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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Work factor
Degree of reaction
Pressure coefficient
Slip factor

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Compressors, Gas Turbines and Jet Engines
In air breathing jet engine, the jet is formed by expanding

Solids
Liquid
Plasma
Highly heated atmospheric air

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

No air stream
One air stream
Solid fuel firing
Two or more air streams

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

Axial flow compressor
Reciprocating compressor
Turbo compressor
Centrifugal compressor

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Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Adiabatic compression
Ideal compression
Isothermal compression
Isentropic compression

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

Low weight and small frontal area
Small frontal area and high h.p.
High h.p. and low weight
High speed and high h.p.

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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