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Consider a flow of air into a converging nozzle with a mass flow rate of 1.8kg/s and the entrance area is 12cm² and the exit area is 6cm². The stagnation temperature is 500K and the pressure at exit was measured as 260kPa. Calculate the net thrust ratio acting on the nozzle.

Consider a flow of air into a converging nozzle with a mass flow rate of 1.8kg/s and the entrance area is 12cm² and the exit area is 6cm². The stagnation temperature is 500K and the pressure at exit was measured as 260kPa. Calculate the net thrust ratio acting on 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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Using isentropic tables
Consider a flow of air into a converging nozzle with a mass flow rate of 1.8kg/s and the entrance area is 12cm² and the exit area is 6cm². The stagnation temperature is 500K and the pressure at exit was measured as 260kPa. Calculate the net thrust ratio acting on the nozzle.
Transcribed Image Text:Consider a flow of air into a converging nozzle with a mass flow rate of 1.8kg/s and the entrance area is 12cm² and the exit area is 6cm². The stagnation temperature is 500K and the pressure at exit was measured as 260kPa. Calculate the net thrust ratio acting on the nozzle.
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