Flight-Loads Effects on Horizontal Tail Free-Play-Induced Limit Cycle Oscillation
Author:
Affiliation:
1. ZONA Technology, Inc., Scottsdale, Arizona 85258
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.29611
Reference15 articles.
1. NONLINEAR BEHAVIOR OF A TYPICAL AIRFOIL SECTION WITH CONTROL SURFACE FREEPLAY: A NUMERICAL AND EXPERIMENTAL STUDY
2. Chaotic and nonlinear dynamic response of aerosurfaces with structural nonlinearities
3. Experimental and Theoretical Study of Nonlinear Flutter
4. Nonlinear Response of Airfoil Section with Control Surface Freeplay to Gust Loads
5. LIMIT CYCLE BEHAVIOR OF AN AIRFOIL WITH A CONTROL SURFACE
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