Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike
Damage is inflicted in a series of carbon fiber/epoxy composite specimens using a simulated lightning strike generator in the effort to understand the fundamental damage response of this material form. The strikes up to 50,000 A and 28,000 V are inflicted on both pristine specimens and specimens con...
Gespeichert in:
Veröffentlicht in: | Composites. Part A, Applied science and manufacturing Applied science and manufacturing, 2009-07, Vol.40 (6), p.954-967 |
---|---|
Hauptverfasser: | , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 967 |
---|---|
container_issue | 6 |
container_start_page | 954 |
container_title | Composites. Part A, Applied science and manufacturing |
container_volume | 40 |
creator | Feraboli, Paolo Miller, Mark |
description | Damage is inflicted in a series of carbon fiber/epoxy composite specimens using a simulated lightning strike generator in the effort to understand the fundamental damage response of this material form. The strikes up to 50,000
A and 28,000
V are inflicted on both pristine specimens and specimens containing a Hilok stainless steel fastener. Damage area is evaluated via ultrasonic scanning, and advanced optical microscopy is used to gain further understanding in the morphology of damage. Subsequent mechanical testing to assess the residual tensile and compressive strength and modulus of the material is performed according to ASTM standards. Results show that residual tension strength counter intuitively increases after the infliction of damage, while residual compressive strength is much more dramatically and negatively affected. Furthermore, the presence of the fastener influences dramatically both the state of damage in the specimen and its residual strength by spreading throughout the thickness rather than limiting it to the specimen surface. |
doi_str_mv | 10.1016/j.compositesa.2009.04.025 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_903624388</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S1359835X09001249</els_id><sourcerecordid>34411128</sourcerecordid><originalsourceid>FETCH-LOGICAL-c480t-9b37f261a7310f3d9253065341afa05bc14c48229c7b6046fd52f760c73467673</originalsourceid><addsrcrecordid>eNqNkc1u1TAQRiNUJErhHcKCsko6_omTLNEt0EqVugGJneU444svSRw8SUXfHqe3qlhVXXlGOjNjfSfLPjAoGTB1cShtGOdAfkEyJQdoS5Al8OpVdsqauimqRsJJqkXVFo2ofr7J3hIdAECIlp1m_tKMZo95RPK0mMlibqY-X8KA8aELLrcmdmG6wDn8vc-fzqVqncNEOa3dAe2C21ROflwHszWD3_9aJj_tc1qi_43vstfODITvH9-z7MfXL993V8XN7bfr3eebwsoGlqLtRO24YqYWDJzoW14JUJWQzDgDVWeZTCDnra07BVK5vuKuVmBrIVWtanGWfTrunWP4syItevRkcRjMhGEl3YJQXIqmSeT5s6SQkjHGN7A9gjYGoohOz9GPJt5rBnrToA_6Pw1606BB6qQhzX58PGLImsFtqXp6WsCZapKm7du7I4cpmzuPUZP1mAz0PqZ0dR_8C679A2nVpTc</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>34411128</pqid></control><display><type>article</type><title>Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike</title><source>ScienceDirect Journals (5 years ago - present)</source><creator>Feraboli, Paolo ; Miller, Mark</creator><creatorcontrib>Feraboli, Paolo ; Miller, Mark</creatorcontrib><description>Damage is inflicted in a series of carbon fiber/epoxy composite specimens using a simulated lightning strike generator in the effort to understand the fundamental damage response of this material form. The strikes up to 50,000
A and 28,000
V are inflicted on both pristine specimens and specimens containing a Hilok stainless steel fastener. Damage area is evaluated via ultrasonic scanning, and advanced optical microscopy is used to gain further understanding in the morphology of damage. Subsequent mechanical testing to assess the residual tensile and compressive strength and modulus of the material is performed according to ASTM standards. Results show that residual tension strength counter intuitively increases after the infliction of damage, while residual compressive strength is much more dramatically and negatively affected. Furthermore, the presence of the fastener influences dramatically both the state of damage in the specimen and its residual strength by spreading throughout the thickness rather than limiting it to the specimen surface.</description><identifier>ISSN: 1359-835X</identifier><identifier>EISSN: 1878-5840</identifier><identifier>DOI: 10.1016/j.compositesa.2009.04.025</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>A. Carbon fiber ; Application fields ; Applied sciences ; B. Damage tolerance ; Damage resistance ; Exact sciences and technology ; Lightning strike ; Polymer industry, paints, wood ; Technology of polymers</subject><ispartof>Composites. Part A, Applied science and manufacturing, 2009-07, Vol.40 (6), p.954-967</ispartof><rights>2009 Elsevier Ltd</rights><rights>2015 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c480t-9b37f261a7310f3d9253065341afa05bc14c48229c7b6046fd52f760c73467673</citedby><cites>FETCH-LOGICAL-c480t-9b37f261a7310f3d9253065341afa05bc14c48229c7b6046fd52f760c73467673</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.compositesa.2009.04.025$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>315,781,785,3551,27929,27930,46000</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=21688787$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Feraboli, Paolo</creatorcontrib><creatorcontrib>Miller, Mark</creatorcontrib><title>Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike</title><title>Composites. Part A, Applied science and manufacturing</title><description>Damage is inflicted in a series of carbon fiber/epoxy composite specimens using a simulated lightning strike generator in the effort to understand the fundamental damage response of this material form. The strikes up to 50,000
A and 28,000
