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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

3.5 : 1
0.20902777777778
0.33402777777778
0.50069444444444

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Compressors, Gas Turbines and Jet Engines
If V, U and Vr represent the absolute velocity of fluid, velocity of blade, and relative velocity of fluid, and suffix ‘I’ and ‘o’ stand for entry and exit conditions, then in a rotary machine whose degree of reaction is unity

U < Vo
Vt > Vo
V = Uo
Vi = Vo

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

Cause moisture and oil vapour to drop out
Cool the air
Reduce volume of air
Remove impurities from air

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Impeller outlet radius
Impeller inlet radius
Diffuser inlet radius
Diffuser outlet radius

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Has compressor and combustion chamber
All of these
Requires less space for installation
Has less efficiency

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

High nickel alloy
Stainless steel
Carbon steel
High alloy steel

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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