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Compressors, Gas Turbines and Jet Engines

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

Lower at low speed
Same at all altitudes
Higher at high speed
Higher at high altitudes

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

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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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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

None of these
Axial flow type
Centrifugal type
Radial flow type

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

1500°C
2000°C
700°C
1000°C

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

Constant speed unloader
Relief valve
Variable speed
Start-stop motor

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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