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碳纤维增强塑料板中分层与基体裂纹的相互作用,第一部分:模型验证的试验方法。

Interaction of delaminations and matrix cracks in a CFRP plate, Part I: A test method for model validation.

作者信息

McElroy Mark, Jackson Wade, Olsson Robin, Hellström Peter, Tsampas Spyros, Pankow Mark

机构信息

NASA Langley Research Center, 2 W. Reid St, Mail Stop 188E, Hampton, VA 23681.

Swerea SICOMP, Gothenburg, Sweden.

出版信息

Compos Part A Appl Sci Manuf. 2017 Dec;103:314-326. doi: 10.1016/j.compositesa.2017.09.011. Epub 2017 Sep 22.

Abstract

Isolating and observing the damage mechanisms associated with low-velocity impact in composites using traditional experiments can be challenging, due to damage process complexity and high strain rates. In this work, a new test method is presented that provides a means to study, in detail, the interaction of common impact damage mechanisms, namely delamination, matrix cracking, and delamination-migration, in a context less challenging than a real impact event. Carbon fiber reinforced polymer specimens containing a thin insert in one region were loaded in a biaxial-bending state of deformation. As a result, three-dimensional damage processes, involving delaminations at no more than three different interfaces that interact with one another via transverse matrix cracks, were observed and documented using ultrasonic testing and x-ray computed tomography. The data generated by the test is intended for use in numerical model validation. Simulations of this test are included in Part II of this paper.

摘要

由于损伤过程复杂且应变率高,使用传统实验来分离和观察复合材料中与低速冲击相关的损伤机制可能具有挑战性。在这项工作中,提出了一种新的测试方法,该方法提供了一种手段,能够在比实际冲击事件挑战性更小的环境中详细研究常见冲击损伤机制(即分层、基体开裂和分层迁移)之间的相互作用。在一个区域含有薄插入物的碳纤维增强聚合物试样在双轴弯曲变形状态下加载。结果,利用超声检测和X射线计算机断层扫描观察并记录了三维损伤过程,该过程涉及不超过三个不同界面处的分层,这些分层通过横向基体裂纹相互作用。该测试生成的数据旨在用于数值模型验证。本文第二部分包含了该测试的模拟。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/7e85/8051255/09005199c27d/nihms-1532148-f0001.jpg

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