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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

All of these
Cooling chamber
Compressor
Heating chamber

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

500°C
700°C
200°C
1000°C

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller on the top
Propeller at back
No propeller
Propeller in front

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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

1.0%
5%
0.1%
0.5%

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Net work output and heat supplied
Work done by turbine and net work output
Net work output and work done by turbine
Work done by turbine and heat supplied

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

None of these
Increases
Decreases
Has no effect on

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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