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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in flow and decrease in efficiency
Increase in efficiency
Increase in flow
Decrease in flow

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Compressors, Gas Turbines and Jet Engines
The gas in cooling chamber of a closed cycle gas turbine is cooled at

Constant pressure
Constant temperature
None of the listed here
Constant volume

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Compressors, Gas Turbines and Jet Engines
A machine used to raise the pressure of air is called

Gas turbine
Air motor
I.C engine
Compressor

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

Before inter-cooler
After receiver
After inter-cooler
Between after-cooler and air receiver

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

0.37569444444444
2.5423611111111
0.16736111111111
0.084027777777778

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

Higher calorific value
Higher heating value
Heating value
Lower heating value

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