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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
Surging is the phenomenon of

Air stream not able to follow the blade contour
Unsteady, periodic and reversed flow
Motion of air at sonic velocity
Air stream blocking the passage

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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Lower
Higher
Same
Dependent on other factors

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

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

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Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Degree of reaction
Pressure ratio
Pressure coefficient
Slip factor

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

6 kg/cm²
10 kg/cm²
25 kg/cm²
16 kg/cm²

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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