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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 5°C increase in atmospheric temperature

0.001
0.005
0.01
0.05

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

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

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Compressors, Gas Turbines and Jet Engines
The minimum work required for a three stage reciprocating air compressor is ___ the work required for each stage.

Equal to
Six times
Three times
Double

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

1500°C
700°C
1000°C
2000°C

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At zero speed
At very slow speed
At average speed
At very high speed

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High altitudes
High speeds
Low speeds
Low altitudes

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