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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A jet engine works on the principle of conservation of

Energy
Mass
Linear momentum
Flow

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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

Slip factor
None of these
Velocity coefficient
Velocity factor

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

Equal to
Less than
None of these
More than

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

None of these
It is inefficient
It is bulky
It requires cooling water for its operation

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Compressors, Gas Turbines and Jet Engines
For supplying intermittent small quantity of air at high pressure, following compressor is best suited

Screw
Reciprocating
Centrifugal
Axial

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Electric motor
Engine
Either (A) or (B)
None of these

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