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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Reduce volume
Decrease the delivery temperature for ease in handling
Cause moisture and oil vapour to drop out
Cool the air

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

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

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Compressors, Gas Turbines and Jet Engines
For speed above 3000 km/hour, it is more advantageous to use

Rockets
Ramjet engine
Propellers
Turbojet engine

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Compressors, Gas Turbines and Jet Engines
In air breathing jet engine, the jet is formed by expanding

Highly heated atmospheric air
Solids
Liquid
Plasma

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

All of the listed here
Produces uniform torque
Has more efficiency
Can be driven at a very high speed

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Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

1.03 kg/cm²
0.53 kg/cm²
1.00 kg/cm²
1.06 kg/cm²

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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