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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
Stainless steel
High nickel alloy
High alloy steel

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Compression ratio
Pressure ratio
None of these
Work ratio

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine may be improved by

Decreasing the compression work
Both (A) and (C) above
Increasing the turbine work
Increasing the compression work

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

kg/m³
m³/min
m³/kg
kg/m²

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Ramjet engine
A propeller system
Gas turbine engine equipped with a propulsive nozzle and diffuse
Chemical rocket engine

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

5%
0.1%
1.0%
0.5%

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