Vortex breakdown on slender sharp-edged wings

Journal of Aircraft

Volumn 8, Issue 3, 1971, Pages 156-161

  Wentz, W H ^a   Kohlman, D L ^b  

^a WICHITA STATE UNIVERSITY   (United States)

^b UNIVERSITY OF KANSAS   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS--WINGS AND AIRFOILS;

EID: 0015021235     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.44247     Document Type: Article

References (14)

1. Polhamus, E. C., “A Concept of the Vortex Lift of Sharp- Edge Delta Wings Based on a Leading-Edge Suction Analogy,” TN D-3767, 1966, NASA.
2. Poisson-Quinton, Ph. and Erlich, E., “Hyperlift and Balancing of Slender Wings,” TT-F-9523, Aug. 1965, NASA.
3. Earnshaw, P. B., “Measurements of Vortex-Breakdown Position at Low Speed on a Series of Sharp-Edged Symmetrical Models,” RAE TR 64047, Nov. 1964, Royal Aircraft Establishment.
4. Bird, J. D., “Tuft-Grid Surveys at Low Speeds for Delta Wings,” TN D-5045, Feb. 1969, NASA.
5. Bossel, H. H., “Stagnation Criterion for Vortex Flows,” AIAA Journal, Vol. 6, No. 6, June 1968, p. 1192.
6. So, K. L., “Vortex Phenomena in a Conical Diffuser,” AIAA Journal, Vol. 5, No. 6, June 1967, p. 1072.
7. Wentz, W. H., Jr “Wind Tunnel Investigations of Vortex Breakdown on Slender Sharp-Edged Wings,” Ph.D. thesis, 1968, Univ. of Kansas, Lawrence,. Kansas; also CR-98737, NASA.
8. Maltby, R. L. and Peckham, D. H., “Low Speed Flow Studies of the Vortex Patterns Above Inclined Slender Bodies Using a Smoke Technique,” RAE Addendum to Tech. Note Aero 2482, March 1957, Royal Aircraft Establishment.
9. Matz, D. L., “Experimental Determination of Some Characteristics of Slender Wing Vortex Sheets,” M.S. thesis, 1969, Wichita State Univ., Wichita, Kansas.
10. Polhamus, E. C., “Application of the Leading-Edge Suction Analogy of Vortex Lift to the Drag Due to Lift of Sharp-Edge Delta Wings,” TN D-4739, Aug. 1968, NASA.
11. Sacks, A. L., Lundberg, R. E., and Hanson, C. W., III “A Theoretical Investigation of the Aerodynamics of Slender Wing- Body Combinations Exhibiting Leading-Edge Separation,” CR-719, 1967, NASA.
12. Rolls, S., Koenig, D. G., and Drinkwater, F. J. “Flight Investigation of the Aerodynamic Properties of the Ogee Wing,” TN D-3071, Dec. 1965, NASA.
13. Rolls, S., “Ogee Wing Improves Low-Speed Characteristics of Deltas,” Space/Aeronautics, Dec. 1965.
14. Poisson-Quinton, Ph. and Werle, H., “Water Tunnel Visualization of Vortex Flow,” Astronautics and Aeronautics, June 1967.