Wing rock generated by forebody vortices
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Inc., Sunnyvale, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45731
Reference22 articles.
1. Experimental study of effects of forebody geometry on high angle-of-attack stability
2. 2Nguyen, L., Yip, L., and Chambers, J. "Self-Induced Wing Rock of Slender Delta Wings,"AIAA Paper 81-1883, Aug. 1981.
3. A possible causative flow mechanism for body rock
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