Consider an oblique shock generated at a compression corner with adeflection angle θ = 18.2◦. A straight horizontal wall is present above thecorner, as shown . If the upstream flow has the propertiesM1 = 3.2, p1 = 1 atm and T1 = 520◦R, calculate M3, p3, and T3 behindthe reflected shock from the upper wall. Also, obtain the angle whichthe reflected shock makes with the upper wall. Reflected shockStreamlineM2M1(2)Figure 9.19 Regular reflection of a shock wave from a solidboundary.Incident shock

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Answered: Reflected shock Streamline M2 M1 (2)…

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 generated at a compression corner with a
deflection angle θ = 18.2^◦. A straight horizontal wall is present above the
corner, as shown . If the upstream flow has the properties
M₁ = 3.2, p₁ = 1 atm and T₁ = 520^◦R, calculate M₃, p₃, and T₃ behind
the reflected shock from the upper wall. Also, obtain the angle which
the reflected shock makes with the upper wall.

Reflected shock
Streamline
M2
M1
(2)
Figure 9.19 Regular reflection of a shock wave from a solid
boundary.
Incident shock

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