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Compressors, Gas Turbines and Jet Engines

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

Turbo compressor
Centrifugal compressor
Axial flow compressor
Reciprocating compressor

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isothermally
Isentropically
Adiabatically
Isochronically

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

In never used
Is used when gas is to be burnt
Provides greater flexibility
Provides lesser flexibility

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Compressors, Gas Turbines and Jet Engines
The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the

Adiabatic temperature drop in the stage
Total temperature drop in the stage
Total temperature drop
Total adiabatic temperature drop

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

200°C
500°C
700°C
1000°C

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

Its own oxygen
Surrounding air
Compressed atmospheric air
None of these

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