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

DOI10.1007/s00707-021-03023-3zbMath1475.74065OpenAlexW3173900446MaRDI QIDQ2234966

Jie Wu, Zhengyin Ye, Liuqing Ye, Kun Ye

Publication date: 19 October 2021

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00707-021-03023-3

zbMATH Keywords

large deflectionRouth-Hurwitz criterionvon Karman platefirst-order piston theoryLyapunov indirect methodshock-induced flutter

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Plates (74K20) Stability of dynamical problems in solid mechanics (74H55) Shock waves and blast waves in fluid mechanics (76L05)

Cites Work

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• Chaotic analysis of nonlinear viscoelastic panel flutter in supersonic flow
• Suppression of nonlinear panel flutter at supersonic speeds and elevated temperatures
• Finite element time domain - Modal formulation for nonlinear flutter of composite panels
• Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method
• Analysis of nonlinear panel flutter and response under random excitation or nonlinear aerodynamic loading

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