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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Both (A) and (B) above
Decrease of thermal efficiency
Decrease of work ratio
Increase of work ratio

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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
Pressure ratio
Work ratio
None of these

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Compressors, Gas Turbines and Jet Engines
The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is

150 KW
6000 KW
15 KW
600 KW

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Reciprocating pump
Turbine
Centrifugal pump
Sliding vane compressor

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

After receiver
After inter-cooler
Before inter-cooler
Between after-cooler and air receiver

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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

0.042361111111111
0.084027777777778
0.16736111111111
0.045833333333333

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