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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Polytropic compression
Isentropic compression
Isothermal compression
None of the listed here

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Compressors, Gas Turbines and Jet Engines
The work ratio of simple gas turbine cycle depends on

All of these
Pressure ratio
Minimum cycle temperature
Maximum cycle temperature

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

10 to 15 bar
5 to 8 bar
1 to 5 bar
8 to 10 bar

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

Axial flow type
Radial flow type
Centrifugal type
None of the listed here

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

More
Less
Same
More/less depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Isentropic compression
Isothermal compression
Adiabatic compression
Ideal compression

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