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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.3
0.4
0.2
0.5

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Compressors, Gas Turbines and Jet Engines
A rocket works with maximum overall efficiency when air craft velocity is equal to the

Twice the jet velocity
Average of the jet velocity
Jet velocity
Half the jet velocity

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Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Isentropic compression
Adiabatic compression
Ideal compression
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
Gas turbines for power generation are normally used

To enable start thermal power plant
In emergency
To supply base load requirements
To supply peak load requirements

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

m³/min
kg/m²
kg/m³
m³/kg

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

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

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