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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Pressure ratio
Slip factor
Degree of reaction
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

1 bar and 20°C
0.1 bar and 20°C
0.1 bar and 40°C
1 bar and 40°C

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

1 bar
16 bar
64 bar
256 bar

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Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Cool the air
Cause moisture and oil vapour to drop out
Reduce volume of air
Remove impurities from air

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Compressors, Gas Turbines and Jet Engines
When the temperature of air leaving the inter-cooler, in a two stage compression with inter-cooler, is ________ the original atmospheric air temperature, then the intercooling is known as perfect or complete intercooling.

Equal to
More than
None of these
Less than

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Better lubrication is possible advantages of multistage
Mechanical balance is better
More loss of air due to leakage past the cylinder
Air can be cooled perfectly in between

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