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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Decreases
Remain unaffected
Increases
May increase or decrease depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Enables compression in two stages
Cools the delivered air
Results in saving of power in compressing a given volume to given pressure
Is the standard practice for big compressors

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Compressors, Gas Turbines and Jet Engines
In air breathing jet engine, the jet is formed by expanding

Solids
Highly heated atmospheric air
Plasma
Liquid

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Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is perpendicular to its axis, then it is a

Reciprocating compressor
Axial flow compressor
Turbo compressor
Centrifugal compressor

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Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

None of the listed here
Discharge pressure
Critical pressure
Back pressure

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller at back
No propeller
Propeller on the top
Propeller in front

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