Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology

T700/6808 composite has been widely used in aerospace field and the damage in composite will seriously influence the safety of aircraft. However, the behavior of damage evolution in T700/6808 composite when it suffered from tensile loading is seldom researched. In this paper, the acoustic emission (...

Full description

Saved in:
Bibliographic Details
Main Authors: Weihan Wang, Weifang Zhang, Shengwang Liu, Xiaoshuai Jin
Format: Article
Language:English
Published: Wiley 2016-01-01
Series:Shock and Vibration
Online Access:http://dx.doi.org/10.1155/2016/6364205
Tags: Add Tag
No Tags, Be the first to tag this record!
_version_ 1849399643449851904
author Weihan Wang
Weifang Zhang
Shengwang Liu
Xiaoshuai Jin
author_facet Weihan Wang
Weifang Zhang
Shengwang Liu
Xiaoshuai Jin
author_sort Weihan Wang
collection DOAJ
description T700/6808 composite has been widely used in aerospace field and the damage in composite will seriously influence the safety of aircraft. However, the behavior of damage evolution in T700/6808 composite when it suffered from tensile loading is seldom researched. In this paper, the acoustic emission (AE) technology is employed to research the process of damage evolution in T700/6808 composite under tensile loading. Results show that the damage in T700/6808 composite is small in the initial stage of tensile loading, and main damage is the matrix cracking. The composite has serious damage in the middle stage of tensile loading, which mainly includes the matrix cracking and the interface damage as well as the fiber breakage. The number of fiber breakages decreases rapidly in the later stage of tensile loading. When it comes into the stage of load holding, the composite has relatively smaller damage than that in the stage of tensile loading, and the fiber breakage rarely occurs in the composite. Analysis of damage modes shows that the criticality of the matrix cracking and the interface damage is higher than the fiber breakage, which illustrates that the reliability of T700/6808 composite could be improved by the optimization of matrix and interface.
format Article
id doaj-art-9d1d56e3366f490ab64a48e27acfa098
institution Kabale University
issn 1070-9622
1875-9203
language English
publishDate 2016-01-01
publisher Wiley
record_format Article
series Shock and Vibration
spelling doaj-art-9d1d56e3366f490ab64a48e27acfa0982025-08-20T03:38:16ZengWileyShock and Vibration1070-96221875-92032016-01-01201610.1155/2016/63642056364205Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission TechnologyWeihan Wang0Weifang Zhang1Shengwang Liu2Xiaoshuai Jin3Science & Technology on Reliability & Environmental Engineering Laboratory, Beihang University, Beijing 100191, ChinaScience & Technology on Reliability & Environmental Engineering Laboratory, Beihang University, Beijing 100191, ChinaScience & Technology on Reliability & Environmental Engineering Laboratory, Beihang University, Beijing 100191, ChinaScience & Technology on Reliability & Environmental Engineering Laboratory, Beihang University, Beijing 100191, ChinaT700/6808 composite has been widely used in aerospace field and the damage in composite will seriously influence the safety of aircraft. However, the behavior of damage evolution in T700/6808 composite when it suffered from tensile loading is seldom researched. In this paper, the acoustic emission (AE) technology is employed to research the process of damage evolution in T700/6808 composite under tensile loading. Results show that the damage in T700/6808 composite is small in the initial stage of tensile loading, and main damage is the matrix cracking. The composite has serious damage in the middle stage of tensile loading, which mainly includes the matrix cracking and the interface damage as well as the fiber breakage. The number of fiber breakages decreases rapidly in the later stage of tensile loading. When it comes into the stage of load holding, the composite has relatively smaller damage than that in the stage of tensile loading, and the fiber breakage rarely occurs in the composite. Analysis of damage modes shows that the criticality of the matrix cracking and the interface damage is higher than the fiber breakage, which illustrates that the reliability of T700/6808 composite could be improved by the optimization of matrix and interface.http://dx.doi.org/10.1155/2016/6364205
spellingShingle Weihan Wang
Weifang Zhang
Shengwang Liu
Xiaoshuai Jin
Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology
Shock and Vibration
title Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology
title_full Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology
title_fullStr Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology
title_full_unstemmed Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology
title_short Investigation on the Behavior of Tensile Damage Evolution in T700/6808 Composite Based on Acoustic Emission Technology
title_sort investigation on the behavior of tensile damage evolution in t700 6808 composite based on acoustic emission technology
url http://dx.doi.org/10.1155/2016/6364205
work_keys_str_mv AT weihanwang investigationonthebehavioroftensiledamageevolutionint7006808compositebasedonacousticemissiontechnology
AT weifangzhang investigationonthebehavioroftensiledamageevolutionint7006808compositebasedonacousticemissiontechnology
AT shengwangliu investigationonthebehavioroftensiledamageevolutionint7006808compositebasedonacousticemissiontechnology
AT xiaoshuaijin investigationonthebehavioroftensiledamageevolutionint7006808compositebasedonacousticemissiontechnology