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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases
Remains same
Decreases
Increases/decreases depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Pressures across the turbine
Inlet pressure to exhaust pressure
Highest pressure to exhaust pressure
Compressor pressure ratio

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Work done by turbine and heat supplied
Net work output and work done by turbine
Work done by turbine and net work output
Net work output and heat supplied

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Axial flow compressors
Radial flow compressors
All of these
Pumps

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Compressors, Gas Turbines and Jet Engines
In turbo fan engine, the jet velocity as compared to turbojet engine is

Same
May be less or more depending upon speed
More
Less

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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