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

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

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Compressors, Gas Turbines and Jet Engines
Intercooling in gas turbines

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

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