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Compressors, Gas Turbines and Jet Engines

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

Plasma
Highly heated atmospheric air
Liquid
Solids

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

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

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the ratio of the ________ to the blade velocity is called slip factor.

Inlet whirl velocity
Outlet velocity of flow
Outlet whirl velocity
Inlet velocity of flow

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Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Polytropic compression
None of the listed here
Isentropic compression
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

May be less or more depending on ambient conditions
Same
More
Less

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

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

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