Supersonic boundary-layer interactions with various micro-vortex generator geometries

Aeronautical Journal

Volumn 113, Issue 1149, 2009, Pages 683-697

  Lee, S ^b   Loth, E ^a  

^a University of Illinois at Urbana Champaign   (United States)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC STREAMING; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; FLOW SEPARATION; GEOMETRY; LARGE EDDY SIMULATION; VORTICITY;

DISPLACEMENT THICKNESS; MICRO VORTEX GENERATORS; MONOTONE INTEGRATED LARGE EDDY SIMULATIONS; SHOCK INTERACTIONS; SHOCK-INDUCED FLOW; STREAMWISE VORTICES; SUPERSONIC BOUNDARY LAYER; SUPERSONIC TURBULENT BOUNDARY LAYERS;

VORTEX FLOW;

EID: 74549159666     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000003353     Document Type: Article

References (18)

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