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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Work ratio
Compression ratio
Pressure ratio
None of these

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Compressors, Gas Turbines and Jet Engines
Surging is the phenomenon of

Air stream blocking the passage
Unsteady, periodic and reversed flow
Air stream not able to follow the blade contour
Motion of air at sonic velocity

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In the form of air and water mixture
In two phases
In a single phase

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

0.5%
0.1%
5%
1.0%

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Axial flow compressors
All of these
Pumps
Radial flow compressors

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Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Impeller channel losses
Inlet losses
Diffuser losses
All of the listed here

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