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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

1000°C
1500°C
700°C
2000°C

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Compressors, Gas Turbines and Jet Engines
What will be the volume of air at 327°C if its volume at 27°C is 1.5 m³/ mt?

18 m³/ mt.
3 m³/ mt.
1.5 m³/ mt.
6 m³/ mt.

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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

Mean effective pressure
Compression ratio
Compression index
Compressor efficiency

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

Two or more air streams
One air stream
No air stream
Solid fuel firing

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Lower volumetric efficiency
Less power requirement
Better mechanical balance
Less loss of air due to leakage past the cylinder

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

To cool the air during compression
To minimize the work of 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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