A gas turbine engine is considered in a race car design. The engine operates on two...

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Mechanical Engineering

A gas turbine engine is considered in a race car design. Theengine operates on two stages of compression with intercooling andtwo stages of expansion. The pressure ratio across each stage ofthe compressor and the turbine is 7. The air enters each stage ofthe compressor at 300K and each stage of the turbine at 1300K.Using air standard assumptions determine:

Thermal efficiency and back work ratio if no regenerator isused;
Thermal efficiency and back work ratio if a regenerator witheffectiveness of 90 % is used

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Given The engine operates on two stages ofcompression with intercooling and two stages of expansion The pressure ratio across each stageof the compressor and the turbine P2P1 7    See Answer
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