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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Pick up wrong statement. Surging phenomenon in centrifugal compressor depends on

Stagnation pressure at the outlet
Pressure ratio
Change in load
Mass flow rate

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a gas turbine as compared to a diesel plant is

Same
Less
Depends on other factors
More

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

Centrifugal type
Axial flow type
None of the listed here
Radial flow type

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Engine output and propulsive power
Propulsive power and fuel input
Thrust power and fuel energy
Thrust power and propulsive power

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Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1.2
1
1.4
1.3

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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