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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

Low speeds
High altitudes
High speeds
Low altitudes

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Compressors, Gas Turbines and Jet Engines
The indicated work per unit mass of air delivered is

Greatly affected by clearance volume
Directly proportional to clearance volume
Not affected by clearance volume
Inversely proportional to clearance volume

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

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

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Better lubrication is possible advantages of multistage
Air can be cooled perfectly in between
More loss of air due to leakage past the cylinder
Mechanical balance is better

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Ericsson cycle
Carnot cycle
Rankine cycle
Joule cycle

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

10 to 15 bar
1 to 5 bar
8 to 10 bar
5 to 8 bar

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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