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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is parallel to its axis, then the compressor is

Axial flow compressor
Reciprocating compressor
Turbo compressor
Centrifugal compressor

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

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

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Isentropic compression
Polytropic compression
Adiabatic compression
Isothermal compression

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

Carbon steel
High nickel alloy
High alloy steel
Stainless steel

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Engine output and propulsive power
Propulsive power and fuel input
Thrust power and fuel energy
Thrust power and propulsive power

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

Compressed atmospheric air
Surrounding air
Its own oxygen
None of these

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