Application of piezoelectric elements in supersonic panel flutter suppression
Author:
Affiliation:
1. Rensselaer Polytechnic Institute, Troy, NY
2. McDonnell Douglas Missile Systems Co., Saint Louis, MO
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-3191
Reference22 articles.
1. Aeroelasticity of Plates and Shells
2. Optimization of structures to satisfy flutter requirements.
3. Aeroelastic Optimization of a Panel in High Mach Number Supersonic Flow
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1. Gust load alleviation wind tunnel tests of a large-aspect-ratio flexible wing with piezoelectric control;Chinese Journal of Aeronautics;2017-02
2. Panel Flutter Constraints: Analytic Sensitivities and Approximations Including Planform Shape Design Variables;Journal of Aircraft;1997-07
3. State-space modeling of aerodynamic forces on plate using singular value decomposition;AIAA Journal;1996-12
4. Panel flutter constraints - Analytic sensitivities and approximations including planform shape design variables;6th Symposium on Multidisciplinary Analysis and Optimization;1996-08-22
5. Active control of panel flutter with piezoelectric transducers;Journal of Aircraft;1996-07
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