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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
For speed above 3000 km/hour, it is more advantageous to use

Rockets
Ramjet engine
Propellers
Turbojet engine

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Cools the delivered air
Enables compression in two stages
Is the standard practice for big compressors
Results in saving of power in compressing a given volume to given pressure

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

First increases and then decreases
Decreases
Increases
Remain same

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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
0.043055555555556
0.048611111111111
0.00070833333333333

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

40 to 60%
10 to 40%
70 to 90%
60 to 70%

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Compressors, Gas Turbines and Jet Engines
With the decrease in compression ratio, the volumetric efficiency

Decreases
Does not change
First decrease and then increase
Increases

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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