Role of blade passage flow structures in axial compressor rotating stall inception

Journal of Turbomachinery

Volumn 121, Issue 4, 1999, Pages 735-742

  Hoying, D A ^a   Tan, C S ^b   Vo, Huu Due ^b   Greitzer, E M ^c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Massachusetts Institute of Technology   (United States)

^c MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL COMPRESSOR; BLADE; COMPUTATIONAL FLUID DYNAMICS; THREE-DIMENSIONAL FLOW;

EID: 0033209720     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2836727     Document Type: Article

References (22)

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