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

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

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Compressors, Gas Turbines and Jet Engines
Intercooling in gas turbines

Decreases net output but increases thermal efficiency
Decreases net output and thermal efficiency both
Increases net output and thermal efficiency both
Increases net output but decreases thermal efficiency

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