Active Flutter Suppression on Composite Tow Steered Panels based on Piezoelectric Actuation
Author:
Affiliation:
1. Federal University of Uberlandia
2. Technological Institute of Aeronautics (ITA)
3. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0188
Reference22 articles.
1. Finite-element panel flutter in three-dimensional supersonic unsteady potential flow
2. Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow
3. Finite element method for large-amplitude two-dimensional panel flutter at hypersonic speeds
4. Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method
5. Flutter of stiffened composite panels considering the stiffener’s base as a structural element
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3. A Review on Applications of Piezoelectric Materials in Aerospace Industry;Integrated Ferroelectrics;2020-10-12
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