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Compressors, Gas Turbines and Jet Engines

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

Carbon steel
High nickel alloy
Stainless steel
High alloy steel

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Compressors, Gas Turbines and Jet Engines
Surging is the phenomenon of

Air stream blocking the passage
Air stream not able to follow the blade contour
Unsteady, periodic and reversed flow
Motion of air at sonic velocity

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Compressors, Gas Turbines and Jet Engines
The air-fuel ratio in gas turbines is of the order of

15: 1
7: 1
30: 1
50: 1.

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler work is known as

Work coefficient
Polytropic reaction
Slip factor
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In two cylinders
In a single cylinder on both sides of the piston
In one cylinder
In two cylinders on both sides of the piston

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio in gas turbines

Improves thermal efficiency
Do not damage turbine blades
Increases power output
Reduces exhaust temperature

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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