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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Ratio of indicated h.p. to shaft h.p. in known as

Mechanical efficiency
Isothermal efficiency
Compressor efficiency
Volumetric efficiency

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

Maximum work output
High thermal efficiency
Decrease of heat loss in exhaust
Reduction in compressor work

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Compressors, Gas Turbines and Jet Engines
In the aircraft propellers

Its functioning does not depend on presence of air
The propulsive matter is caused to flow around the propelled body
Propulsive matter is ejected from within the propelled body
All of these

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Compressors, Gas Turbines and Jet Engines
A machine used to raise the pressure of air is called

Compressor
Gas turbine
I.C engine
Air motor

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Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Carnot cycle
Ericsson cycle
Rankine cycle
Brayton or Atkinson cycle

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Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Decrease the delivery temperature for ease in handling
Reduce volume
Cause moisture and oil vapour to drop out
Cool the air

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