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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compression ratio in a gas turbine is of the order of

0.50069444444444
0.20902777777778
3.5 : 1
0.33402777777778

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

Minimum cycle temperature
All of these
Maximum cycle temperature
Pressure ratio

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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

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

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Ericsson cycle
Brayton or Atkinson cycle
Carnot cycle
Rankine cycle

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Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Lowest
Anything
Atmospheric
Highest

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Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Three times
Two times
Four times
Six times

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