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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.4
0.5
0.3
0.2

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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Same
Dependent on other factors
Higher
Lower

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

Surrounding air
Its own oxygen
Compressed atmospheric air
None of these

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

Polytropic compression
Isothermal compression
Isentropic compression
Adiabatic compression

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the branch connections from compressed air lines should be taken from

Right side of main
Top side of main
Bottom side of main
Left side of main

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In two phases
In a single phase
In three phases
In the form of air and water mixture

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