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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Higher
None of these
Lower
Same

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

No flow of air
Fixed mass flow rate regardless of pressure ratio
Increased inclination of chord with air steam
Reducing mass flow rate with increase in pressure ratio

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Compressors, Gas Turbines and Jet Engines
The axial flow compressor is preferred in aircraft gas turbines because of

None of the listed here
High pressure rise
Higher thrust
Low frontal area

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

Velocity factor
None of these
Velocity coefficient
Slip factor

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

1.4
1
1.2
1.3

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