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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases
Increases/decreases depending on compressor capacity
Decreases
Remains same

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Compressors, Gas Turbines and Jet Engines
The thrust of a jet propulsion power unit can be increased by

All of these
Injecting ammonia into the combustion chamber
Injecting water into the compressor
Burning fuel after gas turbine

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitudes will require ___ power.

None of the listed here
More
Same
Less

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

More power
More/less power depending on other factors
Same power
Less power

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Compressors, Gas Turbines and Jet Engines
The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is

Superheating in compressor
All of these
Clearance volume and leakages
Pressure drop across the valves

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Adiabatic
Polytropic
Isothermal
None of these

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