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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

0.20902777777778
0.33402777777778
0.50069444444444
3.5 : 1

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

Toughness
Creep
Corrosion resistance
Fatigue

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Compressors, Gas Turbines and Jet Engines
Which is false statement about air receivers?

These knock out some oil and moisture
These act as reservoir to take care of sudden demands
These increase compressor efficiency
These are used to dampen pulsations

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Pumps
Radial flow compressors
All of these
Axial flow compressors

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

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

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Compressors, Gas Turbines and Jet Engines
Which of the following fuels can be used in turbojet engines?

Kerosene
Liquid hydrogen
High speed diesel oil
Methyl alcohol

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