Effects of leading-edge bevel angle on the aerodynamic forces of a non-slender 50° delta wing

Aeronautical Journal

Volumn 109, Issue 1098, 2005, Pages 403-407

  Wang, J J ^a   Lu, S F ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; WIND TUNNELS; WINGS;

AERODYNAMIC FORCES; DELTA WINGS; DRAG RATIO; LEADING-EDGE BEVELS;

AERODYNAMICS;

EID: 25144473913     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000000828     Document Type: Article

References (15)

1. WERLE, H. Quelques resultants experimentaux sur les ailes en fleches, aux Faibles vitesses, obtenus en tunnel hydrodynamique. La Recherché Aeronautique, 1954, 41.
2. ASHLEY, H., KATZ, J., JARRAH, M.A. and VANECK, T. Survey of research on unsteady aerodynamic loading of delta wings, J Fluid and Structures, 1991, 5, pp 363-390.
3. ROCKWELL, D. Three-dimensional flow structure on delta wings at high angle-of-attack: experimental concepts and issues, 1993, AIAA Paper 93-0550.
4. GURSUL, I. Review of unsteady vortex flows over delta wings, 2003, AIAA Paper 2003-3942.
5. EARNSHAW, P.B. Measurements of vortex-breakdown position at low speed on a series of sharp-edged symmetrical models, November 1964, ARC CP 828.
6. BARTLETT, G.E. and VIDAL, R.J. Experimental investigation of influence of edge sharp on the aerodynamic characteristics of low aspect ratio wings at low speed, J Aero Sci, 1955, 22, (8).
7. KEGELMAN, J. and ROOS, F. Effects of leading-edge shape and vortex burst on the flowfield of a 70 deg sweep delta wing, January 1989, AIAA Paper, pp 1989-0086.
8. PELLETIER, A. and NELSON, R.C. An experimental study of static and dynamic vortex breakdown on slender delta wing planforms, 1994, AIAA Paper 94-1879-CP.
9. POLHAMUS, E.C. Predictions of vortex lift characteristics by leading-edge suction analogy, J Aircr, 1971, 8, pp 193-199.
10. ERICSSON, L.E. and KING, H.H.C. Effect of leading-edge cross-sectional geometry on slender wing unsteady aerodynamics, January 1992, AIAA Paper, pp 1992-0173.
11. HUANG, X.Z., SUN, Y.Z. and HANFE, E.S. Further investigations of leading-edge vortex breakdown over delta wings, AIAA Paper, 1997, pp 1997-2263.
12. WANG, J.J. and ZHAN, J.X. A new pair of leading-edge vortex structure for flow over delta wing, J of Aircr, 2005, 2005, 42, (3), pp 718-721.
13. MIAU, J.J., KUO, K.T., LIU, W.H., HSIEH, S.J., CHOU, J.H. and LIN, C.K. Flow developments above a 50-deg sweep delta wings with different leading-edge profiles, J of Aircr, 1995, 32, (4), pp 787-794.
14. Lu, S.F. Experimental Investigations on Vortex Structures and Aerodynamics for Flow over 50 deg Sweep Delta Wings, Master thesis, Beijing University of Aeronautics and Astronautics, 2005.
15. KAWAZOE, H., NAKAMURA, Y., ONO, T. and UMHIMARU, Y. Static and total pressure distributions around a thick delta wing with rounded leading-edge, 1994, AIAA Paper, pp 1994-2321.