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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Hydrogen
Carbon dioxide
Nitrogen
Ammonia and water vapour

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Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

None of the listed here
Forward curved
Radial
Backward curved

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Compressor
All of these
Heating chamber
Cooling chamber

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Increase
Decrease
Other factors control it
Remain unaffected

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency is

The ratio of stroke volume to clearance volume
Reciprocal of compression ratio
The ratio of the air actually delivered to the amount of piston displacement
Index of compressor performance

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Joule cycle
Carnot cycle
Ericsson cycle
Rankine cycle

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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