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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during

Polytropic compression
None of these
Isentropic compression
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
The fuel consumption in gas turbines is accounted for by

Lower heating value
Higher heating value
Heating value
Higher calorific value

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Blade camber
Space-chord ratio
Blade camber and space-chord ratio
Blade camber and incidence angle

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Compressors, Gas Turbines and Jet Engines
The air-fuel ratio in gas turbines is of the order of

50: 1.
15: 1
7: 1
30: 1

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Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Hydrogen
Nitrogen
Carbon dioxide
Ammonia and water vapour

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

70 to 90%
10 to 40%
40 to 60%
60 to 70%

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