Effect of reynolds number on the high-incidence flow over double-delta wings

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Fritzelas, A E ^a   Platzer, M F ^a   Hebbar, S K ^a  

^a NAVAL POSTGRADUATE SCHOOL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ANGLE OF ATTACK; DOPPLER EFFECT; HYDRAULIC STRUCTURES; REYNOLDS NUMBER; TUNNELS; VORTEX FLOW; WATER SUPPLY TUNNELS; WIND TUNNELS;

DOUBLE-DELTA WINGS; DYE INJECTION METHOD; HIGH ANGLE OF ATTACK; LASER DOPPLER VELOCIMETRY; PRIMARY OBJECTIVE; VORTEX BREAKDOWN; VORTEX INTERACTIONS; WIND-TUNNEL DATA;

DELTA WING AIRCRAFT;

EID: 84983209680     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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9. S.B. Kern, "Vortex Flow Control Using Fillets on a Double Delta Wing", Journal of Aircraft, Vol. 30, № 6, 1993.
10. C.H. Hsu, C.H. Liu, "Upwind Navier-Stokes Solutions for Leading Edge Vortex Flows", AIAA 89-0265, Reno, Nevada, 1989.
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12. A.E. Fritzelas, "A Water Tunnel Investigation of the Influence of Reynolds Number on the High-Incidence Flow over Double-Delta Wings", MSAE Thesis, Naval Postgraduate School, Monterey, CA, March 1996.