New Flutter-Suppression Method for a Missile Fin with an Actuator
Author:
Affiliation:
1. School of Aeronautic Science and Engineering, Beihang University, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031961
Reference15 articles.
1. Future of Airplane Aeroelasticity
2. Prediction and measurement of the dynamic stiffness and damping of hydraulic servo-actuators
3. Nonlinear flutter analysis of missiles with pneumatic fin actuators
4. Modal coordinates for aeroelastic analysis with large local structural variations
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