首页> 外文会议>Symposium on Composite Structures: Theory and Practice, May 17-18, 1999, Seattle, Washington >Mechanisms and Modeling of Delamination Growth and Failure of Carbon-Fiber Reinforced Skin-Stringer Panels
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Mechanisms and Modeling of Delamination Growth and Failure of Carbon-Fiber Reinforced Skin-Stringer Panels

机译:碳纤维增强皮筋板的脱层生长和失效的机理与模型

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The main objective of this work was to investigate and predict the behavior of damaged structural elements (skin-stringer panels). The study combined characterization through testing with fractographic analysis, and analysis of delamination using the finite-element method. The experimental studies entailed investigation of damage growth from embedded skin defects in panels under compres-sive load, and the subsequent structural failure. Parameters such as defect size, location with respect to substructure and through-thickness position were studied. Local delamination and global panel buckling were modeled, and the resulting delamination growth was simulated using a moving mesh technique. The results illustrated the importance of the location of the 90° plies to the damage evolution, and the criticality of global buckling and stringer detachment in the structural failure. The understanding gained from both the experimental investigations and numerical simulations has led to guidelines for realistic modeling and rules for designing damage tolerant structures.
机译:这项工作的主要目的是调查和预测损坏的结构元件(纵梁面板)的行为。该研究将通过测试的表征与分形分析相结合,并使用有限元方法对分层进行了分析。实验研究需要调查在压力作用下面板中嵌入的皮肤缺陷造成的损伤增长,以及随后的结构破坏。研究了诸如缺陷尺寸,相对于子结构的位置以及贯穿厚度位置等参数。对局部分层和整体面板屈曲建模,并使用移动网格技术模拟最终的分层增长。结果说明了90°铺层的位置对损伤演变的重要性,以及整体屈曲和桁条脱离在结构破坏中的重要性。从实验研究和数值模拟中获得的理解导致了逼真的建模准则和设计耐损伤结构的规则。

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