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Impact response of thick composite plates under uniaxial tensile preloading

机译:单轴拉伸预压下厚板的冲击响应

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摘要

This work focuses on the impact response of composite plates 5 mm thick subjected to uniaxial tension preload. Laminated carbon/epoxy with quasi-isotropic stacking sequence ([0/45/90/ - 45](2))(S) samples were used. Doehlert-type design of experiments was proposed to investigate the influence of both preload and impact energy on impact composite responses. Deformation, varying from 300 to 3000 micro-strain, was imposed thanks to a preload device designed for this purpose. Impacts were generated using a home made drop tower. Imposed impact energy was varying from 30 to 214J. Post-impact damage was characterized by both non-destructive (ultrasound) and destructive (deply) techniqtres. Influence of the preloading on delamination areas (total and projected) was quantified and found sensitive to the preloading. (C) 2014 Elsevier Ltd. All rights reserved.
机译:这项工作着重于5mm厚的复合板在单轴拉伸预载荷下的冲击响应。使用具有准各向同性堆叠顺序([0/45/90 /-45](2))(S)的层压碳/环氧树脂样品。提出了Doehlert型实验设计,以研究预紧力和冲击能量对冲击复合材料响应的影响。多亏了为此目的设计的预紧装置,变形范围从300到3000微应变不等。使用自制的落塔产生了影响。施加的冲击能量从30到214J不等。撞击后损害的特征是非破坏性(超声波)和破坏性(严重)技术。定量分析了预加载对分层区域(总和投影)的影响,发现对预加载敏感。 (C)2014 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Composite Structures》 |2015年第3期|172-181|共10页
  • 作者单位

    Arts & Metiers Paristech, Inst Mecan & Ingn Bordeaux, UMR CNRS 5295, F-33400 Talence, France;

    Univ Bordeaux, Inst Mecan & Ingn Bordeaux, UMR CNRS 5295, F-33400 Talence, France;

    Arts & Metiers Paristech, Inst Mecan & Ingn Bordeaux, UMR CNRS 5295, F-33400 Talence, France;

    Arts & Metiers Paristech, Inst Mecan & Ingn Bordeaux, UMR CNRS 5295, F-33400 Talence, France;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Composites; Carbon fibers; Low-velocity impact; Preloading; Thick plate;

    机译:复合材料;碳纤维;低速冲击;预压;厚板;

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