3Compressor12Dif fuser A portion of a turbojet engine is shown in the figure below. Air flowing at 25kg/s at 240 K and 80 kPa (State 1) enters an adiabatic and reversible diffuserwith a velocity of 250 m/s. It leaves the diffuser with negligible velocity (State2). As a result, you may assume the velocity of the air leaving the diffuser issmall compared to the velocity of air entering the diffuser. The air is thencompressed in an adiabatic compressor with an isentropic efficiency of 80%.The compressor requires 7 MW of power (work input). You may assume air isan ideal gas with constant specific heats. Use the correct specific heats in thetable below in analyzing the different processes.Air PropertiesCpCyRkJ/kgK kJ/kgKkJ/kgKDiffuser(Process 1 to 2)Compressor(Process 2 to 3)1.0030.7160.2871.0140.7270.2871. Calculate the pressure of the air in kPa leaving the compressor (State 3).

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Answered: 1. Calculate the pressure of the air in…

Engineering

Mechanical Engineering

1. Calculate the pressure of the air in kPa leaving the compressor (State 3).

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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