表征复合材料/金属结构损伤容限的降维替代模型

Corey Arndt, Cody Crusenberry, Bozhi Heng, Rochelle Butler, Stephanie TerMaath
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引用次数: 1

摘要

复杂的工程模型通常需要大量的计算,并由高维参数空间定义,对参数效应的综合探索和设计优化提出了挑战。为了克服这种维数的诅咒,并最大限度地减少计算资源需求,本研究展示了一种用户友好的方法来制定一个表示高维、高保真源模型的降维代理模型。这种方法是专门为非专业人士使用商业工具开发的。在这种方法中,高保真源模型的复杂物理行为被分离成单个的、相互作用的物理行为。为每个行为创建一个单独的降维代理模型,然后将所有行为相加,形成表示源模型的降维代理模型。除了大量减少计算资源和相当的准确性外,该方法还提供了每个个体行为的特征,从而进一步了解源模型行为。该方法包括实验测试、有限元分析、替代模型和敏感性分析,并通过制定用共固化e -玻璃/环氧复合材料层压板增强铝板在四点弯曲下的损伤容限的降维替代模型进行了验证。结论是,该问题难以表征,将问题分解为相互作用的机制可以改善有关影响参数的信息和有效的降维代理建模。树脂与金属界面处的脱粘损伤是最困难的降维代理建模机制,因为它只涉及全参数空间的一小部分子空间。基于最具影响力参数的值,二元函数在适用时成功地参与了这种破坏机制。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Reduced-Dimension Surrogate Modeling to Characterize the Damage Tolerance of Composite/Metal Structures
Complex engineering models are typically computationally demanding and defined by a high-dimensional parameter space challenging the comprehensive exploration of parameter effects and design optimization. To overcome this curse of dimensionality and to minimize computational resource requirements, this research demonstrates a user-friendly approach to formulating a reduced-dimension surrogate model that represents a high-dimensional, high-fidelity source model. This approach was developed specifically for a non-expert using commercially available tools. In this approach, the complex physical behavior of the high-fidelity source model is separated into individual, interacting physical behaviors. A separate reduced-dimension surrogate model is created for each behavior and then all are summed to formulate the reduced-dimension surrogate model representing the source model. In addition to a substantial reduction in computational resources and comparable accuracy, this method also provides a characterization of each individual behavior providing additional insight into the source model behavior. The approach encompasses experimental testing, finite element analysis, surrogate modeling, and sensitivity analysis and is demonstrated by formulating a reduced-dimension surrogate model for the damage tolerance of an aluminum plate reinforced with a co-cured bonded E-glass/epoxy composite laminate under four-point bending. It is concluded that this problem is difficult to characterize and breaking the problem into interacting mechanisms leads to improved information on influential parameters and efficient reduced-dimension surrogate modeling. The disbond damage at the interface between the resin and metal proved the most difficult mechanism for reduced-dimension surrogate modeling as it is only engaged in a small subspace of the full parameter space. A binary function was successful in engaging this damage mechanism when applicable based on the values of the most influential parameters.
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