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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Increases the thermal efficiency
Increases the turbine work
Decreases the thermal efficiency
Increases the compressor work

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Impeller inlet radius
Diffuser inlet radius
Diffuser outlet radius
Impeller outlet radius

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Net work output and work done by turbine
Net work output and heat supplied
Work done by turbine and net work output
Work done by turbine and heat supplied

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

30 bar
50 bar
20 bar
10 bar

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

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