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For a jet propulsion unit , ideally the compressor work and turbine work are: A equal B unequal C not related to each other D unpredictable

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Question added by Alex Al Yazouri , General Manager , Al Mushref Cooperative Society
Date Posted: 2014/12/27
Basit Ali
by Basit Ali , Director of Engineering , Laverda Suites & Villas / Blue Bay Resorts

These typically consist of an engine with a rotary (rotating) air compressor powered by a turbine with the leftover power providing thrust via a propelling nozzle.

Gas turbines are rotary engines that extract energy from a flow of combustion gas. They have an upstream compressor coupled to a downstream turbine with a combustion chamber in-between. In aircraft engines, those three core components are often called the "gas generator. There are many different variations of gas turbines, but they all use a gas generator system of some type.

D Opt

RAJ DAHIYA
by RAJ DAHIYA , Senior MEP Projects Manager , Trinity Engineering Services L.L.C.

My Opinion goes with Option D

younan abdo
by younan abdo , MECHANICAL DESIGN ENGINEER , ARCHITECTURAL & ENGINEERING CONSULTANTS

equal

Elke Woofter
by Elke Woofter , Project Assistant , American Technical Associates

my answer option D

Alex Al Yazouri
by Alex Al Yazouri , General Manager , Al Mushref Cooperative Society

 D unpredictable.

Vinod Jetley
by Vinod Jetley , Assistant General Manager , State Bank of India

A. equal, ideally.

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