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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Polytropic
Isothermal
Adiabatic
None of these

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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

Centrifugal compressor
Axial flow compressor
Turbo compressor
Reciprocating compressor

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

Increased inclination of chord with air steam
Reducing mass flow rate with increase in pressure ratio
No flow of air
Fixed mass flow rate regardless of pressure ratio

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

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

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Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

2 kg/cm²
6 kg/cm²
10 kg/cm²
14.7 kg/cm²

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Compressors, Gas Turbines and Jet Engines
In a closed cycle gas turbine, the air is compressed

Polytropically
Isentropically
Isothermally
None of these

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