有限元弯矩格式在非均匀结构弹性薄壳研究中的应用

O. Krivenko, P. Lizunov, Yu. M. Vorona, O. Kalashnikov
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引用次数: 0

摘要

本文致力于开发一种通用的方法来研究复杂形状和结构的薄、中厚壳在机械和热载荷作用下的变形、屈曲、后屈曲行为和振动。广泛的壳类被考虑:恒定和光滑可变厚度,肋和盖板,通道和空腔,孔,中间表面的尖锐弯曲,以及材料的多层结构。该方法基于三维几何非线性热弹性理论的位置,不使用壳理论的简化假设。计算模型的开发是基于使用具有多线性形状函数的通用等参空间有限元,这对于具有逐步变厚度的壳的所有截面都是相同的。根据有限元力矩格式的要求,建立了控制方程。以壳体的中表面为单一参考面。通过解析积分,得到了通用空间多层有限元控制方程的所有矩阵的显式形式。这加快了该方法的算法实现中计算的执行速度。该方法基于统一的方法,使得研究具有不同几何特征的多层壳在复杂热机械载荷下的厚度行为成为可能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Application of the finite element moment scheme to the investigation of thin elastic shells of inhomogeneous structure
The work is devoted to the problem of developing a universal method for studying the deformation, buckling, postbuckling behavior and vibrations of thin and medium-thickness shells of complex shape and structure under the action of mechanical and thermal loads. A wide class of shells is considered: of constant and smooth-variable thickness, with ribs and cover plates, channels and cavities, holes, sharp bends of the mid-surface, and with a multilayer structure of the material. The method is based on the positions of the 3D geometrically nonlinear theory of thermoelasticity without the use of simplifying hypotheses of the theory of shells. The development of the computational model is based on the use of a universal isoparametric spatial finite element with multilinear shape functions, which is the same for all sections of the shell with stepwise variable thickness. The governing equations are constructed in accordance with the requirements of the finite element moment scheme. The mid-surface of the shell’s casing is taken as a single reference surface. All matrices of governing equations for a universal spatial multilayer finite element are obtained in explicit form by analytical integration. This speeds up the execution of calculations in the algorithmic implementation of the method. Such an approach, based on a unified methodology, makes it possible to study the behavior of multilayer shells with different geometric features in terms of thickness under complex thermo-mechanical loading.
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