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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

1.0%
5%
0.5%
0.1%

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Decreased discharge temperature
Higher volumetric efficiency
All of these
Lower power consumption per unit of air delivered

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

None of these
Polytropic
Isothermal
Adiabatic

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

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

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Compressors, Gas Turbines and Jet Engines
The indicated work per unit mass of air delivered is

Directly proportional to clearance volume
Inversely proportional to clearance volume
Greatly affected by clearance volume
Not affected by clearance volume

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

0.34
0.6
0.72
0.5

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