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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

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

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Compressors, Gas Turbines and Jet Engines
A turboprop is preferred to turbojet because

It has high power for take off
It can fly at high elevations
It has high propulsive efficiency at high speeds
It can fly at supersonic speeds

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Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

More
May be less or more depending on ambient conditions
Same
Less

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Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Ideal compression
Isentropic compression
Isothermal compression
Adiabatic compression

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Compressors, Gas Turbines and Jet Engines
Which of the following plants is smallest and lightest for generating a given amount of power?

Diesel engine
Gas turbine plant
Solar plant
Petrol engine

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Compressors, Gas Turbines and Jet Engines
In a closed cycle gas turbine, the air is compressed

Isentropically
None of these
Polytropically
Isothermally

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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