Suppression of nonlinear panel flutter at supersonic speeds and elevated temperatures

DOI10.2514/3.13070zbMath0932.74024OpenAlexW2095320990MaRDI QIDQ4373185

Chuh Mei, Ruichao Zhou, Jen-Kuang Huang

Publication date: 2 March 2000

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

Full work available at URL: https://doi.org/10.2514/3.13070

zbMATH Keywords

feedback controlmodal coordinatesthermal loadsmodal transformationcomposite panelsembedded piezoelectric layersmaximum flutter-free dynamic pressurenonlinear modal equationsvon Kármán's large-deflection theory

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Thermal effects in solid mechanics (74F05) Electromagnetic effects in solid mechanics (74F15)

Related Items (1)

Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model

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