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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.3
0.2
0.4
0.5

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

None of these
Less than
More than
Equal to

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

High speed and high h.p.
Small frontal area and high h.p.
Low weight and small frontal area
High h.p. and low weight

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In two phases
In the form of air and water mixture
In a single phase

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Standard air
Compressed air at delivery pressure
Free air
Compressed air

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Other factors control it
Remain unaffected
Increase
Decrease

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