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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To increase the efficiency
To reduce the exit temperature
To save fuel
To increase the output

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Isentropic efficiency
Pressure coefficient
Compressor efficiency
Euler

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency, even when running at high speed, can be approached by using

Both (A) and (B) above
Cold water spray
Multistage compression
Fully insulating the cylinder

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Compressors, Gas Turbines and Jet Engines
In a closed cycle gas turbine, the air is compressed

Polytropically
Isothermally
Isentropically
None of these

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

Lower heating value
Higher calorific value
Higher heating value
Heating value

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

Decrease of thermal efficiency
Decrease of work ratio
Increase of work ratio
Both (A) and (B) above

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