Leading-edge vortex dynamics on a slender oscillating wing
Author:
Affiliation:
1. University of Notre Dame, Notre Dame, Indiana
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45664
Reference10 articles.
1. Investigation of Nonlinear Motion Experienced on a Slender-Wing Research Aircraft
2. Wing Rock Due to Aerodynamic Hysteresis
3. The fluid mechanics of slender wing rock
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