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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.048611111111111
0.043055555555556
0.00070833333333333
0.045138888888889

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Compressors, Gas Turbines and Jet Engines
A large clearance volume in a reciprocating compressor results in

Lower suction pressure
Reduced volume flow rate
Increased volume flow rate
Lower delivery pressure

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

Carbon steel
Stainless steel
High nickel alloy
High alloy steel

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Compressors, Gas Turbines and Jet Engines
The volume of air sucked by the compressor during its suction stroke is called

Swept volume
Compressor capacity
Free air delivery
None of these

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isothermally
Isochronically
Adiabatically
Isentropically

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the branch connections from compressed air lines should be taken from

Top side of main
Left side of main
Right side of main
Bottom side of main

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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