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What is the area where the shock appears? Calculate (b) the pressure and (c) the temperature downstream of the shock.

What is the area where the shock appears? Calculate (b) the pressure and (c) the temperature downstream of the shock.

Elements Of Electromagnetics
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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e. Q3 / Air, from a reservoir at 350 K and 500 kPa, flows through a converging diverging nozzle. The throat area is 3 cm². A normal shock appears, for which the downstream Mach number is 0.6405. (a) What is the area where the shock appears? Calculate (b) the pressure and (c) the temperature downstream of the shock.
Transcribed Image Text:e. Q3 / Air, from a reservoir at 350 K and 500 kPa, flows through a converging diverging nozzle. The throat area is 3 cm². A normal shock appears, for which the downstream Mach number is 0.6405. (a) What is the area where the shock appears? Calculate (b) the pressure and (c) the temperature downstream of the shock.
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