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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature

0.005
0.05
0.01
0.001

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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 weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Same
None of these
Lower
Higher

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

All of these
Heating chamber
Compressor
Cooling chamber

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Compressors, Gas Turbines and Jet Engines
The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of

0.045833333333333
0.084027777777778
0.16736111111111
0.042361111111111

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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
Axial flow compressor
Reciprocating compressor
Centrifugal compressor

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