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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In two phases
In three phases
In the form of air and water mixture
In a single phase

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Increase
Decrease
Other factors control it
Remain unaffected

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

500°C
1000°C
700°C
200°C

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Polytropic
Isothermal
Adiabatic
None of these

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Control fire hazards
Increase efficiency
Control output of turbine
Control temperature

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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

Higher
Can't be compared
Equal
Lower

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