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Compressors, Gas Turbines and Jet Engines

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

Same
Higher
Lower
None of these

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Compressors, Gas Turbines and Jet Engines
Out of the following, from where you will prefer to take intake for air compressor

From coal yard side
From an air conditioned room maintained at 20°C
From outside atmosphere at 1°C
From a side where cooling tower is located nearby

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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
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Work factor
Pressure coefficient
Degree of reaction
Slip factor

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Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Decreases heat loss is exhaust
Allows operation at very high altitudes
Increases thermal efficiency
Allows high compression ratio

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Compressors, Gas Turbines and Jet Engines
Surging is the phenomenon of

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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