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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Remain constant
Decreases
First decreases and then increases
Increases

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Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating air compressor, without clearance, the compression of air may be

Polytropic
Isothermal
Isentropic
Any one of these

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Compressors, Gas Turbines and Jet Engines
The axial flow compressor is preferred in aircraft gas turbines because of

Higher thrust
High pressure rise
Low frontal area
None of the listed here

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Compressors, Gas Turbines and Jet Engines
In the aircraft propellers

Propulsive matter is ejected from within the propelled body
Its functioning does not depend on presence of air
All of these
The propulsive matter is caused to flow around the propelled body

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Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Isothermal H.P./shaft H.R
Compression work/motor input
Total output/air input
Isothermal H.P/indicated H.R

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Compressors, Gas Turbines and Jet Engines
Which of the following fuels can be used in turbojet engines?

High speed diesel oil
Liquid hydrogen
Kerosene
Methyl alcohol

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