Reduced order models for the nonlinear dynamic analysis of shells

被引:15
|
作者
Goncalves, Paulo B. [1 ]
Silva, Frederico M. A. [2 ]
Del Prado, Zenon J. G. N. [2 ]
机构
[1] Pontificial Catholic Univ, Marques Sao Vicente 225, BR-22451900 Rio De Janeiro, Brazil
[2] Univ Fed Goias, Av Univ 1488, BR-74605220 Goiania, Go, Brazil
关键词
Shells; reduced order models; modal coupling and interaction; internal resonances; nonlinear shell vibrations;
D O I
10.1016/j.piutam.2016.03.016
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The non-linear dynamic analysis of continuous systems, such as thin plates and shells, is a problem of relevance in many engineering fields. The finite element method is the most used approach for nonlinear dynamic analyses of these structures. However, the computational effort is very high. As an alternative to complex numerical approaches, analytical methods using simplified models can be successfully used to understand the main nonlinear features of the problem and may constitute efficient tools in the initial design stages. For plates and shells, the derivation of efficient reduced order models is in fact essential due to the complex nonlinear response of these structures. The usual procedure is to reduce the partial differential equations of motion of the continuous system to an approximate system of time-dependent ordinary differential equations of motion, which are in turn solved by numerical methods or, approximately, by perturbation procedures. However, the use of inappropriate modal expansions usually leads to misleading results or may require a rather large number of terms. The aim of the present work is to show how the application of a perturbation analyses together with the Galerkin method can be used to derive precise low order models for plates and shells, by capturing the influence of modal couplings and interactions. (C) 2016 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:118 / 125
页数:8
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