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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

0.045138888888889
0.048611111111111
0.043055555555556
0.00070833333333333

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Lobe type
Reciprocating type
Centrifugal type
Axial flow type

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

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

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Compressors, Gas Turbines and Jet Engines
The efficiency of jet engine is

Higher at high altitudes
Lower at low speed
Higher at high speed
Same at all altitudes

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

By constantly cooling the cylinder
Employing inter-cooler
By insulating the cylinder
By running compressor at very slow speed

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Compressors, Gas Turbines and Jet Engines
Rotary compressors are suitable for

Low discharge at high pressure
Low discharge at low pressure
Large discharge at low pressure
Large discharge at high pressure

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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