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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

Minimum cycle temperature
All of these
Pressure ratio
Maximum cycle temperature

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

Before inter-cooler
After inter-cooler
Between after-cooler and air receiver
After receiver

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Convert kinetic energy into pressure energy
Convert pressure energy into kinetic energy
Increase velocity
Make the flow streamline

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Carnot cycle
Rankine cycle
Brayton or Atkinson cycle
Ericsson cycle

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Compressors, Gas Turbines and Jet Engines
The gas in cooling chamber of a closed cycle gas turbine is cooled at

Constant pressure
Constant temperature
None of the listed here
Constant volume

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Does not require oxygen
Uses compressed atmospheric air
Carries its own oxygen
Uses surrounding air

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