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Investigation of failure mechanisms in aged aerospace composites

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dc.contributor.authorFox, Bronwyn
dc.contributor.authorLowe, Adrian
dc.contributor.authorHodgkin, Jonathan
dc.date.accessioned2015-12-13T22:36:23Z
dc.date.available2015-12-13T22:36:23Z
dc.date.issued2004
dc.date.updated2015-12-11T09:31:35Z
dc.description.abstractThe effect of isothermal ageing on two high temperature, bismaleimide composite materials, a novel CSIRO CBR 320/328 composite and a commercial CIBA GEIGY Matrimid® 5292 composite, was examined at 204 and 250-°C. Delamination is a major cause of failure
dc.identifier.issn1350-6307
dc.identifier.urihttp://hdl.handle.net/1885/76736
dc.publisherPergamon-Elsevier Ltd
dc.sourceEngineering Failure Analysis
dc.subjectKeywords: Age hardening; Aromatic compounds; Curing; Degradation; Delamination; Failure analysis; Fourier transform infrared spectroscopy; Fracture toughness; Metallic matrix composites; Oxidation; Raman spectroscopy; Resins; Thermal effects; Double cantilever beam Ageing; Bismaleimide; Composite; Delamination; FTIR
dc.titleInvestigation of failure mechanisms in aged aerospace composites
dc.typeJournal article
local.bibliographicCitation.issue2
local.bibliographicCitation.lastpage241
local.bibliographicCitation.startpage235
local.contributor.affiliationFox, Bronwyn, Deakin University
local.contributor.affiliationLowe, Adrian, College of Engineering and Computer Science, ANU
local.contributor.affiliationHodgkin, Jonathan, Deakin University
local.contributor.authoruidLowe, Adrian, u9504352
local.description.notesImported from ARIES
local.description.refereedYes
local.identifier.absfor091202 - Composite and Hybrid Materials
local.identifier.ariespublicationMigratedxPub5545
local.identifier.citationvolume11
local.identifier.doi10.1016/j.engfailanal.2003.05.010
local.identifier.scopusID2-s2.0-0347930704
local.type.statusPublished Version

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