NASA NTRS · 20080004001
Rotating stall suppression
Abstract
Rotating stall in an axial-flow compressor is suppressed by the positioning of a fixed inlet flow divider in the annular inlet flow passage upstream of the compressor. The inlet flow divider is aligned with the flow of fluid through the duct and acts to block or interfere with any rotating wave in the inlet and thereby suppresses rotating stall in the compressor.
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Moore, Franklin K.. 1994-03-29. Rotating stall suppression. https://ntrs.nasa.gov/citations/20080004001
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