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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

Pressure coefficient
Pressure ratio
Degree of reaction
Slip factor

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

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

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Compressors, Gas Turbines and Jet Engines
In jet engines, paraffin is usually used as the fuel because of its

Both (A) and (C) above
Low freezing point
Ease of atomisation
High calorific value

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Compressors, Gas Turbines and Jet Engines
During base load operation, the best method of controlling compressor is

Variable speed
Start-stop motor
Relief valve
Constant speed unloader

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Compressors, Gas Turbines and Jet Engines
The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called

Mechanical efficiency
Compressor efficiency
Volumetric efficiency
Isothermal efficiency

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Compressors, Gas Turbines and Jet Engines
A turboprop is preferred to turbojet because

It can fly at high elevations
It can fly at supersonic speeds
It has high power for take off
It has high propulsive efficiency at high speeds

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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