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Compressors, Gas Turbines and Jet Engines

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 coefficient
Pressure ratio
Slip factor

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Compressors, Gas Turbines and Jet Engines
For slow speed large capacity compressor, following type of valve will be best suited

Any of the above
Poppet valve
Disc or feather type
Mechanical valve of the Corliss, sleeve, rotary or semi rotary type

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

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At zero speed
At very high speed
At average speed
At very slow speed

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

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

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Compressors, Gas Turbines and Jet Engines
In the aircraft propellers

Its functioning does not depend on presence of air
The propulsive matter is caused to flow around the propelled body
All of these
Propulsive matter is ejected from within the propelled body

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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