Question 3: Consider an ideal air-standard cycle for a gas-turbine, jet propulsion unit, such as that shown in Fig. The pressure and temperature entering the compressor are PkPa, 290 K. The pressure ratio across the compressor is 14 to 1, and the turbine inlet temperature is 1500 K. When the air leaves the turbine COMPR. BURNER TURBINE (a) Sketch the Ts diagram of the cycle. (b) Determine the velocity of the air leaving the nozzle. NOZ

Question 3: Consider an ideal air-standard cycle for a gas-turbine, jet propulsion unit, such as that shown in Fig. The pressure and temperature entering the compressor are PkPa, 290 K. The pressure ratio across the compressor is 14 to 1, and the turbine inlet temperature is 1500 K. When the air leaves the turbine COMPR. BURNER TURBINE (a) Sketch the Ts diagram of the cycle. (b) Determine the velocity of the air leaving the nozzle. NOZ

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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Step 1: Given data:

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Step 2: T-s diagram

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Step 3: Calculate the compression work done of air

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Step 4: Calculate the temp. at the outlet of the nozzle

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Step 5: Calculate the velocity at the nozzle outlet.

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