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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Isothermal H.P./shaft H.R
Total output/air input
Compression work/motor input
Isothermal H.P/indicated H.R

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

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

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

Centrifugal type
Axial flow type
None of these
Radial flow type

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Compressors, Gas Turbines and Jet Engines
A jet engine has

No propeller
Propeller in front
Propeller at back
Propeller on the top

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Compressors, Gas Turbines and Jet Engines
Fighter bombers use following type of engine

Rocket
Ramjet
Turbojet
Turbo-propeller

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Compressors, Gas Turbines and Jet Engines
Adiabatic compression is one in which

Temperature during compression remains constant
No heat leaves or enters the compressor cylinder during compression
Work done is maximum
Temperature rise follows a linear relationship

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