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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

A source of high temperature air
A source at 0° C
The atmosphere
A source of low temperature air

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Compressors, Gas Turbines and Jet Engines
The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)

1 - r ɣ-1
1 - (1/r) ɣ-1/ɣ
1 - (1/r) ɣ/ɣ-1
r ɣ-1

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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.
6 m³/ mt.
3 m³/ mt.
1.5 m³/ mt.

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

Free air
Standard air
Compressed air at delivery pressure
Compressed air

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Compressors, Gas Turbines and Jet Engines
The compression ratio in a gas turbine is of the order of

0.20902777777778
0.33402777777778
3.5 : 1
0.50069444444444

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

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

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