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Compressors, Gas Turbines and Jet Engines

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

Constant speed unloader
Start-stop motor
Variable speed
Relief valve

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Compressors, Gas Turbines and Jet Engines
For perfect intercooling in a two stage compressor

p₁ = p₂ p3
p₂/p₁ = p₃/p₂
p₁ = p3
p₁/p₃ = p₂/p₁

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

0.20902777777778
3.5 : 1
0.33402777777778
0.50069444444444

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It requires cooling water for its operation
None of these
It is bulky
It is inefficient

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Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

Back pressure
None of the listed here
Discharge pressure
Critical pressure

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Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Nitrogen
Carbon dioxide
Hydrogen
Ammonia and water vapour

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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