Modeling the Benchmark Active Control Technology wind-tunnel model for application to flutter suppression
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-3437
Reference12 articles.
1. Durham, M.H.; Keller, D.F.;Bennett, R.M.; and Wieseman, C.D.: A Status Report on a Model for Benchmark Active Controls Testing. AIAA Paper No. 91-1011.
2. On-line analysis capabilities developed to support the active flexible wing wind-tunnel tests
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