Vortex Flow Visualization of a Yawed Delta Wing with Leading-Edge Extension

Journal of Aircraft

Volumn 41, Issue 2, 2004, Pages 231-237

  Sohn, Myong Hwan ^a,c   Lee, Ki Young ^a,c   Chang, Jo Won ^b,c  

^a Korean Air Force Academy   (South Korea)

^b Hankuk Aviation University   (South Korea)

^c Department of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; CAMERAS; FLOW VISUALIZATION; LASER BEAMS; MATHEMATICAL MODELS; REYNOLDS NUMBER; VORTEX FLOW; WINGS;

LEADING-EDGE EXTENSION; VORTEX FLOW VISUALIZATION; WING ROOT CHORDS; WING VORTICES;

DELTA WING AIRCRAFT;

EID: 2342458328     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.9281     Document Type: Article

References (9)

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2. Olsen, P. E., and Nelson, R. C., "Vortex Interaction over Double Delta Wings at High Angles of Attack," AIAA Paper 1989-2191, July 1989.
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7. Hoeijmakers, H. W. M., Vaatstra, W., and Verhaagen, N. G., "Vortex Flow over Delta and Double-Delta Wing," Journal of Aircraft, Vol. 20, No. 9, 1983, pp. 825-832.
8. Sohn, M. H., and Lee, K. Y., "Experimental Investigation of Vortex Flow of a Yawed Delta Wing Having Leading Edge Extension," AIAA Paper 2002-3267, June 2002.
9. Sohn, M. H., and Lee, K. Y., "Effects of Sideslip on the High-Incidence Vortical Flow of a Delta Wing with the Leading Edge Extension," AIAA Paper 2003-1107, Jan. 2003.