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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
Toughness
Fatigue

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Uses surrounding air
Carries its own oxygen
Does not require oxygen
Uses compressed atmospheric air

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

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

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

All of these
Pressure ratio
Minimum cycle temperature
Maximum cycle temperature

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Compressors, Gas Turbines and Jet Engines
The axial flow compressor is preferred in aircraft gas turbines because of

None of the listed here
Low frontal area
High pressure rise
Higher thrust

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

All of these
Pumps
Centrifugal compressor
Axial compressor

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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