A converging diverging nozzle is supplied by air from large reservoir where the temperature is 400K. The velocity at inlet section is 120m/s. A normal shock wave stands at the diverging part of the nozzle where the cross-sectional area is twice the area at inlet. The exit cross-sectional area of the nozzle is four times the inlet cross-sectional area. If the nozzle discharges to an ambient pressure of 100kPa, determine the pressure in the reservoir. Also find the stagnation pressure and stagnation temperature at the exit plane.
A converging diverging nozzle is supplied by air from large reservoir where the temperature is 400K. The velocity at inlet section is 120m/s. A normal shock wave stands at the diverging part of the nozzle where the cross-sectional area is twice the area at inlet. The exit cross-sectional area of the nozzle is four times the inlet cross-sectional area. If the nozzle discharges to an ambient pressure of 100kPa, determine the pressure in the reservoir. Also find the stagnation pressure and stagnation temperature at the exit plane.
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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Using isentropic and normal shock tables

Transcribed Image Text:A converging diverging nozzle is supplied by air from large reservoir where the
temperature is 400K. The velocity at inlet section is 120m/s. A normal shock wave stands at
the diverging part of the nozzle where the cross-sectional area is twice the area at inlet. The
exit cross-sectional area of the nozzle is four times the inlet cross-sectional area. If the nozzle
discharges to an ambient pressure of 100kPa, determine the pressure in the reservoir. Also
find the stagnation pressure and stagnation temperature at the exit plane.
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