Study of Impact Damage Behavior in Woven Carbon Fiber Plates
Composites are being used extensively in aerospace structures as their properties offer significant advantages such as better strength to weight capacity. However, failure in composite structures due to low-velocity impact raises a maintenance concern because it can lead to an invisible damage. Henc...
| 發表在: | Procedia Engineering |
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| 主要作者: | |
| 格式: | Conference paper |
| 語言: | English |
| 出版: |
Elsevier Ltd
2017
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| 在線閱讀: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-85022011940&doi=10.1016%2fj.proeng.2017.03.009&partnerID=40&md5=4004a7c65066c23aed5331c55777fc9f |
| id |
Murat B.I.S.; Rahman A.A.A. |
|---|---|
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Murat B.I.S.; Rahman A.A.A. 2-s2.0-85022011940 Study of Impact Damage Behavior in Woven Carbon Fiber Plates 2017 Procedia Engineering 170 10.1016/j.proeng.2017.03.009 https://www.scopus.com/inward/record.uri?eid=2-s2.0-85022011940&doi=10.1016%2fj.proeng.2017.03.009&partnerID=40&md5=4004a7c65066c23aed5331c55777fc9f Composites are being used extensively in aerospace structures as their properties offer significant advantages such as better strength to weight capacity. However, failure in composite structures due to low-velocity impact raises a maintenance concern because it can lead to an invisible damage. Hence, the objective of this study is to investigate impact damage behavior in woven composite plates via microscopic examinations. Several specimens were fabricated and were subjected to different levels of impact energy. Scanning Electron Microscopy (SEM) and X-ray imaging were used to examine the impacted area. The results showed that the impact damage is dependent on the plate thickness and also the impact energy. The outcome of this research will help to establish an efficient modelling technique for non-destructive evaluation of composites. © 2017 Published by Elsevier Ltd. Elsevier Ltd 18777058 English Conference paper All Open Access; Gold Open Access |
| author |
2-s2.0-85022011940 |
| spellingShingle |
2-s2.0-85022011940 Study of Impact Damage Behavior in Woven Carbon Fiber Plates |
| author_facet |
2-s2.0-85022011940 |
| author_sort |
2-s2.0-85022011940 |
| title |
Study of Impact Damage Behavior in Woven Carbon Fiber Plates |
| title_short |
Study of Impact Damage Behavior in Woven Carbon Fiber Plates |
| title_full |
Study of Impact Damage Behavior in Woven Carbon Fiber Plates |
| title_fullStr |
Study of Impact Damage Behavior in Woven Carbon Fiber Plates |
| title_full_unstemmed |
Study of Impact Damage Behavior in Woven Carbon Fiber Plates |
| title_sort |
Study of Impact Damage Behavior in Woven Carbon Fiber Plates |
| publishDate |
2017 |
| container_title |
Procedia Engineering |
| container_volume |
170 |
| container_issue |
|
| doi_str_mv |
10.1016/j.proeng.2017.03.009 |
| url |
https://www.scopus.com/inward/record.uri?eid=2-s2.0-85022011940&doi=10.1016%2fj.proeng.2017.03.009&partnerID=40&md5=4004a7c65066c23aed5331c55777fc9f |
| description |
Composites are being used extensively in aerospace structures as their properties offer significant advantages such as better strength to weight capacity. However, failure in composite structures due to low-velocity impact raises a maintenance concern because it can lead to an invisible damage. Hence, the objective of this study is to investigate impact damage behavior in woven composite plates via microscopic examinations. Several specimens were fabricated and were subjected to different levels of impact energy. Scanning Electron Microscopy (SEM) and X-ray imaging were used to examine the impacted area. The results showed that the impact damage is dependent on the plate thickness and also the impact energy. The outcome of this research will help to establish an efficient modelling technique for non-destructive evaluation of composites. © 2017 Published by Elsevier Ltd. |
| publisher |
Elsevier Ltd |
| issn |
18777058 |
| language |
English |
| format |
Conference paper |
| accesstype |
All Open Access; Gold Open Access |
| record_format |
scopus |
| collection |
Scopus |
| _version_ |
1828987880174780416 |