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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

Degree of reaction
Pressure coefficient
Slip factor
Work factor

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To increase the output
To save fuel
To reduce the exit temperature
To increase the efficiency

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitudes will require ___ power.

More
Same
Less
None of the listed here

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Compressors, Gas Turbines and Jet Engines
During peak load periods, the best method of controlling compressors is

Variable speed
Constant speed unloader
Relief valve
Start-stop motor

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Compressors, Gas Turbines and Jet Engines
The ratio of the volume of free air delivery per stroke to the swept volume of the piston, is known as

Compressor efficiency
Mechanical efficiency
Isothermal efficiency
Volumetric efficiency

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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