Aeroelastic Wing with Leading- and Trailing-Edge Control Surfaces
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3130
Reference18 articles.
1. Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity, Addison Wesley Longman Reading, MA, 1955, pp.460-474.
2. 2Dowell, E. H., Crawley, E. F., Curtiss, H. C., Jr., Peters, D. A., Scanlan, R. H., and Sisto, F., A Modern Course in Aeroelasticity, 3rd ed.Kluwer, Dordrecht, TheNetherlands,1995, pp.25-41.
3. Active Flexible Wing Program
4. Rolling maneuver load alleviation using active controls
5. Multiple Control Surface Utilization in Active Aeroelastic Wing Technology
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