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

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 °C and is having negligible velocity. Find the mass flow rate, area and fluid properties (p, T, pand v) at the exit of the nozzle.