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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase power output
Increase speed
Increase temperature
Reduce turbine size

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Compressors, Gas Turbines and Jet Engines
The ratio of work-done per cycle to the stroke volume of the compressor is known as

Mean effective pressure
Compression ratio
Compressor capacity
Compressor efficiency

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

Higher at high speed
Higher at high altitudes
Same at all altitudes
Lower at low speed

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Isothermal
Polytropic
None of these
Adiabatic

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Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Atmospheric
Lowest
Highest
Anything

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

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

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