Consider an oblique shock wave with a wave angle of 36.87◦. Theupstream flow is given by M1 = 3 and p1 = 1 atm. Calculate the totalpressure behind the shock usinga. p0,2/p0,1 b. p0,2/p1 Compare the results.

Given data Oblique shock wave with a wave angle of 36.870 Upstream flow of mach with Mach no M1 = 3…

Answered: Consider an oblique shock wave with a…

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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Consider an oblique shock wave with a wave angle of 36.87◦. The
upstream flow is given by M₁ = 3 and p₁ = 1 atm. Calculate the total
pressure behind the shock using
a. p_0,2/p_0,1
b. p_0,2/p₁
Compare the results.

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