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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

None of these
Velocity factor
Velocity coefficient
Slip factor

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Pressure ratio
Maximum cycle temperature
All of these
Minimum cycle temperature

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

Isentropically
Isochronically
Adiabatically
Isothermally

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Compressor
All of these
Heating chamber
Cooling chamber

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

0.2
0.4
0.3
0.5

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

2000°C
1000°C
1500°C
700°C

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