Hysteresis of vortex development and breakdown on an oscillating delta wing

AIAA Journal

Volumn 25, Issue 11, 1987, Pages 1512-1513

  Atta, R ^a   Rockwell, D ^a  

^a LEHIGH UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT - DELTA WING; FLOW OF FLUIDS - VORTEX FLOW;

OSCILLATING DELTA WING; SWEPT LEADING EDGE; VORTEX CORE;

AERODYNAMICS;

EID: 0023452375     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.9812     Document Type: Article

References (5)

1. Wedemeyer, E., “Vortex Breakdown,” High Angie of Attack Aerodynamics, AGARD Lecture Series 121, 1982, pp. 9-1-9-7.
2. Rockwell, D., Atta, R., Klink, A., Lawson, R., Magness, C., and Utsch, T., “Unsteady Flow Structure from Swept Edges Subjected to Controlled Motion,” Progress Rept. on AFOSR Grant 86-0177, 1986.
3. McCroskey, W. J., “Unsteady Airfoils,” Annual Review of Fluid Mechanics, Vol. 14, 1982, pp. 285-312.
4. Gad-el-Hak, M. and Ho, C. M., “The Pitching Delta Wing,” AIAA Journal, Vol. 23, Nov. 1985, pp. 1660-1665.
5. Atta, R., “Flow Structure on a Pitching Delta Wing,” Ph.D. Dissertation, Dept, of Mechancial Engineering and Mechanics, Lehigh University, Bethlehem, PA, 1987.