No Cover Image

Journal article 995 views 181 downloads

High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction

E. Rolfe, C. Kaboglu, R. Quinn, P. A. Hooper, H. Arora, J. P. Dear, Hari Arora Orcid Logo

Journal of Dynamic Behavior of Materials, Volume: 4, Issue: 3, Pages: 359 - 372

Swansea University Author: Hari Arora Orcid Logo

  • rolfe2018(2).pdf

    PDF | Version of Record

    Released under the terms of a Creative Commons Attribution 4.0 International License (CC-BY).

    Download (7.11MB)

Check full text

DOI (Published version): 10.1007/s40870-018-0163-5

Abstract

This research investigates whether the layup order of the carbon-fibre/glass-fibre skins in hybrid composite sandwich panels has an effect on impact response. Composite sandwich panels with carbon-fibre/glass-fibre hybrid skins were subjected to impact at velocities of 75 ± 3 and 90 ± 3 m s−1. Measu...

Full description

Published in: Journal of Dynamic Behavior of Materials
ISSN: 2199-7446 2199-7454
Published: 2018
Online Access: Check full text

URI: https://cronfa.swan.ac.uk/Record/cronfa40929
Tags: Add Tag
No Tags, Be the first to tag this record!
first_indexed 2018-07-05T13:41:36Z
last_indexed 2018-09-11T12:55:50Z
id cronfa40929
recordtype SURis
fullrecord <?xml version="1.0"?><rfc1807><datestamp>2018-09-11T11:48:54.9048464</datestamp><bib-version>v2</bib-version><id>40929</id><entry>2018-07-05</entry><title>High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction</title><swanseaauthors><author><sid>ed7371c768e9746008a6807f9f7a1555</sid><ORCID>0000-0002-9790-0907</ORCID><firstname>Hari</firstname><surname>Arora</surname><name>Hari Arora</name><active>true</active><ethesisStudent>false</ethesisStudent></author></swanseaauthors><date>2018-07-05</date><deptcode>MEDE</deptcode><abstract>This research investigates whether the layup order of the carbon-fibre/glass-fibre skins in hybrid composite sandwich panels has an effect on impact response. Composite sandwich panels with carbon-fibre/glass-fibre hybrid skins were subjected to impact at velocities of 75&#x2009;&#xB1;&#x2009;3 and 90&#x2009;&#xB1;&#x2009;3 m s&#x2212;1. Measurements of the sandwich panels were made using high-speed 3D digital image correlation (DIC), and post-impact damage was assessed by sectioning the sandwich panels. It was concluded that the introduction of glass-fibre layers into carbon-fibre laminate skins reduces brittle failure compared to a sandwich panel with carbon-fibre reinforced polymer skins alone. Furthermore, if the impact surface is known, it would be beneficial to select an asymmetrical panel such as Hybrid-(GCFGC) utilising glass-fibre layers in compression and carbon-fibre layers in tension. This hybrid sandwich panel achieves a specific deflection of 0.322 mm kg&#x2212;1 m2 and specific strain of 0.077% kg&#x2212;1 m2 under an impact velocity of 75&#x2009;&#xB1;&#x2009;3 m s&#x2212;1. However, if the impact surface is not known, selection of a panel with a symmetric yet more dispersed hybridisation would be effective. By distributing the different fibre layers more evenly within the skin, less surface and core damage is achieved. The distributed hybrid investigated in this research, Hybrid-(GCGFGCG), achieved a specific deflection of 0.394 mm kg&#x2212;1 m2 and specific strain of 0.085% kg&#x2212;1 m2 under an impact velocity of 75&#x2009;&#xB1;&#x2009;3 m s&#x2212;1. Blast loading was performed on a large scale version of Hybrid-(GCFGC) and it exhibited a maximum deflection of 75 mm following a similar deflection profile to those observed for the impact experiments.</abstract><type>Journal Article</type><journal>Journal of Dynamic Behavior of Materials</journal><volume>4</volume><journalNumber>3</journalNumber><paginationStart>359</paginationStart><paginationEnd>372</paginationEnd><publisher/><issnPrint>2199-7446</issnPrint><issnElectronic>2199-7454</issnElectronic><keywords>Impact, Blast, Hybrid composite, Composite sandwich</keywords><publishedDay>31</publishedDay><publishedMonth>12</publishedMonth><publishedYear>2018</publishedYear><publishedDate>2018-12-31</publishedDate><doi>10.1007/s40870-018-0163-5</doi><url/><notes/><college>COLLEGE NANME</college><department>Biomedical Engineering</department><CollegeCode>COLLEGE CODE</CollegeCode><DepartmentCode>MEDE</DepartmentCode><institution>Swansea University</institution><apcterm/><lastEdited>2018-09-11T11:48:54.9048464</lastEdited><Created>2018-07-05T09:05:08.1330793</Created><authors><author><firstname>E.</firstname><surname>Rolfe</surname><order>1</order></author><author><firstname>C.</firstname><surname>Kaboglu</surname><order>2</order></author><author><firstname>R.</firstname><surname>Quinn</surname><order>3</order></author><author><firstname>P. A.</firstname><surname>Hooper</surname><order>4</order></author><author><firstname>H.</firstname><surname>Arora</surname><order>5</order></author><author><firstname>J. P.</firstname><surname>Dear</surname><order>6</order></author><author><firstname>Hari</firstname><surname>Arora</surname><orcid>0000-0002-9790-0907</orcid><order>7</order></author></authors><documents><document><filename>0040929-24072018085527.pdf</filename><originalFilename>rolfe2018(2).pdf</originalFilename><uploaded>2018-07-24T08:55:27.9070000</uploaded><type>Output</type><contentLength>7472462</contentLength><contentType>application/pdf</contentType><version>Version of Record</version><cronfaStatus>true</cronfaStatus><embargoDate>2018-07-24T00:00:00.0000000</embargoDate><documentNotes>Released under the terms of a Creative Commons Attribution 4.0 International License (CC-BY).</documentNotes><copyrightCorrect>true</copyrightCorrect><language>eng</language></document></documents><OutputDurs/></rfc1807>
