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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
During peak load periods, the best method of controlling compressors is

Variable speed
Constant speed unloader
Start-stop motor
Relief valve

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Compressors, Gas Turbines and Jet Engines
The ratio of work-done per cycle to the stroke volume of the compressor is known as

Mean effective pressure
Compressor efficiency
Compression ratio
Compressor capacity

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

in the center
at the tip
between ~ to i of the blade height
at the base

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Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

Same
One sixth
One fourth
One-half

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

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

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Control output of turbine
Increase efficiency
Control temperature
Control fire hazards

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