Self-induced roll oscillations measured on a delta wing/canard configuration
Author:
Affiliation:
1. San Diego State University, San Diego, California
2. Technion R&D Foundation, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45386
Reference10 articles.
1. ^rlic-Rukemann, K.J. "Aerodynamic Aspects of Aircraft Dynamics at High Angles of Attack/' Journal of Aircraft, Vol.20, Sept. 1983, pp.737-752.
2. Wing Rock Due to Aerodynamic Hysteresis
3. Dynamic load measurements with delta wings undergoing self-induced roll oscillations
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