Studies on vortex flaps having different flap hinge-line positions

Journal of Aircraft

Volumn 38, Issue 2, 2001, Pages 396-398

  Rinoie, Kenichi ^a   Kwak, Dong Youn ^a,b  

^a UNIVERSITY OF TOKYO   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; FLOW PATTERNS; LIFT; MATHEMATICAL MODELS; VORTEX FLOW; WINGS;

CROSSFLOW PATTERN; FLAP HINGE LINE POSITION; LIFT COEFFICIENTS; VORTEX FLAPS;

DELTA WING AIRCRAFT;

EID: 0035273354     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2776     Document Type: Article

References (4)

1. Rao, D. M., "Leading Edge Vortex-Flap Experiments on a 74 deg. Delta Wing," NASA CR-159161, Nov. 1979.
2. Rinoie, K., Fujita, T., Iwasaki, A., and Fujieda, H., "Experimental Studies of a 70-Degree Delta Wing with Vortex Flaps," Journal of Aircraft, Vol. 34, No. 5, 1997, pp. 600-605.
3. Rinoie, K., "Experiments of a 60-Degree Delta Wing with Rounded Leading-Edge Vortex Flaps," Journal of Aircraft, Vol. 37, No. 1, 2000, pp. 37-44.
4. Ellis, D. G., and Stollery, J. L., "The Behaviour and Performance of Leading-Edge Vortex Flaps," Proceedings of 16th Congress of the International Council of the Aeronautical Sciences, (ICAS Paper 88-4.5.2) 1988, pp. 758-765.