Durability Improvement of Co-cured Carbon/Epoxy Composite-Aluminum Laminate With Nano-size Carbon Black at Cryogenic Temperature

Cited 7 time in webofscience Cited 0 time in scopus
  • Hit : 392
  • Download : 0
DC FieldValueLanguage
dc.contributor.authorLee, Kwan-Hoko
dc.contributor.authorKim, Byoung-Jungko
dc.contributor.authorYoon, Soon-Hoko
dc.contributor.authorLee, Dai-Gilko
dc.date.accessioned2013-03-11T20:26:22Z-
dc.date.available2013-03-11T20:26:22Z-
dc.date.created2012-02-06-
dc.date.created2012-02-06-
dc.date.issued2009-
dc.identifier.citationJOURNAL OF ADHESION SCIENCE AND TECHNOLOGY, v.23, no.4, pp.639 - 649-
dc.identifier.issn0169-4243-
dc.identifier.urihttp://hdl.handle.net/10203/100182-
dc.description.abstractSince metal foils such as aluminum, copper or nickel foils have been used in composite structures for radiation shielding and EMI protection in space environments, high adhesive bonding strength and durability between metal foils and composites under large temperature variations are very important. In this study, the strength of co-cure bonded joint between an aluminum foil and a composite has been investigated, with three different aluminum surface treatments such as standard PAA (Phosphoric Acid Anodization) procedure, abrasion with sandpaper, and carbon black pasting on the metal foils. From the double cantilever beam (DCB) tests, it was found that the interlaminar peel strength with carbon black pasting improved 60% compared to the laminate without any surface treatment. Also it was found that the interlaminar peel strength of the co-cure carbon/epoxy composite-aluminum foil hybrid laminate with the carbon black pasting on the aluminum foil did not decrease after many thermal cycles from 30 degrees C to -196 degrees C. (C) Koninklijke Brill NV, Leiden, 2009-
dc.languageEnglish-
dc.publisherBRILL ACADEMIC PUBLISHERS-
dc.subjectSINGLE LAP JOINTS-
dc.subjectSURFACE-ROUGHNESS-
dc.titleDurability Improvement of Co-cured Carbon/Epoxy Composite-Aluminum Laminate With Nano-size Carbon Black at Cryogenic Temperature-
dc.typeArticle-
dc.identifier.wosid000265356600010-
dc.identifier.scopusid2-s2.0-77949660113-
dc.type.rimsART-
dc.citation.volume23-
dc.citation.issue4-
dc.citation.beginningpage639-
dc.citation.endingpage649-
dc.citation.publicationnameJOURNAL OF ADHESION SCIENCE AND TECHNOLOGY-
dc.identifier.doi10.1163/156856108X379146-
dc.contributor.localauthorLee, Dai-Gil-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorSpace-
dc.subject.keywordAuthorlaminate-
dc.subject.keywordAuthorinterlaminar peel strength-
dc.subject.keywordAuthorthermal cycle-
dc.subject.keywordAuthornano-size carbon black-
dc.subject.keywordPlusSINGLE LAP JOINTS-
dc.subject.keywordPlusSURFACE-ROUGHNESS-
Appears in Collection
ME-Journal Papers(저널논문)
Files in This Item
There are no files associated with this item.
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡ Click to see webofscience_button
⊙ Cited 7 items in WoS Click to see citing articles in records_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0