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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Can be driven at a very high speed
Has more efficiency
All of the listed here
Produces uniform torque

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Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

A source at 0° C
A source of high temperature air
A source of low temperature air
The atmosphere

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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

Work ratio
Compression ratio
Pressure ratio
None of these

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Increase of work ratio
Decrease of thermal efficiency
Both (A) and (B) above
Decrease of work ratio

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Compressors, Gas Turbines and Jet Engines
Mechanical efficiency of gas turbines as compared to I.C engines is

Lower
None of these
Higher
Same

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High altitudes
Low speeds
High speeds
Low altitudes

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