Wake-Induced Boundary Layer Transition in a Low-Speed Axial Compressor

Flow, Turbulence and Combustion

Volumn 69, Issue 3-4, 2002, Pages 271-294

  Mailach, Ronald ^a   Vogeler, Konrad ^a  

^a DRESDEN UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

Axial compressor; Boundary layer; Turbomachine; Unsteady flow; Wake induced transition

Indexed keywords

AXIAL FLOW TURBOMACHINERY; BOUNDARY LAYER FLOW; COMPRESSORS; LAMINAR FLOW; REYNOLDS NUMBER; STATORS; TURBOMACHINE BLADES; UNSTEADY FLOW;

AXIAL COMPRESSORS; VELOCITY DISTRIBUTION;

WAKES;

EID: 0345358642     PISSN: 13866184     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1027398920038     Document Type: Article

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