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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

Is used when gas is to be burnt
Provides greater flexibility
In never used
Provides lesser flexibility

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

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

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated H.P. and brake H.P. is known as

Mechanical efficiency
Adiabatic efficiency
Volumetric efficiency
Isothermal efficiency

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

Adding a regenerator
Reheating
Inter cooling
All of the listed here

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Compressors, Gas Turbines and Jet Engines
A simple turbojet engine is basically

Ramjet engine
Gas turbine engine equipped with a propulsive nozzle and diffuse
A propeller system
Chemical rocket engine

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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