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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The ratio of work done per cycle to the swept volume in case of compressor is called

Compressor efficiency
Compression index
Mean effective pressure
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

at the base
at the tip
in the center
between ~ to i of the blade height

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Compressors, Gas Turbines and Jet Engines
Reciprocating air compressor is best suited for

Small quantity of air at high pressure
Large quantity of air at high pressure
Small quantity of air at low pressure
Large quantity of air at low pressure

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Zero
Same
More
Less

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

Propellers
Turbojet engine
Ramjet engine
Rockets

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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