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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

High alloy steel
Stainless steel
High nickel alloy
Carbon steel

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

Less than
None of these
More than
Equal to

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Mechanical balance is better
Air can be cooled perfectly in between
Better lubrication is possible advantages of multistage
More loss of air due to leakage past the cylinder

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Compressors, Gas Turbines and Jet Engines
The fuel consumption in gas turbines is accounted for by

Higher heating value
Lower heating value
Higher calorific value
Heating value

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Compressors, Gas Turbines and Jet Engines
The pressure of air at the beginning of the compression stroke is ___ the atmospheric pressure.

Equal to
None of the listed here
More than
Less than

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Compressors, Gas Turbines and Jet Engines
The compressed air may be used

All of the listed here
In starting and supercharging of I.C. engines
For operating pneumatic drills
In gas turbine plants

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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