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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

None of these
Radial component
Axial component
Tangential component

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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

0.9
0.99
0.75
0.85

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

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

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Compressors, Gas Turbines and Jet Engines
The material commonly used for air craft gas turbine is

Duralumin
Timken, Haste alloys
Stainless steel
High alloy steel

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Compressors, Gas Turbines and Jet Engines
Open cycle gas turbine works on

Ericsson cycle
Carnot cycle
Brayton or Atkinson cycle
Rankine cycle

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Compressors, Gas Turbines and Jet Engines
What will be the volume of air at 327°C if its volume at 27°C is 1.5 m³/ mt?

18 m³/ mt.
1.5 m³/ mt.
3 m³/ mt.
6 m³/ mt.

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