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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

4-stroke petrol engine
Gas turbine
4-stroke diesel engine
Multi cylinder engine

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Axial flow
None of these
Radial flow
Centrifugal

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Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Lowest
Atmospheric
Highest
Anything

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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

Slip factor
Pressure coefficient
Work factor
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor without clearance volume, the work-done is maximum during

Polytropic compression
None of these
Isentropic compression
Isothermal compression

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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