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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Pressure coefficient
Slip factor
Pressure ratio
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

25 kg/cm²
6 kg/cm²
10 kg/cm²
16 kg/cm²

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

No air stream
Two or more air streams
Solid fuel firing
One air stream

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

None of these
Centrifugal
Axial flow
Radial flow

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Compressors, Gas Turbines and Jet Engines
The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of

0.99
0.9
0.85
0.75

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Compressors, Gas Turbines and Jet Engines
Ramjet engine

Produces a jet consisting of plasma
Is not self operating at zero flight speed
Requires no air for its operation
Is self operating at zero flight speed

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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