On the aeroelastic stability and bifurcation structure of subsonic nonlinear thin panels subjected to external excitation

DOI10.1007/s00419-012-0618-4zbMath1293.74233OpenAlexW2024214372MaRDI QIDQ396306

Yiren Yang, Guo Chen, Wei Xu, Peng Li

Publication date: 13 August 2014

Published in: Archive of Applied Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00419-012-0618-4

zbMATH Keywords

Galerkin methodchaossubsonic flowaeroelastic stabilitybifurcation structureparameter spaces

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Stability of dynamical problems in solid mechanics (74H55) General aerodynamics and subsonic flows (76G25) Dynamical bifurcation of solutions to dynamical problems in solid mechanics (74H60)

Related Items (5)

On double stable limit cycle flutter of a plate with motion constraints in subsonic flow ⋮ Bifurcation structure and scaling properties of a subsonic periodically driven panel with geometric nonlinearity ⋮ The instability of a plate fixed at both ends in an axial flow revisited: an application of the DQ-BE method ⋮ Stability analysis and active control of a nonlinear composite laminated plate with piezoelectric material in subsonic airflow ⋮ Nonlinear flutter behavior of a plate with motion constraints in subsonic flow

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