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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/decreases depending on compressor capacity
Increases
Remains same
Decreases

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Compressors, Gas Turbines and Jet Engines
Propulsion efficiency of the following order is obtained in practice

0.72
0.34
0.5
0.6

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Increases the turbine work
Increases the thermal efficiency
Increases the compressor work
Decreases the thermal efficiency

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Compressors, Gas Turbines and Jet Engines
The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

Less than
None of these
Equal to
More than

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Compressors, Gas Turbines and Jet Engines
The performance of air compressor at high altitudes will be ________ as compared to that at sea level.

Same
None of these
Lower
Higher

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

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

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