Instantaneous topology of the unsteady leading-edge vortex at high angle of attack
Author:
Affiliation:
1. Lehigh University, Bethlehem, Pennsylvania 18015
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11786
Reference32 articles.
1. On the feasibility of low-speed aircraft maneuvers involving extreme angles of attack
2. 2Reynolds, G., and Abtahi, A. A. "Instabilities in Leading-Edge Vortex Development," AIAA Paper 87-2424,1987.
3. 3Magness, C., Robinson, O., and Rockwell, D. "Control of Leading-Edge Vortices on a Delta Wing," AIAA Paper 89-0999,1989.
4. Hysteresis of vortex development and breakdown on an oscillating delta wing
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