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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the ratio of the ________ to the blade velocity is called slip factor.

Outlet whirl velocity
Outlet velocity of flow
Inlet velocity of flow
Inlet whirl velocity

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

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

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Enables compression in two stages
Cools the delivered air
Results in saving of power in compressing a given volume to given pressure
Is the standard practice for big compressors

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in flow and decrease in efficiency
Increase in efficiency
Increase in flow
Decrease in flow

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Compressors, Gas Turbines and Jet Engines
If the clearance ratio for a reciprocating air compressor is 'K', then its volumetric efficiency is given by

1 + k - k (p₂/p₁)1/n
1 + k - k (p₂/p₁) n-1/n
1 - k + k (p₁/p₂) n- 1/n
1 - k + k (p₁/p₂)1/n

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

Decreases
Increases
First increases and then decreases
First decreases and then increases

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