Nonlinear Structural, Nonlinear Aerodynamic Model for Static Aeroelastic Problems
Author:
Affiliation:
1. Technion—Israel Institute of Technology, 32000 Haifa, Israel
2. Charles III University of Madrid, 28911 Leganés, Spain
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057309
Reference32 articles.
1. Nonlinear Flight Dynamics of Very Flexible Aircraft
2. Dynamic Response of Highly Flexible Flying Wings
3. Modeling of High Aspect Ratio Active Flexible Wings for Roll Control
4. Active Warping Control of a Joined Wing/Tail Airplane Configuration
5. Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft
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