Management of “counter-rotating structures over a delta wing”

AIAA Journal

Volumn 35, Issue 4, 1997, Pages 758-759

  Gursul, Ismet ^a  

^a University of Cincinnati   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85008306719     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.175     Document Type: Note

References (10)

1. Hubner, J. P., and Komerath, N. M., “Counter-Rotating Structures over a Delta Wing,” AIAA Journal, Vol. 34, No. 9, 1996, pp. 1958-1960.
2. Gursul, I., “Unsteady Flow Phenomena over DeltaWings at High Angle of Attack,” AIAA Journal, Vol. 32, No. 2, 1994, pp. 225-231.
3. Wentz, W. H., and Kohlman, D. L., “Vortex BreakdownonSlenderSharp- EdgedWings,” Journal of Aircraft, Vol. 8, No. 3, 1971, pp. 156-161.
4. Thompson, D. H., “A Water Tunnel Study of Vortex Breakdown over Wings with Highly Swept Leading Edges,” Australian Research Labs., Note ARL/A356, 1975.
5. Wolffelt, K.W., “Investigationon theMovement ofVortexBurst Position with Dynamically Changing Angle of Attack for a Schematic Delta Wing in a Water Channel with Correlation to Similar Studies in Wind Tunnel,” Aerodynamic and Related Hydrodynamic Studies Using Water Facilities, AGARD-CP-413, 1987.
6. Earnshaw, P. B., and Lawford, J. A., “ Low-Speed Wind-Tunnel Experiments on a Series of Sharp-Edged Delta Wings,” Pt. 1, Royal Aircraft Establishment, RAE TN, Aero. 2780, 1961.
7. Erickson, G. E., “Water-Tunnel Studies of Leading-EdgeVortices,” Journal of Aircraft, Vol. 19, No. 9, 1982, pp. 442-448.
8. Garg, A. K., and Leibovich, S., “ SpectralCharacteristics ofVortex Breakdown Flow elds,” Physics of Fluids, Vol. 22, No. 11, 1979, pp. 2053-2064.
9. Roos, F.W., and Kegelman, J. T., “ Recent Explorations of Leading Edge Vortex Flow elds,” NASA High-Angle-of-Attack TechnologyConf., NASA Langley Research Center, Hampton, VA, Oct.-Nov. 1990.
10. Visbal, M. R., “ Computational and Physical Aspects of Vortex Breakdown on Delta Wings,” AIAA Paper 95-0585, Jan. 1995.