 downstream of the expansion corner. (Round the final answers to two decimal places.)

A supersonic flow at M = 3, T1 = 295 K, and pi = 3 atm is deflected upward through a compression corner with e = 30.6° and then is subsequently expanded around a corner of the same angle such that the flow direction is the same as its original direction. Calculate M3, p3, and T3 downstream of the expansion corner. (Round the final answers to two decimal places.)

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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