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Compressors, Gas Turbines and Jet Engines

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

Compressor capacity
Compression ratio
Compressor efficiency
Mean effective pressure

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Decrease
Remain same
Increase
Does not change

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Compressors, Gas Turbines and Jet Engines
The maximum propulsion efficiency of a turbojet is attained at around following speed

2400 km/hr
1050 km/hr
1700 km/hr
550 km/hr

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Impeller outlet radius
Impeller inlet radius
Diffuser inlet radius
Diffuser outlet radius

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At average speed
At very high speed
At very slow speed
At zero speed

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

Lowest
Atmospheric
Highest
Anything

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