V are inflicted on both pristine specimens and specimens containing a Hilok stainless steel fastener. Damage area is evaluated via ultrasonic scanning, and advanced optical microscopy is used to gain further understanding in the morphology of damage. Subsequent mechanical testing to assess the residual tensile and compressive strength and modulus of the material is performed according to ASTM standards. Results show that residual tension strength counter intuitively increases after the infliction of damage, while residual compressive strength is much more dramatically and negatively affected. Furthermore, the presence of the fastener influences dramatically both the state of damage in the specimen and its residual strength by spreading throughout the thickness rather than limiting it to the specimen surface.</description><subject>A. Carbon fiber</subject><subject>Application fields</subject><subject>Applied sciences</subject><subject>B. Damage tolerance</subject><subject>Damage resistance</subject><subject>Exact sciences and technology</subject><subject>Lightning strike</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>1359-835X</issn><issn>1878-5840</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2009</creationdate><recordtype>article</recordtype><recordid>eNqNkc1u1TAQRiNUJErhHcKCsko6_omTLNEt0EqVugGJneU444svSRw8SUXfHqe3qlhVXXlGOjNjfSfLPjAoGTB1cShtGOdAfkEyJQdoS5Al8OpVdsqauimqRsJJqkXVFo2ofr7J3hIdAECIlp1m_tKMZo95RPK0mMlibqY-X8KA8aELLrcmdmG6wDn8vc-fzqVqncNEOa3dAe2C21ROflwHszWD3_9aJj_tc1qi_43vstfODITvH9-z7MfXL993V8XN7bfr3eebwsoGlqLtRO24YqYWDJzoW14JUJWQzDgDVWeZTCDnra07BVK5vuKuVmBrIVWtanGWfTrunWP4syItevRkcRjMhGEl3YJQXIqmSeT5s6SQkjHGN7A9gjYGoohOz9GPJt5rBnrToA_6Pw1606BB6qQhzX58PGLImsFtqXp6WsCZapKm7du7I4cpmzuPUZP1mAz0PqZ0dR_8C679A2nVpTc</recordid><startdate>20090701</startdate><enddate>20090701</enddate><creator>Feraboli, Paolo</creator><creator>Miller, Mark</creator><general>Elsevier Ltd</general><general>Elsevier</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>F28</scope><scope>FR3</scope><scope>JG9</scope></search><sort><creationdate>20090701</creationdate><title>Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike</title><author>Feraboli, Paolo ; Miller, Mark</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c480t-9b37f261a7310f3d9253065341afa05bc14c48229c7b6046fd52f760c73467673</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2009</creationdate><topic>A. Carbon fiber</topic><topic>Application fields</topic><topic>Applied sciences</topic><topic>B. Damage tolerance</topic><topic>Damage resistance</topic><topic>Exact sciences and technology</topic><topic>Lightning strike</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Feraboli, Paolo</creatorcontrib><creatorcontrib>Miller, Mark</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><jtitle>Composites. Part A, Applied science and manufacturing</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Feraboli, Paolo</au><au>Miller, Mark</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike</atitle><jtitle>Composites. Part A, Applied science and manufacturing</jtitle><date>2009-07-01</date><risdate>2009</risdate><volume>40</volume><issue>6</issue><spage>954</spage><epage>967</epage><pages>954-967</pages><issn>1359-835X</issn><eissn>1878-5840</eissn><abstract>Damage is inflicted in a series of carbon fiber/epoxy composite specimens using a simulated lightning strike generator in the effort to understand the fundamental damage response of this material form. The strikes up to 50,000
A and 28,000
V are inflicted on both pristine specimens and specimens containing a Hilok stainless steel fastener. Damage area is evaluated via ultrasonic scanning, and advanced optical microscopy is used to gain further understanding in the morphology of damage. Subsequent mechanical testing to assess the residual tensile and compressive strength and modulus of the material is performed according to ASTM standards. Results show that residual tension strength counter intuitively increases after the infliction of damage, while residual compressive strength is much more dramatically and negatively affected. Furthermore, the presence of the fastener influences dramatically both the state of damage in the specimen and its residual strength by spreading throughout the thickness rather than limiting it to the specimen surface.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.compositesa.2009.04.025</doi><tpages>14</tpages></addata></record> |
fulltext | fulltext |
identifier | ISSN: 1359-835X |
ispartof | Composites. Part A, Applied science and manufacturing, 2009-07, Vol.40 (6), p.954-967 |
issn | 1359-835X 1878-5840 |
language | eng |
recordid | cdi_proquest_miscellaneous_903624388 |
source | ScienceDirect Journals (5 years ago - present) |
subjects | A. Carbon fiber Application fields Applied sciences B. Damage tolerance Damage resistance Exact sciences and technology Lightning strike Polymer industry, paints, wood Technology of polymers |
title | Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lightning strike |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-15T18%3A10%3A30IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Damage%20resistance%20and%20tolerance%20of%20carbon/epoxy%20composite%20coupons%20subjected%20to%20simulated%20lightning%20strike&rft.jtitle=Composites.%20Part%20A,%20Applied%20science%20and%20manufacturing&rft.au=Feraboli,%20Paolo&rft.date=2009-07-01&rft.volume=40&rft.issue=6&rft.spage=954&rft.epage=967&rft.pages=954-967&rft.issn=1359-835X&rft.eissn=1878-5840&rft_id=info:doi/10.1016/j.compositesa.2009.04.025&rft_dat=%3Cproquest_cross%3E34411128%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=34411128&rft_id=info:pmid/&rft_els_id=S1359835X09001249&rfr_iscdi=true |