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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Brayton or Atkinson cycle
Carnot cycle
Ericsson cycle
Rankine cycle

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Compressors, Gas Turbines and Jet Engines
For minimum work required to compress and deliver a quantity of air by multistage compression

The work-done in each stage should be same
The intercooling should be perfect
All of the listed here
The compression ratio in each stage should be same

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Compressors, Gas Turbines and Jet Engines
The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of

0.9
0.75
0.99
0.85

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

Multistage compression with intercooling
None of these
Multistage compression without intercooling
Single stage compression

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Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

Same
High
Low
Low/high depending on make and type

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Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Reduce volume
Cool the air
Cause moisture and oil vapour to drop out
Decrease the delivery temperature for ease in handling

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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