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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1.2
1.4
1.3
1

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To increase the output
To increase the efficiency
To save fuel
To reduce the exit temperature

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Increases the turbine work
Decreases the thermal efficiency
Increases the thermal efficiency
Increases the compressor work

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Compression of inlet air
Reduction of speed of incoming air and conversion of part of it into pressure energy
Lost work
Increasing speed of incoming air

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency, even when running at high speed, can be approached by using

Multistage compression
Fully insulating the cylinder
Cold water spray
Both (A) and (B) above

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Results in saving of power in compressing a given volume to given pressure
Enables compression in two stages
Cools the delivered air
Is the standard practice for big compressors

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