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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during

Isentropic compression
Polytropic compression
Isothermal compression
None of these

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

in the center
between ~ to i of the blade height
at the base
at the tip

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Compressors, Gas Turbines and Jet Engines
The volume of air sucked by the compressor during its suction stroke is called

Free air delivery
None of these
Compressor capacity
Swept volume

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

Maximum work output
Decrease of heat loss in exhaust
Reduction in compressor work
High thermal efficiency

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

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

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Compressors, Gas Turbines and Jet Engines
Stalling of blades in axial flow compressor is the phenomenon of

Unsteady periodic and reversed flow
Air stream not able to follow the blade contour
Air stream blocking the passage
Motion of air at sonic velocity

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