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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Can be driven at a very high speed
Has more efficiency
Produces uniform torque
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Compression ratio
Work ratio
Pressure ratio
None of these

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

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

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Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Impeller channel losses
Inlet losses
All of the listed here
Diffuser losses

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Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

Low/high depending on make and type
High
Low
Same

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Compressors, Gas Turbines and Jet Engines
The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of

0.16736111111111
0.045833333333333
0.084027777777778
0.042361111111111

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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