A novel process-linked assembly failure model for adhesively bonded composite structures

dc.contributor.authorYazdani Nezhad, Hamed
dc.contributor.authorZhao, Yifan
dc.contributor.authorLiddel, Paul D.
dc.contributor.authorMarchante, Veronica
dc.contributor.authorRoy, Rajkumar
dc.date.accessioned2017-09-12T14:18:52Z
dc.date.available2017-09-12T14:18:52Z
dc.date.issued2017-04-24
dc.description.abstractThe globally growing market for polymer composites and their increasing use within aircraft structures has necessitated reliable bonding of composite laminates to prevent structural failure. However, knowledge behind the interaction between curing process parameters and the failure of polymer composite bonded joints is not keeping pace with the market. A novel nonlinear correlation analysis has been employed and applied to experimental data, to attentively quantify the effect of curing parameters on the failure of bonded composite assemblies. The materials (adherends and adhesive) and the bonding processes were selected from those used in assembly of composite aircraft structures.en_UK
dc.identifier.citationYazdani Nezhad H, Zhao Y, Liddel PD, et al., (2017) A novel process-linked assembly failure model for adhesively bonded composite structures. CIRP Annals - Manufacturing Technology, Volume 66, Issue 1, 2017, pp. 29-32en_UK
dc.identifier.issn0007-8506
dc.identifier.urihttp://dx.doi.org/10.1016/j.cirp.2017.04.103
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/12472
dc.language.isoenen_UK
dc.publisherElsevieren_UK
dc.rightsAttribution 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectBondingen_UK
dc.subjectAssemblyen_UK
dc.subjectCompositeen_UK
dc.titleA novel process-linked assembly failure model for adhesively bonded composite structuresen_UK
dc.typeArticleen_UK

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