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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as adiabatic
Better than isothermal and adiabatic
In between isothermal and adiabatic
Same as isothermal

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Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

The atmosphere
A source at 0° C
A source of high temperature air
A source of low temperature air

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of air compressors is of the order of

70 - 90%
60 - 70%
40 - 50%
20 - 30%

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Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

Radial component
None of these
Tangential component
Axial component

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Compressors, Gas Turbines and Jet Engines
The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of

0.9
0.75
0.85
0.99

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

More
Same
Zero
Less

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