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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At average speed
At very slow speed
At zero speed
At very high speed

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Compressed air
Standard air
Compressed air at delivery pressure
Free air

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Compressors, Gas Turbines and Jet Engines
In a jet engine, the air-fuel ratio is

1.6673611111111
1.2506944444444
2.5006944444444
2.0840277777778

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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 ratio
Compressor efficiency
Compression index
Mean effective pressure

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Compressors, Gas Turbines and Jet Engines
In gas turbines, high thermal efficiency is obtained in

Closed cycle
Open cycle
Closed cycle & Open cycle
Closed/open depending on other considerations

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Ramjet engine
Chemical rocket engine
Gas turbine engine equipped with a propulsive nozzle and diffuse
A propeller system

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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