Calculation of Aeroelastic Limit Cycles due to Localized Nonlinearity and Static Preload
Author:
Affiliation:
1. Aeronautical Development Agency, Bangalore 560 017, India
2. Duke University, Durham, North Carolina 27708
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055505
Reference21 articles.
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4. NONLINEAR BEHAVIOR OF A TYPICAL AIRFOIL SECTION WITH CONTROL SURFACE FREEPLAY: A NUMERICAL AND EXPERIMENTAL STUDY
5. Nonlinear aeroelastic analysis of airfoils: bifurcation and chaos
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