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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In a single phase
In three phases
In two phases
In the form of air and water mixture

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

None of these
Polytropic compression
Isothermal compression
Isentropic compression

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Cooling chamber
Compressor
Heating chamber
All of these

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency is

The ratio of stroke volume to clearance volume
Reciprocal of compression ratio
The ratio of the air actually delivered to the amount of piston displacement
Index of compressor performance

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

2.0840277777778
2.5006944444444
1.2506944444444
1.6673611111111

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To minimize the work of compression
To cool the air during compression
To cool the air at delivery
To enable compression in two stages

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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