Wing Rock Suppression Using Recessed Angle Spanwise Blowing
Author:
Affiliation:
1. Australian Defence Force Academy, Canberra, Australian Capital Territory 2600, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3015
Reference7 articles.
1. Development of an analytical model of wing rock for slender delta wings
2. Forebody vortex control for wing rock suppression
3. Delta wing vortex control via recessed angled spanwise blowing
4. Delta wing vortex manipulation using pulsed and steady blowing during ramp-pitching
5. Arena, A. S., Nelson, R. C., and Schiff, L. B. “The Effect of Asymmetric Vortex Wake Characteristics on a Slender Delta Wing Undergoing Wing Rock Motion,” AIAA Paper 89-3348, Aug. 1989.
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