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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Cause moisture and oil vapour to drop out
Cool the air
Remove impurities from air
Reduce volume of air

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isothermal
Isentropic
Isochoric
Adiabatic

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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 volume
None of the listed here
Constant temperature

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

30 bar
10 bar
20 bar
50 bar

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Can't be compared
Lower
Higher
Equal

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Minimum cycle temperature
All of these
Pressure ratio
Maximum cycle temperature

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