New pair of leading-edge vortex structure for flow over delta wing

Journal of Aircraft

Volumn 42, Issue 3, 2005, Pages 718-721

  Wang, Jinjun ^a,b   Zhan, Jingxia ^a,b  

^a BEIHANG UNIVERSITY   (China)

^b Fluid Mechanics Institute   (China)

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; RESEARCH; REYNOLDS NUMBER; SURFACES; VISUALIZATION; VORTEX FLOW;

DELTA WING; FLOW STRUCTURES; SHEAR LAYERS; SWEEPBACK ANGLE;

WIND TUNNELS;

EID: 22544486305     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.9929     Document Type: Article

References (9)

1. Kegelman, J., and Roos, F., "Effects of Leading-Edge Shape and Vortex Burst on the Flow Field of a 70 Degree Sweep Delta Wing," AIAA Paper 89-0086, Jan. 1989.
2. Miau, J. J., Kuo, K. T., Liu, W. H., Hsieh, S. J., and Chou, J. H., "Flow Developments Above 50-Deg Sweep Deita Wings with Different Leading-Edge Profiles," Journal of Aircraft, Vol. 32, No. 4, 1995, pp. 787-794.
3. Taylor, G.S., Schnorbus, T., and Gursul, I., "An Investigation of Vortex Flows over Low Sweep Delta Wings," AIAA Paper 2003-4021, June 2003.
4. Polhamus, E. C., "Predictions of Vortex-Lift Characteristics by Leading-Edge Suction Analogy," Journal of Aircraft, Vol. 8, No. 4, 1971, pp. 193-199.
5. Pelletier, A., and Nelson, R. C., "An Experimental Study of Static and Dynamic Vortex Breakdown on Slender Delta Wing Planforms," AIAA Paper 94-1879-CP, June 1994.
6. Ericsson, L. E., and King, H. H. C., "Effect of Leading-Edge Geometry on Delta Wing Unsteady Aerodynamics," Journal of Aircraft, Vol. 30, No. 5, 1992, pp. 793-795.
7. Ericsson, L. E., "Effect of Leading-Edge Cross-Sectional Shape on Nonslender Wing Rock," Journal of Aircraft, Vol. 40, No. 2, 2003, pp. 407-410.
8. Huang, X. Z., Sun, Y. Z., and Hanff, E. S., "Further Investigations of Leading-Edge Vortex Breakdown over Delta Wings," AIAA Paper 97-2263, June 1997.
9. Wang, J. J., Miao, F. Y., Niu, Z. N., Xue, Q. Z., and Feng, Y. N., "The Effect of Reynolds Number on Delta Wing Flow," Journal of Experimental Mechanics, Vol. 13, No. 4, 1998, pp. 497-501 (in Chinese).