Effect of microvortex generators on separated normal shock/boundary layer interactions

Journal of Aircraft

Volumn 44, Issue 1, 2007, Pages 170-174

  Holden, H ^a,b,c   Babinsky, H ^a,b,c  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^b Engineering Department   (United Kingdom)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW SEPARATION; PRESSURE EFFECTS; REYNOLDS NUMBER; SHOCK WAVES;

BOUNDARY LAYER INTERACTION; SHOCK INDUCED SEPARATION; VORTEX GENERATORS;

VORTEX FLOW;

EID: 33847724345     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.22770     Document Type: Article

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