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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work ratio of simple gas turbine cycle depends on

Minimum cycle temperature
Pressure ratio
All of these
Maximum cycle temperature

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

Start-stop motor
Constant speed unloader
Variable speed
Relief valve

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Decrease
Increase
None of these
Remain same

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

In never used
Provides greater flexibility
Is used when gas is to be burnt
Provides lesser flexibility

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Engine
Electric motor
None of these
Either (A) or (B)

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isochronically
Isothermally
Adiabatically
Isentropically

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