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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

10 kg/cm²
14.7 kg/cm²
2 kg/cm²
6 kg/cm²

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

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Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

Zero
Less
Same
More

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

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

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Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

None of the listed here
Back pressure
Critical pressure
Discharge pressure

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Increase of work ratio
Decrease of work ratio
Both (A) and (B) above
Decrease of thermal efficiency

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