Design of Adjoint-Based Laws for Wing Flutter Control
Author:
Affiliation:
1. Stanford University, Stanford, California 78733
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031005
Reference16 articles.
1. SYNTHETIC JETS
2. Virtual aerodynamic shape modification at low angles of attack using synthetic jet actuators
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