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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The following property is most important for material used for gas turbine blade

Creep
Corrosion resistance
Fatigue
Toughness

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Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1.4
1.3
1
1.2

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

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

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
20 bar
30 bar
50 bar

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Compressors, Gas Turbines and Jet Engines
In gas turbines, high thermal efficiency is obtained in

Closed/open depending on other considerations
Closed cycle & Open cycle
Closed cycle
Open cycle

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

in the center
at the base
between ~ to i of the blade height
at the tip

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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