Nonlinear Flutter Analysis for the Scaled F-35 with Horizontal-Tail Free Play
Author:
Affiliation:
1. ZONA Technology, Scottsdale, Arizona 85258
2. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032501
Reference17 articles.
1. HoffmanN. R. “Subsonic Flutter Tests of an All-Movable Stabilizer with 35 deg Sweepback,” WADC TN-55-623, Nov. 1955.
2. Flight-Loads Effects on Horizontal Tail Free-Play-Induced Limit Cycle Oscillation
3. Nonlinear Response of Aeroservoelastic Systems Using Discrete State-Space Approach
4. Aeroelastic Response Induced by Free Play, Part 1: Theory
5. Aeroelastic Response Induced by Free Play, Part 2: Theoretical/Experimental Correlation Analysis
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