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Compressors, Gas Turbines and Jet Engines

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

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

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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

Turbo compressor
Centrifugal compressor
Axial flow compressor
Reciprocating compressor

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is bulky
It is inefficient
None of these
It requires cooling water for its operation

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Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating air compressor, without clearance, the compression of air may be

Isothermal
Isentropic
Any one of these
Polytropic

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Increase efficiency
Control output of turbine
Control temperature
Control fire hazards

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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