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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

Discharge pressure
Back pressure
Critical pressure
None of the listed here

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Compressors, Gas Turbines and Jet Engines
A centrifugal compressor works on the principle of

Conversion of pressure energy into kinetic energy
Generating pressure directly
Conversion of kinetic energy into pressure energy
Centripetal action

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

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

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

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

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

Liquid
Plasma
Solids
Highly heated atmospheric air

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Same
Less
More
Zero

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