Results of wind-tunnel testing from the piezoelectric aerostatic response tailoring investigation
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1511
Reference16 articles.
1. Fundamental mechanisms of aeroelastic control with control surface and strain actuation
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