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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

After inter-cooler
Between after-cooler and air receiver
Before inter-cooler
After receiver

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

1.0%
0.5%
0.1%
5%

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

Opposite to the direction of motion of blades
Equal to zero
In the direction of motion of blades
Depending on the velocity

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Remain unaffected
Other factors control it
Decrease
Increase

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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
A compressor at high altitude will draw

Less power
More/less power depending on other factors
Same power
More power

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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