Wind-tunnel study on a 65-deg delta wing at sideslip

Journal of Aircraft

Volumn 40, Issue 2, 2003, Pages 290-296

  Verhaagen, N G ^a   Jobe, C E ^b  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; HYSTERESIS; VORTEX FLOW; WIND TUNNELS; WINGS;

SIDESLIP;

FIGHTER AIRCRAFT;

EID: 0037365750     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3092     Document Type: Article

References (14)

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4. Verhaagen, N. G., "Effect of Sideslip on the Flow over a 65-deg Delta Wing," AIAA Paper 2000-0977, Jan. 2000.
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