The Nonlinear Dynamical Analysis of a Sandwich Plate with In-Plane Loading in Supersonic Flow

DOI10.1142/S0218127416501443zbMath1347.34081OpenAlexW2508229406MaRDI QIDQ2827017

Minghui Yao, HongBo Wang, Wei Zhang, Xiao-Dong Yang

Publication date: 12 October 2016

Published in: International Journal of Bifurcation and Chaos (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0218127416501443

zbMATH Keywords

chaosbifurcationnonlinear dynamicsfluttersandwich plate

Mathematics Subject Classification ID

Bifurcation theory for ordinary differential equations (34C23) Plates (74K20) Characteristic and Lyapunov exponents of ordinary differential equations (34D08) Qualitative investigation and simulation of ordinary differential equation models (34C60) Complex behavior and chaotic systems of ordinary differential equations (34C28) Supersonic flows (76J20) Multiple scale methods for ordinary differential equations (34E13)

Related Items (1)

A new method for suppressing nonlinear flutter and thermal buckling of composite lattice sandwich beams

Cites Work

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• Influence of corner stresses on the stability characteristics of composite skew plates
• A higher-order theory for free vibration of unsymmetrically laminated composite and sandwich plates—finite element evaluations
• Dynamic response of orthotropic, homogeneous, and laminated cylindrical shells
• Flutter analysis of stiffened laminated composite plates and shells in supersonic flow
• Finite element flutter analysis of composite skew panels
• The Fluttering Panel as a Continuous Nonlinear Nonconservative System

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