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A Biaxial-Bending Test to Observe the Growth of Interacting Delaminations in a Composite Laminate Plate

机译:观察复合层压板中相互作用分层的增长的双轴弯曲试验

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It is not easy to isolate the damage mechanisms associated with low-velocityimpact in composites using traditional experiments. In this work, a new experiment ispresented with the goal of generating data representative of progressive damageprocesses caused by low-velocity impact in composite materials. Carbon fiberreinforced polymer test specimens were indented quasi-statically such that a biaxialbendingstate of deformation was achieved. As a result, a three-dimensional damageprocess, involving delamination and delamination-migration, was observed anddocumented using ultrasonic and x-ray computed tomography. Results from twodifferent layups are presented in this paper. Delaminations occurred at up to threedifferent interfaces and interacted with one another via transverse matrix cracks.Although this damage pattern is much less complex than that of low-velocity impacton a plate, it is more complex than that of a standard delamination coupon test andprovides a way to generate delamination, matrix cracking, and delamination-migrationin a controlled manner. By limiting the damage process in the experiment to threedelaminations, the same damage mechanisms seen during impact could be observedbut in a simplified manner. This type of data is useful in stages of model developmentand validation when the model is capable of simulating simple tests, but not yetcapable of simulating more complex and realistic damage scenarios.
机译:隔离与低速相关的破坏机制并不容易 传统实验对复合材料的影响。在这项工作中,一个新的实验是 提出的目的是生成代表渐进性损伤的数据 复合材料中低速冲击引起的过程。碳纤维 增强聚合物试样准静态压痕,使双轴弯曲 达到变形状态。结果,三维损坏 观察到了涉及分层和分层迁移的过程,并且 使用超声波和X射线计算机断层扫描进行记录。来自两个的结果 本文介绍了不同的上篮方式。多达三层发生分层 不同的界面,并通过横向基体裂纹相互作用。 尽管这种损坏方式比低速撞击的方式复杂得多 在板上,它比标准分层试样测试更复杂,并且 提供了一种产生分层,基质开裂和分层迁移的方法 以受控的方式。通过将实验中的损坏过程限制为三个 分层,可以观察到在撞击过程中看到的相同破坏机制 但以简化的方式。此类数据在模型开发阶段很有用 当模型能够模拟简单测试但尚未验证时进行验证 能够模拟更复杂和现实的损坏情况。

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