Further Research for Sensitivity Analyses of Discrete Periodic Systems
Author:
Affiliation:
1. Fudan University, 200433 Shanghai, People’ s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.767
Reference14 articles.
1. 1Conner, M. D. “Nonlinear Aeroelasticity of an Airfoil Section with Control Surface Freeplay,” Ph.D. Dissertation,Dept. of Mechanical Engineering and Material Science, Duke Univ., Durham, NC,1996.
2. NONLINEAR BEHAVIOR OF A TYPICAL AIRFOIL SECTION WITH CONTROL SURFACE FREEPLAY: A NUMERICAL AND EXPERIMENTAL STUDY
3. Reduced-Order Aerodynamic Model and Its Application to a Nonlinear Aeroelastic System
4. LIMIT CYCLE BEHAVIOR OF AN AIRFOIL WITH A CONTROL SURFACE
5. Unsteady aerodynamic modeling for arbitrary motions
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