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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compression ratio in a gas turbine is of the order of

0.20902777777778
3.5 : 1
0.33402777777778
0.50069444444444

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Compressors, Gas Turbines and Jet Engines
The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

More than
Equal to
None of these
Less than

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Compressors, Gas Turbines and Jet Engines
An air compressor may be controlled by

Throttle control
Blow off control
Clearance control
Any one of the above

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

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

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Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.00070833333333333
0.048611111111111
0.045138888888889
0.043055555555556

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Compressors, Gas Turbines and Jet Engines
The ratio of work done per cycle to the swept volume in case of compressor is called

Compression index
Mean effective pressure
Compression ratio
Compressor efficiency

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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