Dissipative properties of three-layered composite structures. 4. Numerical experiment

B. Yartsev, V. Ryabov, L. Parshina
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Abstract

Object and purpose of research. The study is concerned with a three-layer plate formed by two rigid anisotropic layers and a soft medium isotropic layer of viscoelastic polymer. Each rigid layer presents anisotropic structure formed by a finite number of randomly oriented orthotropic viscoelastic layers of composites. The paper is intended to study the influence of reinforcement orientation of rigid layers, relative thickness of the soft layer of an isotropic viscoelastic polymer and the ambient temperature on values values of natural frequencies and mechanical loss factors of the coupled damped oscillations in symmetric and assymetric plates. Materials and methods. Numerical experiment using a computer program implementing the previously proposed method for solving coupled differential equations of damped oscillations in anisotropic three-layer plates [2]. Main results. It was shown that in unsupported globally monoclinic symmetrical three-layer rectangular plate a bendingtorsional interaction occurs, generating mutual transformations of the eigenforms of the coupled oscillation modes if at least in one of the directions of the plate one of the eigenforms is characterized by an even number of quarters of the wave, and the other eigenform is characterized by an odd number of quarters of the wave. In unsupported globally orthotropic asymmetric three-layer rectangular plate interaction of bending modes of oscillations occurs in two mutually orthogonal planes, if both eigenforms are characterized by either an even or an odd number of wave quarters in main directions of the plate. It was found that each mode of natural oscillations of both symmetric and asymmetric three-layer plates has its own effective relative thickness of the soft layer of an isotropic viscoelastic polymer corresponding to the maximum level of dissipative properties. A further increase in the relative thickness is often accompanied by a decrease in values of the mechanical loss factors. The significant influence of ambient temperature on natural frequencies values and mechanical loss factors of all considered oscillation modes of symmetric and asymmetric unsupported rectangular three-layer composite plates is demonstrated. Conclusion. It was found that coupled damped oscillations of a symmetric three-layer plate are described by two systems of differential equations, with structures close to that of the systems of corresponding differential equations describing the damped oscillations of a quasi-homogeneous monoclinic plate. At the same time, the coupled damped oscillations of an asymmetric three-layer plate are described by two systems of differential equations that coincide with the systems of corresponding differrential equations describing the damped oscillations of a globally orthotropic three-layer plate.
三层复合材料结构的耗散特性。4. 数值实验
研究对象和目的。研究了由两层刚性各向异性层和软介质各向同性层组成的粘弹性聚合物三层板。每一刚性层都是由有限数量的随机取向正交各向异性粘弹性层构成的各向异性结构。本文研究了各向同性粘弹性聚合物刚性层的增强取向、软层的相对厚度和环境温度对对称和非对称板耦合阻尼振荡的固有频率和力学损耗因子的影响。材料和方法。利用计算机程序实现了先前提出的求解各向异性三层板[2]阻尼振荡耦合微分方程的方法。主要的结果。结果表明,在无支撑的全局单斜对称三层矩形板中,如果至少在板的一个方向上,其中一个本征形式具有偶数四分之一波的特征,而另一个本征形式具有奇数四分之一波的特征,则会产生耦合振荡模式的本征形式的相互变换。在无支撑的全局正交各向异性非对称三层矩形板中,如果两个本征形式在板的主要方向上具有偶数或奇数波四分之一,则振荡的弯曲模态相互作用发生在两个相互正交的平面上。研究发现,对称和非对称三层板的每种自然振荡模式都有各自对应于耗散性能最大水平的各向同性粘弹性聚合物软层有效相对厚度。相对厚度的进一步增加往往伴随着机械损耗因子值的降低。证明了环境温度对对称和非对称无支承矩形三层复合材料板的固有频率值和所有考虑的振动模态的机械损耗因子的显著影响。结论。研究发现,对称三层板的耦合阻尼振荡可以用两个系统的微分方程来描述,其结构与描述准均匀单斜板阻尼振荡的相应微分方程系统的结构接近。同时,用两组微分方程描述了非对称三层板的耦合阻尼振荡,这两组微分方程与描述全局正交各向异性三层板的耦合阻尼振荡的相应微分方程组重合。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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