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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Lowest
Highest
Anything
Atmospheric

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in flow and decrease in efficiency
Decrease in flow
Increase in efficiency
Increase in flow

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Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Total output/air input
Compression work/motor input
Isothermal H.P/indicated H.R
Isothermal H.P./shaft H.R

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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

Higher
None of these
Same
Lower

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

Radial component
Axial component
Tangential component
None of these

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Does not change
Remain same
Decrease
Increase

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