A study on the failure mechanisms of carbon fiber/epoxy composite laminates using acoustic emission

被引:163
|
作者
Liu, P. F. [1 ]
Chu, J. K. [1 ]
Liu, Y. L. [1 ,2 ]
Zheng, J. Y. [1 ]
机构
[1] Zhejiang Univ, Inst Chem Machinery & Proc Equipment, Hangzhou 310027, Zhejiang, Peoples R China
[2] Hangzhou Special Equipment Inspect Inst, Hangzhou 310003, Zhejiang, Peoples R China
来源
MATERIALS & DESIGN | 2012年 / 37卷
关键词
B; Laminates; E; Mechanical; H. Failure analysis; DAMAGE MECHANISMS; DELAMINATION; POLYPROPYLENE; INITIATION; EVOLUTION; EVENTS; MODES;
D O I
10.1016/j.matdes.2011.12.015
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The complex failure mechanisms that are commonly considered as the distinctive characteristic of composites are being amenable to nondestructive test advance. This research adopts the acoustic emission technique to study the failure mechanisms and damage evolution of carbon fiber/epoxy composite laminates. Effects of different lay-up patterns and hole sizes on the acoustic emission response are studied to set up the mapping between the failure properties and the acoustic signal features such as the energy, counting and amplitude. Moreover, the microscopic properties of different composite specimens after fracture are watched and analyzed by scanning electron microscope (SEM). Based on the mapping conception, the controlling microscopic failure mechanisms of composites including the splitting matrix cracking, fiber/matrix interface debonding, fiber pull-out and breakage as well as delamination are identified. It is expected the influence of complex lay-up patterns and sizes on the damage and failure properties of composites is represented by creating true mapping based on the acoustic emission technique. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:228 / 235
页数:8
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