94. 6.16. Nitrogen flows through a converging-diverging nozzle designed to operate at a Mach number of 3.0. If it is subjected to an operating pressure ratio of 0.5: (a) Determine the Mach number at the exit. (b) What is the entropy change in the nozzle? (c) Compute the area ratio at the shock location. (d) What value of the operating pressure ratio would be required to move the shock to the exit?
94. 6.16. Nitrogen flows through a converging-diverging nozzle designed to operate at a Mach number of 3.0. If it is subjected to an operating pressure ratio of 0.5: (a) Determine the Mach number at the exit. (b) What is the entropy change in the nozzle? (c) Compute the area ratio at the shock location. (d) What value of the operating pressure ratio would be required to move the shock to the exit?
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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Transcribed Image Text:94. 6.16. Nitrogen flows through a converging-diverging nozzle designed to
operate at a Mach number of 3.0. If it is subjected to an operating pressure ratio
of 0.5: (a) Determine the Mach number at the exit.
(b) What is the entropy change in the nozzle?
(c) Compute the area ratio at the shock location.
(d) What value of the operating pressure ratio would be required to move the shock
to the exit?
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