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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Adiabatically
Isothermally
Isentropically
Isochronically

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

Lower heating value
Higher heating value
Higher calorific value
Heating value

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Compressors, Gas Turbines and Jet Engines
The ratio of work-done per cycle to the stroke volume of the compressor is known as

Compression ratio
Mean effective pressure
Compressor efficiency
Compressor capacity

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

30: 1
15: 1
7: 1
50: 1.

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitudes will require ___ power.

More
Same
None of the listed here
Less

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

None of these
Has no effect on
Increases
Decreases

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