具有弹性蜂窝芯的三层双弯曲壳体的强迫振动

K. Avramov, B. Uspensky
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引用次数: 0

摘要

本文建立了三层双弯曲壳在几何非线性变形作用下振动的数学模型。中间层是采用FDM增材技术制造的蜂窝结构。采用均匀化方法对蜂窝的力学性能进行了评价。外壳的外层很薄,由碳填充的塑料制成。该模型基于高阶剪切理论,并考虑了所有壳层力学性能的正交异性。壳的每一层由五个变量(三个位移投影和两个法线与中间表面的旋转角度)来描述。用Rayleigh?里兹方法。由于壳的中间层比外层更轻,更柔顺,因此计算过程具有一些特点。得到了壳体的本征频率和本征模态,为进一步的非线性振动分析奠定了基础。几何非线性变形作用下壳体受迫振动的数学模型是采用假设模态法推导的非线性常微分方程组。采用延拓法和射击法相结合的数值方法研究了非线性周期振动及其分岔问题。用数值方法研究了非线性周期振动在基频和次谐波共振区及其分岔的性质。考虑了球面面板和双曲抛物面面板。结果表明,当扰动力施加于面板重心外的一点时,面板的本征模态相互作用,频率响应和分岔图与施加于面板重心的情况相比发生了定性变化。结果之间的一致性作为瑞利-里兹和假设模式展开中项数的函数进行了研究。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Forced vibrations of a three-layered double-curved shell with an elastic honeycomb core
This paper presents a mathematical model of vibrations of a three-layered double-curved shell under geometrically nonlinear deformation. The middle layer is a honeycomb manufactured using FDM additive technologies. The mechanical properties of the honeycomb were assessed by a homogenization procedure. The outer layers of the shell are thin, and they are made of carbon-filled plastic. The model is based on a higher-order shear theory and accounts for the orthotropy of the mechanical properties of all the shell layers. Each layer of the shell is described by five variables (three displacement projections and two rotation angles of the normal to the middle surface). The properties of linear vibrations were studied using discretization by the Rayleigh?Ritz method. Because the middle layer of the shell is far lighter and more compliant in comparison with the outer layers, the computational process has some features. The eigenferquencies and eigenmodes of the shell were found for a further analysis of nonlinear vibrations. The mathematical model of forced vibrations of the shell under geometrically nonlinear deformation is a system of nonlinear ordinary differential equations derived by the assumed-mode method. Nonlinear periodic vibrations and their bifurcations were studied using a numerical procedure, which is a combination of the continuation method and the shooting technique. The properties of the nonlinear periodic vibrations and their bifurcations in the regions of fundamental and subharmonic resonances were studied numerically. A spherical panel and a hyperbolic paraboloid panel were considered. It was shown that when a disturbing force is applied at a point out of the panel’s center of gravity, the panel’s eigenmodes interact, and the frequency response and the bifurcation diagram change qualitatively in comparison with the case where that force is applied at the panel’s center of gravity. An agreement between the results was studied as a function of the number of terms in the Rayleigh-Ritz and assumed-mode expansions.
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