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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Does not require oxygen
Uses surrounding air
Carries its own oxygen
Uses compressed atmospheric air

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

Flow
Mass
Linear momentum
Energy

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Compressors, Gas Turbines and Jet Engines
The material commonly used for air craft gas turbine is

High alloy steel
Duralumin
Timken, Haste alloys
Stainless steel

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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 thermal efficiency of a gas turbine as compared to a diesel plant is

Same
Depends on other factors
More
Less

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

Less than
Equal to
More than
None of these

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