Issue |
MATEC Web Conf.
Volume 151, 2018
2017 Asia Conference on Mechanical and Aerospace Engineering (ACMAE 2017)
|
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Article Number | 01003 | |
Number of page(s) | 5 | |
Section | Material Performance Analysis and Testing | |
DOI | https://doi.org/10.1051/matecconf/201815101003 | |
Published online | 21 February 2018 |
Nonlinear Dynamic Responses of a Honeycomb Sandwich Plate Subject to Transverse Excitations
1
College of science, Tianjin University of Science and Technology, 300457 Tianjin, P. R. China
2
College of Mechanical Engineering, Beijing University of Technology, 100124 Beijing, P. R. China
Nonlinear dynamic behaviors of a simply supported honeycomb sandwich plate subjected to the transverse excitations are investigated in this paper. Based on the classical thin plate theory and Von Karman large deformation theory, the governing equation of motion for the honeycomb sandwich plate is established by using the Hamilton principle. The nonlinear governing partial differential equation is discretized to the ordinary differential equations by differential quadrature method and then solved by Runge-Kutta-Fehlberg method. Based on the numerical simulations, combined with nonlinear dynamic theory, the influences of the frequency and amplitude of the transverse excitation are investigated respectively by using the bifurcation diagrams, Poincare maps and phase portraits. The results exhibit the existence of the period-1, period-2 and chaotic responses with the variation of the excitations, which demonstrate that those motions appear alternately.
© The Authors, published by EDP Sciences, 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. (http://creativecommons.org/licenses/by/4.0/).
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