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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Isentropic compression
Polytropic compression
Isothermal compression
None of the listed here

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

Stainless steel
Carbon steel
High alloy steel
High nickel alloy

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Compressors, Gas Turbines and Jet Engines
The pressure of air at the beginning of the compression stroke is ___ the atmospheric pressure.

More than
None of the listed here
Less than
Equal to

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in gas turbines, is of

Axial flow type
Centrifugal type
None of the listed here
Radial flow type

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Compressors, Gas Turbines and Jet Engines
A jet engine has

No propeller
Propeller in front
Propeller on the top
Propeller at back

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