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Compressors, Gas Turbines and Jet Engines

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

6000 KW
15 KW
150 KW
600 KW

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

None of these
Multistage compression without intercooling
Single stage compression
Multistage compression with intercooling

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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

High
Same
Low/high depending on make and type
Low

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

0.5 kg
1.0 kg
1.3 kg
2.2 kg

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Decreases
First decreases and then increases
Increases
Remain constant

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Reciprocating pump
Centrifugal pump
Turbine
Sliding vane compressor

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