Reduced-Order Analysis of Aeroelastic Systems with Freeplay Using an Augmented Modal Basis
Author:
Affiliation:
1. Technology Development Department, Embraer S.A., 12227-901 São José dos Campos, Brazil
2. Aerospace and Mechanical Engineering Department, University of Liège, 4000 Liège, Belgium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032912
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5. Behavior of Airfoil with Control Surface Freeplay for Nonzero Angles of Attack
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