横向荷载作用下层合纤维增强复合材料梁的随机有限元模拟

Boyang Chen, S. Jones, Matt Riley
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引用次数: 0

摘要

在分析纤维增强复合材料理论中,通常假设材料性能在纤维方向上均匀分布,以尽量减少计算费用。然而,制造工艺在复合材料的构建过程中引入了缺陷,如局部分层、基体和纤维中的不均匀分布、预先存在的应力和公差问题[1]。这些缺陷使得预测复合材料在载荷作用下的行为变得更加困难。因此,制造商和设计师必须对材料强度进行保守估计。本研究的目的是在宏观尺度上量化受悬臂荷载作用的层压纤维增强复合材料梁的不确定性,并全面介绍采用有限元方法的随机复合材料建模。本导论适用于已经熟悉结构力学和有限元方法的高年级本科生或新研究生。本文的目标是介绍与随机复合建模相关的关键主题,并提供验证材料,用于开发和验证自定义有限元代码。本文研究的系统是一个受横向尖端位移作用的复合悬臂梁。首次利用经典层合理论(CLT)预测了可调纤维取向的四层梁的横向尖端位移。然后,利用CLT方法建立了有限元模型,模拟了复合梁在尖端载荷作用下的变形。欧拉-伯努利梁单元包含两个节点,每个节点有两个自由度:横向挠度和旋转。与其他复合有限元相比,这些单元相对简单,但足以证明随机材料特性变化对梁的整体响应的影响,而不会混淆方法。有限元结果与多纤维方向铺层的解析预测结果进行了对比验证,保证了数值预测的准确性。然后将变化材料性能的随机方法添加到验证的有限元代码中。利用修正指数核的karhunen - lo展开,得到了复合梁中各层的弹性模量随空间变化的分布。计算了具有不同性能的梁的预测尖端位移,然后使用CLT确定产生相同尖端位移所需的有效均匀弹性模量。这种比较使读者能够量化空间变化属性对单一设计属性的影响:有效弯曲模量。然后用蒙特卡罗方法模拟了1000根组合梁,确定了有效弯曲模量的统计分布。结果表明,将具有不同材料性能的多层板粘结在一起形成复合梁的“平均效应”产生的梁的有效挠曲模量变化不像多层板的弹性模量变化那么大。发现有效弯曲模量的标准偏差比施加在板弹性模量上的变化小一个数量级。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Stochastic Finite Element Modeling of Laminated Fiber-Reinforced Composite Beams Under Transverse Loading
It is common in analytic fiber-reinforced composite theory to assume uniformly distributed material properties across the fiber direction to minimize computational expense. However, manufacturing processes introduce imperfections during the construction of composite materials, such as localized delamination, non-uniform distribution in matrix and fibers, pre-existing stress, and tolerance issues [1]. These imperfections make it more difficult to predict the behavior of composite materials under loading. As a result, manufacturers and designers must use conservative estimates of material strength. This study aims to quantify the uncertainty in laminated fiber-reinforced composite beams subjected to cantilever loads on a macroscopic scale and to provide an all-inclusive introduction to stochastic composite modeling using the finite element method. This introduction is intended for upper undergraduates or new graduate students how are already familiar with structural mechanics and the finite element method. The goal of the paper is to introduce the key topics related to stochastic composite modeling and have validation material with which they can develop and verify custom finite element code. The system investigated herein is a composite cantilever beam subjected to a transverse tip displacement. Classical Lamination Theory (CLT) is first employed to predict the transverse tip displacement of a beam composed of four lamina at adjustable fiber orientations. A finite element model is then created using a CLT approach to simulate the composite beam’s deformation under tip loading. The Euler-Bernoulli beam elements contain two nodes with two degrees of freedom each: transverse deflection and rotation. These elements are relatively simplistic relative to other composite finite elements, but are sufficient to demonstrate the effect of stochastic material property variation on the overall response of the beam without obfuscating the approach. The finite element results are validated against the analytic predictions for multiple fiber direction layups to ensure the numerical predictions are accurate. The stochastic approach for varying material properties is then added to the validated finite element code. A Karhunen–Loève expansion of a modified exponential kernel is used to produce spatially-varying elastic modulus profiles for each lamina in the composite beam. The predicted tip displacement for the beam with varying properties is computed, and then CLT is used to determine the effective uniform elastic modulus that is required to produce the same tip displacement. This comparison allows the reader to quantify the impact of the spatially varying properties to a single design property: the effective flexural modulus. A Monte Carlo simulation of 1000 composite beams is then used to determine the statistical distribution of the effective flexural modula. Results suggest that the “averaging effect” of bonding multiple laminas with varying material properties together into composite beams produces effective flexural modula for the beams that do not vary as significantly as the laminas’ elastic modula. Standard deviations of the effective flexural modula are found to be an order of magnitude smaller than that of the variation imposed on the laminas’ elastic modulus.
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