Flutter Tests of the Pazy Wing
Author:
Affiliation:
1. Technion—Israel Institute of Technology, 3200003 Haifa, Israel
2. Rafael, Advanced Defense Systems, 3102102 Haifa, Israel
3. Tel-Aviv University, 6997801 Ramat-Aviv, Israel
Funder
PAZY Foundation
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061717
Reference15 articles.
1. Recent advance in nonlinear aeroelastic analysis and control of the aircraft
2. Dynamic Response of Highly Flexible Flying Wings
3. Geometrically Nonlinear Structural Modal Analysis Using Fictitious Masses
4. Nonlinear Structural, Nonlinear Aerodynamic Model for Static Aeroelastic Problems
5. Modal Rotations: A Modal-Based Method for Large Structural Deformations of Slender Bodies
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