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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

500°C
700°C
200°C
1000°C

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

Increase of work ratio
Decrease of thermal efficiency
Both (A) and (B) above
Decrease of work ratio

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

Polytropic compression
Isentropic compression
None of the listed here
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Joule cycle
Rankine cycle
Ericsson cycle
Carnot cycle

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In two phases
In a single phase
In the form of air and water mixture

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Compressors, Gas Turbines and Jet Engines
For supplying intermittent small quantity of air at high pressure, following compressor is best suited

Axial
Reciprocating
Screw
Centrifugal

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