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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In gas turbines, high thermal efficiency is obtained in

Open cycle
Closed cycle
Closed/open depending on other considerations
Closed cycle & Open cycle

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

1.3 kg
0.5 kg
1.0 kg
2.2 kg

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Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

Multi cylinder engine
Gas turbine
4-stroke diesel engine
4-stroke petrol engine

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Compressors, Gas Turbines and Jet Engines
The performance of air compressor at high altitudes will be ________ as compared to that at sea level.

Lower
None of these
Higher
Same

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

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

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

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

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