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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is parallel to its axis, then the compressor is

Axial flow compressor
Turbo compressor
Reciprocating compressor
Centrifugal compressor

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Compressors, Gas Turbines and Jet Engines
Cylinder clearance in a compressor should be

As small as possible
As large as possible
About 50% of swept volume
About 100% of swept volume

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

10 to 15 bar
5 to 8 bar
1 to 5 bar
8 to 10 bar

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In two cylinders
In two cylinders on both sides of the piston
In a single cylinder on both sides of the piston
In one cylinder

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Compressors, Gas Turbines and Jet Engines
The ideal efficiency of simple gas turbine cycle depends on

All of these
Minimum cycle temperature
Maximum cycle temperature
Pressure ratio

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Higher
Equal
Can't be compared
Lower

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