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Compressors, Gas Turbines and Jet Engines

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

Less
More
Zero
Same

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

0.4
0.2
0.3
0.5

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Isentropic compression
Isothermal compression
Adiabatic compression
Polytropic compression

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Compressors, Gas Turbines and Jet Engines
In jet engines the products of combustion after passing through the gas turbine are discharged into

Atmosphere
Discharge nozzle
Back to the compressor
Vacuum

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Compressors, Gas Turbines and Jet Engines
The work ratio of a gas turbine plant is defined as the ratio of

Net work output and heat supplied
Net work output and work done by turbine
Actual heat drop and isentropic heat drop
Net work output and isentropic heat drop

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

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

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