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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a single acting reciprocating air compressor, without clearance, the compression of air may be

Polytropic
Any one of these
Isothermal
Isentropic

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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

0.00070833333333333
0.045138888888889
0.048611111111111
0.043055555555556

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Sliding vane compressor
Reciprocating pump
Centrifugal pump
Turbine

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Compressors, Gas Turbines and Jet Engines
The thrust of a jet propulsion power unit can be increased by

Injecting ammonia into the combustion chamber
Burning fuel after gas turbine
All of these
Injecting water into the compressor

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Compressors, Gas Turbines and Jet Engines
In jet engines the products of combustion after passing through the gas turbine are discharged into

Vacuum
Discharge nozzle
Back to the compressor
Atmosphere

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Pumps
All of these
Axial flow compressors
Radial flow compressors

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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