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Compressors, Gas Turbines and Jet Engines

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isochoric
Isentropic
Isothermal
Adiabatic

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

Relief valve
Constant speed unloader
Variable speed
Start-stop motor

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In one cylinder
In two cylinders on both sides of the piston
In a single cylinder on both sides of the piston
In two cylinders

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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

None of these
Pressure ratio
Work ratio
Compression ratio

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