Active Control of Panel Oscillation Induced by Accelerating Boundary Layer and Sound
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.7449
Reference19 articles.
1. Control of panel response to turbulent boundary-layer and acoustic excitations
2. Chaotic oscillations in mechanical systems
3. Stabilization of non-linear panel vibrations by boundary damping
4. Acoustic field in unsteady moving media
5. Synchronization in chaotic systems
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