Further analysis of 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/10.2514/3.45886
Reference14 articles.
1. Experimental study of effects of forebody geometry on high angle-of-attack stability
2. Wing rock generated by forebody vortices
3. Moving wall effects in unsteady flow
4. The Magnus Effect: A Summary of Investigations to Date
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