Declining angle effects of the trailing edge of a microramp vortex generator

Journal of Aircraft

Volumn 47, Issue 6, 2010, Pages 2086-2095

  Li, Qin ^a,b   Liu, Chaoqun ^a,b  

^a UNIVERSITY OF TEXAS AT ARLINGTON   (United States)

^b Math Department   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; LARGE EDDY SIMULATION; VORTICITY;

ANGLE EFFECTS; MONOTONE INTEGRATED LARGE EDDY SIMULATIONS; TRAILING EDGES; VORTEX GENERATORS; WEIGHTED ESSENTIALLY NONOSCILLATORY SCHEME;

VORTEX FLOW;

EID: 79251475272     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.C000318     Document Type: Article

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