Targeted Energy Transfer Between a Swept Wing and Winglet-Housed Nonlinear Energy Sink
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Illinois at Urbana–Champaign, Urbana, Illinois 61801
2. NextGen Aeronautics, Inc., Torrance, California 90505
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052538
Reference28 articles.
1. On the Transonic-Dip Mechanism of Flutter of a Sweptback Wing
2. Limit Cycle Oscillation Flight Test Results of a Fighter with External Stores
3. Store-induced limit cycle oscillations and internal resonances in aeroelastic systems
4. Limit Cycle Oscillation Characteristics of Fighter Aircraft
5. Active Flutter Suppression-A Flight Test Demonstration
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