Open- and closed-loop results of a strain-actuated active aeroelastic wing
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139-4307
2. 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/10.2514/3.47045
Reference20 articles.
1. Summary of an Active Flexible Wing program
2. Control of aeroelastic instabilities through stiffness cross-coupling
3. Static aeroelastic control of an adaptive lifting surface
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