First look into effects of discrete midspan vortex injection on wing performance

Journal of Aircraft

Volumn 41, Issue 5, 2004, Pages 1177-1182

  Nikolic, Vojin R ^a,c   Jumper, Eric J ^b,c  

^a MINNESOTA STATE UNIVERSITY   (United States)

^b UNIVERSITY OF NOTRE DAME   (United States)

^c Department of Mechanical Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIR NAVIGATION; COMPUTATIONAL GEOMETRY; COMPUTER AIDED ANALYSIS; MATHEMATICAL MODELS; TURBULENCE; WAKES; WIND TUNNELS; WINGS;

ANGLE OF ATTACK; DISCRETE MIDPSAN VORTEX INJECTION; WING MODEL SPAN; ZERO LIFT DRAG;

VORTEX FLOW;

EID: 7544223756     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.3888     Document Type: Article

References (6)

1. Nikolic, V. R., and Jumper, E. J., "Atanuation of Airplane Wake Vortices by Excitation of Far-Field Instability," AIAA Paper 93-3511, Aug. 1993.
2. Nikolic, V. R., "A Study of the Development and Attenuation of Wing-Generated, Vortical Wakes," Ph.D. Dissertation, Dept of Aerospace and Mechanical Engineering, Univ. of Notre Dame, Notre Dame, IN, March 1993.
3. Rossow, V. J., "Lift-Generated Vortex Wakes of Subsonic Aircraft," Progress in Aerospace Sciences, Vol. 35, 1999, pp. 507-660.
4. Rossow, V. I., "Prospects for Alleviation of Hazard Posed by Lift-Generated Wakes," Proceedings of the Aircraft Wake Vortices Conference, Vol. 1, Federal Aviation Administration, Rept. DOT/FAA/SB-92/1.1, DOT-VNTSC-FAA-92-7.1, Dept of Transportation, Washington, DC, 29-31 Oct. 1991, p. 22-1-22-40.
5. Abbot, I. H., and von Doenhoff, A. E., Theory of Wing Sections, Dover, New York, 1959, pp. 488-489.
6. Barlow, J. B., Rae, W. H., Jr., and Pope, A., Low-Speed Wind Tunnel Testing, 3rd ed., Wiley, New York, 1999, p. 227.