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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
In jet engines, for the efficient production of large power, fuel is burnt in an atmosphere of

Oxygen alone
Vacuum
Atmospheric air
Compressed air

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is inefficient
None of these
It requires cooling water for its operation
It is bulky

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Compressors, Gas Turbines and Jet Engines
The efficiency and work ratio of a gas turbine plant can be increased by

Reheating the air after partial expansion in the turbine
All of these
Injecting water in/around combustion chamber
Adding heat exchanger

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

All of the listed here
Inter cooling
Reheating
Adding a regenerator

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Maximum cycle temperature
Minimum cycle temperature
Pressure ratio
All of these

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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