多块壳体结构的等距拓扑优化

IF 4.3 3区 材料科学 Q1 ENGINEERING, ELECTRICAL & ELECTRONIC
Qiong Pan , Xiaoya Zhai , Hongmei Kang , Xiaoxiao Du , Falai Chen
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引用次数: 0

摘要

壳体结构指的是结构元件,其强度和承载能力来自于其薄而弯曲的几何形状。在实际应用中,壳体结构通常由多个补片组成,以忠实再现复杂多样的建筑结构。尽管如此,多补丁壳体结构的设计仍大有可为。然而,以往的工作大多致力于多补丁壳体结构的数值分析,而没有进一步的优化设计。本研究以 Reissner-Mindlin 理论为基础,提出了一种反向设计框架,特别关注多补丁结构。首先,对所提供的多补丁壳结构进行重新参数化和全局细化操作。对界面上具有共享自由度的控制点进行重新编号,自然而然地确保了补丁之间的 C0 连续性。随后,本研究探讨了等距分析法(IGA)和各向同性固体材料加惩罚法(SIMP)在壳结构拓扑优化中的结合。通过数值实例对所提出的方法进行了验证,强调了该方法在增强多补丁壳体结构设计方面的能力,并展示了其稳健性和高效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Isogeometric Topology Optimization of Multi-patch Shell Structures

Shell structures refer to structural elements that derive strength and load-bearing capacity from their thin and curved geometry. In practical applications, shell structures are commonly composed of multiple patches to represent intricate and diverse architectural configurations faithfully. Nevertheless, the design of multi-patch shell structures holds considerable promise. However, most of the previous work is devoted to the numerical analysis of multi-patch shell structures without further optimization design. The work proposes an inverse design framework, specifically focusing on multi-patch configurations based on Reissner–Mindlin theory. First, reparameterization and global refinement operations are employed on the provided multi-patch shell structures. Renumbering the indices of control points with shared degrees of freedom at the interface naturally ensures C0-continuity between patches. Subsequently, this study investigates the amalgamation of Isogeometric Analysis (IGA) and the Solid Isotropic Material with Penalization (SIMP) method for topology optimization of shell structures. The proposed approach is validated through numerical examples, emphasizing its capacity to enhance multi-patch shell structure design, showcasing robustness and efficiency.

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来源期刊
CiteScore
7.20
自引率
4.30%
发文量
567
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