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Air enters a convergent-divergent nozzle having a throat area of 930 cm2 and attains a Mach number of 2.5 at the exit. The supply air is a pressure of 1.05 bar and a temperature of 21 °Cand is having negligible velocity. Find the mass flow rate, area and fluid properties (p, T, gand v) at the exit of the nozzle.

Air enters a convergent-divergent nozzle having a throat area of 930 cm2 and attains a Mach number of 2.5 at the exit. The supply air is a pressure of 1.05 bar and a temperature of 21 °Cand is having negligible velocity. Find the mass flow rate, area and fluid properties (p, T, gand v) at the exit of the nozzle.

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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Air enters a convergent-divergent nozzle having a throat area of 930 cm? and attains a Mach number of 2.5 at the exit. The supply air is a pressure of 1.05 bar and a temperature of 21 °Cand is having negligible velocity. Find the mass flow rate, area and fluid properties (p, T, pand v) at the exit of the nozzle.
Transcribed Image Text:Air enters a convergent-divergent nozzle having a throat area of 930 cm? and attains a Mach number of 2.5 at the exit. The supply air is a pressure of 1.05 bar and a temperature of 21 °Cand is having negligible velocity. Find the mass flow rate, area and fluid properties (p, T, pand v) at the exit of the nozzle.
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