Finite element time domain - Modal formulation for nonlinear flutter of composite panels

DOI10.2514/3.12250zbMath0826.73063OpenAlexW2010695200MaRDI QIDQ4840027

Chuh Mei, Ruichao Zhou, David Y. Xue

Publication date: 4 December 1995

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

Full work available at URL: https://doi.org/10.2514/3.12250

zbMATH Keywords

convergencequasisteady first-order piston theory aerodynamicsquasisteady thermal stress theoryvon Kármán large-deflection strain-displacement relations

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Finite element methods applied to problems in solid mechanics (74S05) Composite and mixture properties (74E30)

Related Items (6)

Regular and chaotic oscillations of a Timoshenko beam subjected to mechanical and thermal loadings ⋮ A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel ⋮ Unified 2D continuous and reduced order modeling of thermomechanically coupled laminated plate for nonlinear vibrations ⋮ Nonlinear dynamics of a reduced multimodal Timoshenko beam subjected to thermal and mechanical loadings ⋮ Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model ⋮ Aerothermoelastic analysis of curvilinear fiber variable stiffness laminated panels in supersonic flow

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