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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

None of the listed here
Isentropic compression
Polytropic compression
Isothermal compression

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.

None of these
Higher
Same
Lower

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

Free air delivery
Swept volume
Compressor capacity
None of the listed here

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

High h.p. and low weight
Small frontal area and high h.p.
High speed and high h.p.
Low weight and small frontal area

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