Effect of shear-layer control on leading-edge vortices

Journal of Aircraft

Volumn 33, Issue 6, 1996, Pages 1087-1093

  McCormick, S ^a   Gursul, I ^a,b  

^a UNIVERSITY OF CINCINNATI   (United States)

^b University of Cincinnati ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DELTA WING AIRCRAFT; FLOW CONTROL; REYNOLDS NUMBER; VELOCITY; WINGS;

LEADING EDGE VORTICES; SHEAR LAYER CONTROL; VORTEX BREAKDOWN; VORTEX CORE;

VORTEX FLOW;

EID: 0030289786     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.47061     Document Type: Article

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