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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

16 kg/cm²
10 kg/cm²
6 kg/cm²
25 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

First decreases and then increases
Decreases
Increases
Remain constant

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

Higher heating value
Lower heating value
Heating value
Higher calorific value

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Joule cycle
Ericsson cycle
Rankine cycle
Carnot cycle

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

Isothermally
Isentropically
Adiabatically
Isochronically

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

1.2506944444444
2.5006944444444
1.6673611111111
2.0840277777778

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