Analytic prediction of the maximum amplitude of slender wing rock
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/10.2514/3.45720
Reference16 articles.
1. Dynamic load measurements with delta wings undergoing self-induced roll oscillations
2. Self-induced roll oscillations measured on a delta wing/canard configuration
3. The fluid mechanics of slender wing rock
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1. Novel model reference adaptive control with application to wing rock example;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-05-27
2. Review of self-induced roll oscillations and its attenuation for low-aspect-ratio wings;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-09-24
3. Experimental investigation of roll characteristics of a cruciform-finned slender body;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2016-08-06
4. A General Theory of Aircraft Wing Rock;Multiple Scales Theory and Aerospace Applications;2010-08-22
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