spelling 2018-09-11T11:48:54.9048464 v2 40929 2018-07-05 High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction ed7371c768e9746008a6807f9f7a1555 0000-0002-9790-0907 Hari Arora Hari Arora true false 2018-07-05 MEDE This research investigates whether the layup order of the carbon-fibre/glass-fibre skins in hybrid composite sandwich panels has an effect on impact response. Composite sandwich panels with carbon-fibre/glass-fibre hybrid skins were subjected to impact at velocities of 75 ± 3 and 90 ± 3 m s−1. Measurements of the sandwich panels were made using high-speed 3D digital image correlation (DIC), and post-impact damage was assessed by sectioning the sandwich panels. It was concluded that the introduction of glass-fibre layers into carbon-fibre laminate skins reduces brittle failure compared to a sandwich panel with carbon-fibre reinforced polymer skins alone. Furthermore, if the impact surface is known, it would be beneficial to select an asymmetrical panel such as Hybrid-(GCFGC) utilising glass-fibre layers in compression and carbon-fibre layers in tension. This hybrid sandwich panel achieves a specific deflection of 0.322 mm kg−1 m2 and specific strain of 0.077% kg−1 m2 under an impact velocity of 75 ± 3 m s−1. However, if the impact surface is not known, selection of a panel with a symmetric yet more dispersed hybridisation would be effective. By distributing the different fibre layers more evenly within the skin, less surface and core damage is achieved. The distributed hybrid investigated in this research, Hybrid-(GCGFGCG), achieved a specific deflection of 0.394 mm kg−1 m2 and specific strain of 0.085% kg−1 m2 under an impact velocity of 75 ± 3 m s−1. Blast loading was performed on a large scale version of Hybrid-(GCFGC) and it exhibited a maximum deflection of 75 mm following a similar deflection profile to those observed for the impact experiments. Journal Article Journal of Dynamic Behavior of Materials 4 3 359 372 2199-7446 2199-7454 Impact, Blast, Hybrid composite, Composite sandwich 31 12 2018 2018-12-31 10.1007/s40870-018-0163-5 COLLEGE NANME Biomedical Engineering COLLEGE CODE MEDE Swansea University 2018-09-11T11:48:54.9048464 2018-07-05T09:05:08.1330793 E. Rolfe 1 C. Kaboglu 2 R. Quinn 3 P. A. Hooper 4 H. Arora 5 J. P. Dear 6 Hari Arora 0000-0002-9790-0907 7 0040929-24072018085527.pdf rolfe2018(2).pdf 2018-07-24T08:55:27.9070000 Output 7472462 application/pdf Version of Record true 2018-07-24T00:00:00.0000000 Released under the terms of a Creative Commons Attribution 4.0 International License (CC-BY). true eng
title High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction
spellingShingle High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction
Hari Arora
title_short High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction
title_full High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction
title_fullStr High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction
title_full_unstemmed High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction
title_sort High Velocity Impact and Blast Loading of Composite Sandwich Panels with Novel Carbon and Glass Construction
author_id_str_mv ed7371c768e9746008a6807f9f7a1555
author_id_fullname_str_mv ed7371c768e9746008a6807f9f7a1555_***_Hari Arora
author Hari Arora
author2 E. Rolfe
C. Kaboglu
R. Quinn
P. A. Hooper
H. Arora
J. P. Dear
Hari Arora
format Journal article
container_title Journal of Dynamic Behavior of Materials
container_volume 4
container_issue 3
container_start_page 359
publishDate 2018
institution Swansea University
issn 2199-7446
2199-7454
doi_str_mv 10.1007/s40870-018-0163-5
document_store_str 1
active_str 0
description This research investigates whether the layup order of the carbon-fibre/glass-fibre skins in hybrid composite sandwich panels has an effect on impact response. Composite sandwich panels with carbon-fibre/glass-fibre hybrid skins were subjected to impact at velocities of 75 ± 3 and 90 ± 3 m s−1. Measurements of the sandwich panels were made using high-speed 3D digital image correlation (DIC), and post-impact damage was assessed by sectioning the sandwich panels. It was concluded that the introduction of glass-fibre layers into carbon-fibre laminate skins reduces brittle failure compared to a sandwich panel with carbon-fibre reinforced polymer skins alone. Furthermore, if the impact surface is known, it would be beneficial to select an asymmetrical panel such as Hybrid-(GCFGC) utilising glass-fibre layers in compression and carbon-fibre layers in tension. This hybrid sandwich panel achieves a specific deflection of 0.322 mm kg−1 m2 and specific strain of 0.077% kg−1 m2 under an impact velocity of 75 ± 3 m s−1. However, if the impact surface is not known, selection of a panel with a symmetric yet more dispersed hybridisation would be effective. By distributing the different fibre layers more evenly within the skin, less surface and core damage is achieved. The distributed hybrid investigated in this research, Hybrid-(GCGFGCG), achieved a specific deflection of 0.394 mm kg−1 m2 and specific strain of 0.085% kg−1 m2 under an impact velocity of 75 ± 3 m s−1. Blast loading was performed on a large scale version of Hybrid-(GCFGC) and it exhibited a maximum deflection of 75 mm following a similar deflection profile to those observed for the impact experiments.
published_date 2018-12-31T03:52:09Z
_version_ 1763752572710027264
score 11.017797

Similar Items