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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work ratio of simple gas turbine cycle depends on

Pressure ratio
Maximum cycle temperature
Minimum cycle temperature
All of these

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Can't be compared
Equal
Higher
Lower

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Compressors, Gas Turbines and Jet Engines
The ratio of work-done per cycle to the stroke volume of the compressor is known as

Compressor capacity
Compression ratio
Compressor efficiency
Mean effective pressure

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Compressors, Gas Turbines and Jet Engines
A centrifugal compressor works on the principle of

Centripetal action
Generating pressure directly
Conversion of pressure energy into kinetic energy
Conversion of kinetic energy into pressure energy

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Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.4
0.3
0.5
0.2

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

In between isothermal and adiabatic
Better than isothermal and adiabatic
Same as isothermal
Same as adiabatic

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