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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

700°C
1500°C
2000°C
1000°C

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

Compressor capacity
Swept volume
Free air delivery
None of the listed here

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

Decreases
Remain constant
Increases
First decreases and then increases

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To cool the air during compression
To enable compression in two stages
To minimize the work of compression
To cool the air at delivery

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Compressors, Gas Turbines and Jet Engines
The efficiency of roots blower ________ with the increase in pressure ratio.

None of these
Increases
Does not change
Decreases

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

Isothermal
None of these
Adiabatic
Polytropic

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