Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method

DOI10.2514/3.12530zbMath0846.73045OpenAlexW1561203869MaRDI QIDQ4876558

Chuh Mei, Ruichao Zhou, David Y. Xue, Jen-Kuang Huang, Zhihong Lai

Publication date: 10 June 1996

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.12530

zbMATH Keywords

feedback controloptimal controllerrectangular isotropic plateslimit-cycle flutter motionslinearized modal equations

Mathematics Subject Classification ID

Control, switches and devices (``smart materials) in solid mechanics (74M05) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite element methods applied to problems in solid mechanics (74S05)

Related Items (4)

Active control of laminated composite truncated conical shells using vertically and obliquely reinforced 1-3 piezoelectric composites ⋮ Vibration and dynamic instability analyses of functionally graded porous doubly curved panels with piezoelectric layers in supersonic airflow ⋮ Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model ⋮ Short-wave instability of an elastic plate in supersonic flow in the presence of the boundary layer

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