Simulations of Pitch–Heave Limit-Cycle Oscillations at a Transitional Reynolds Number
Author:
Affiliation:
1. National Research Council Canada, Ottawa, Ontario K1A 0R6, Canada
2. Department of Mechanical and Aerospace Engineering, Royal Military College of Canada, Kingston, Ontario K7K 7B4, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052225
Reference44 articles.
1. Nonlinear Aeroelasticity
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4. Vortex shedding and shear-layer instability of wing at low-Reynolds numbers
5. Progress in Astronautics and Aeronautics;Lutz Th.,2001
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