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Compressors, Gas Turbines and Jet Engines

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
The compressed air may be used

In starting and supercharging of I.C. engines
For operating pneumatic drills
All of the listed here
In gas turbine plants

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

700°C
2000°C
1000°C
1500°C

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Pressure ratio
None of these
Work ratio
Compression ratio

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Cools the delivered air
Is the standard practice for big compressors
Results in saving of power in compressing a given volume to given pressure
Enables compression in two stages

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Compressors, Gas Turbines and Jet Engines
Isothermal compression though most efficient, but is not practicable because

It does not increase pressure much
It requires very big cylinder
Compressor has to run at very slow speed to achieve it
It is impossible in practice

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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