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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

None of the listed here
Radial
Forward curved
Backward curved

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Compressors, Gas Turbines and Jet Engines
A rotary compressor is driven by an

Engine
Either (A) or (B)
Electric motor
None of these

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases
Increases/decreases depending on compressor capacity
Decreases
Remains same

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Compressors, Gas Turbines and Jet Engines
The air power of the compressor is also known as

Indicated power
Frictional power
Brake power
None of these

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Compressors, Gas Turbines and Jet Engines
The work ratio of a gas turbine plant is defined as the ratio of

Actual heat drop and isentropic heat drop
Net work output and work done by turbine
Net work output and heat supplied
Net work output and isentropic heat drop

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

10 kg/cm²
16 kg/cm²
6 kg/cm²
25 kg/cm²

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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