Computational and experimental investigation of a nonslender delta wing

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 16, Issue , 2007, Pages 10787-10810

  Gordnier, Raymond E ^a,c,d   Visbal, Miguel R ^a,c,d   Gursul, Ismet ^b,d,e   Zhijin, Wang ^b,d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF BATH   (United Kingdom)

^c Air Vehicles Directorate   (United States)

^d AIAA   (United States)

^e Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; BOUNDARY LAYERS; FLOW STRUCTURE; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; TURBULENCE; VORTEX FLOW;

BOUNDARY LAYER TRANSITIONS; SEPARATED FLOW; SURFACE FLOW FEATURES; VORTEX BREAKDOWN;

WINGS;

EID: 34250832056     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-894     Document Type: Conference Paper

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