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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

Multi cylinder engine
4-stroke petrol engine
Gas turbine
4-stroke diesel engine

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Decrease
Increase
Remain unaffected
Other factors control it

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

All of these
Pumps
Centrifugal compressor
Axial compressor

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isothermal
Isochoric
Isentropic
Adiabatic

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

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

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Compressors, Gas Turbines and Jet Engines
A centrifugal compressor works on the principle of

Conversion of pressure energy into kinetic energy
Generating pressure directly
Centripetal action
Conversion of kinetic energy into pressure energy

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