Dynamic Aeroservoelastic Response with Nonlinear Structural Elements
Author:
Affiliation:
1. Department of Aerospace Engineering, Technion—Israel Institute of Technology, 32000 Haifa, Israel
2. Israeli Computational Fluid Dynamics Center, 38900 Caesarea Industrial Park, Israel
3. Airbus Defense and Space, 28906 Getafe, Spain
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053550
Reference8 articles.
1. Reduced-Size Aeroservoelastic Modeling and Limit-Cycle-Oscillation Simulations with Structurally Nonlinear Actuators
2. Limit Cycle Oscillations of Plate-Type Fins Using Increased-Order Models
3. Rigid-Body Issues in FFT-Based Dynamic Loads Analysis with Aeroservoelastic Nonlinearities
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