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Compressors, Gas Turbines and Jet Engines

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
Propulsion efficiency of the following order is obtained in practice

0.72
0.34
0.5
0.6

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Isothermal compression
Polytropic compression
Isentropic compression
Adiabatic compression

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Compressors, Gas Turbines and Jet Engines
The efficiency and work ratio of a gas turbine plant can be increased by

Reheating the air after partial expansion in the turbine
Adding heat exchanger
Injecting water in/around combustion chamber
All of these

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Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

More
Same
Less
Zero

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

None of these
Either (A) or (B)
Electric motor
Engine

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