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Compressors, Gas Turbines and Jet Engines

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

Pressure coefficient
Work factor
Slip factor
Degree of reaction

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

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

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

By constantly cooling the cylinder
By insulating the cylinder
Employing inter-cooler
By running compressor at very slow speed

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

Decreases
First decreases and then increases
First increases and then decreases
Increases

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Work done by turbine and net work output
Net work output and heat supplied
Net work output and work done by turbine
Work done by turbine and heat supplied

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Compressors, Gas Turbines and Jet Engines
With the decrease in compression ratio, the volumetric efficiency

Increases
Decreases
Does not change
First decrease and then increase

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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