The low-velocity impact response of fiber-metal laminates

Author:

Fan J.1,Cantwell WJ2,Guan ZW2

Affiliation:

1. Department of Engineering, University of Liverpool, Liverpool, UK,

2. Department of Engineering, University of Liverpool, Liverpool, UK

Abstract

The low-velocity impact response of a series of glass fiber reinforced epoxy/aluminum alloy fiber metal laminates has been investigated. The influence of varying target thickness, plate diameter, and impactor radius has been studied and the results compared to those offered by plain composite samples. After testing, many samples were sectioned in order to highlight the failure modes under low-velocity impact loading. The FMLs absorbed significant energy in plastic deformation, tearing the metal layers and fiber fracture, and offered a superior impact resistance to the plain composite on which the FMLs were based. The perforation data were normalized by the areal density of the target and the superiority of the metal—composite hybrids remained in evidence. Increasing the target size, the plate thickness, and the indentor diameter resulted in an increase in the energy required to perforate the target. In contrast, impacting the square panels at the corner or along the edge of the target did not have a significant effect on the perforation response of the structures.

Publisher

SAGE Publications

Subject

Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Cited by 59 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. High‐velocity ballistic response of AA 1100‐H14 based carbon‐fiber metal laminates: An experimental investigation;Polymer Composites;2023-12-11

2. Effect of Impact Energy Divisions for Repeated Low-Velocity Impacts by Varied Masses on GLARE;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2023-11-21

3. Low velocity impact on fibre metal laminates: A review;Journal of Composite Materials;2023-10-25

4. Study on off-center impact behavior and damage characterization of carbon fiber reinforced aluminum laminate;Composite Structures;2023-01

5. Impact behaviour of fibre-metal laminates;Dynamic Deformation, Damage and Fracture in Composite Materials and Structures;2023

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3