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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

Same
More
Zero
Less

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Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Pressure coefficient
Degree of reaction
Slip factor
Pressure ratio

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature

0.001
0.01
0.05
0.005

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

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

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

Velocity factor
Velocity coefficient
None of these
Slip factor

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

Provides greater flexibility
Provides lesser flexibility
In never used
Is used when gas is to be burnt

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