Vortex breakdown over unsteady delta wings and its control

AIAA Journal

Volumn 35, Issue 3, 1997, Pages 571-574

  Yang, H ^a,b   Gursul, I ^a,b  

^a UNIVERSITY OF CINCINNATI   (United States)

^b Dept of Mech Nuclear Engineering ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DELTA WING; UNSTEADY FLOW; VORTEX BREAKDOWN;

EID: 0030958393     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.137     Document Type: Article

References (10)

1. Lee, M., and Ho, C.-M., "Lift Force of Delta Wings," Applied Mechanics Reviews, Vol. 43, No. 9, 1990, pp. 209-221.
2. Rockwell, D., "Three-Dimensional Flow Structure on Delta Wings at High Angle-of-Attack: Experimental Concepts and Issues," AIAA Paper 93-0550, Jan. 1993.
3. Visbal, M. R., "Computational and Physical Aspects of Vortex Breakdown on Delta Wings," AIAA Paper 95-0585, Jan. 1995.
4. LeMay, S. P., Batill, S. M., and Nelson, R. C., "Vortex Dynamics on a Pitching Delta Wing," Journal of Aircraft, Vol. 27, No. 2, 1990, pp. 131-138.
5. Gursul, I., and Yang, H., "Vortex Breakdown over a Pitching Delta Wing," Journal of Fluids and Structures, Vol. 9, 1995, pp. 571-583.
6. Hall, M. G., "Vortex Breakdown," Annual Review of Fluid Mechanics, Vol. 4, 1972, pp. 195-218.
7. Gursul, I., Srinivas, S., and Batta, G., "Active Control of Vortex Breakdown over a Delta Wing," AIAA Journal Vol. 33, No. 9, 1995, pp. 1743-1745.
8. Gursul, I., Yang, H., and Deng, Q., "Control of Vortex Breakdown with Leading-Edge Devices," AIAA Paper 95-0676, Jan. 1995.
9. Yang, H., "Unsteady Nature of Vortex Breakdown over Delta Wings and Its Control," Ph.D. Thesis, Dept. of Mechanical, Industrial, and Nuclear Engineering, Univ. of Cincinnati, OH, 1996.
10. Gursul, I., and Ho, C.-M., "Vortex Breakdown over Delta Wings in Unsteady Freestream," AIAA Journal Vol. 32, No. 2, 1994, pp. 433-436.