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Predicting residual stiffness of cracked composite laminates subjected to multi-axial inplane loading

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dc.contributor.authorKashtalyan, M
dc.contributor.authorSoutis, C.
dc.contributor.institutionUniversity of Aberdeen.Engineeringen
dc.contributor.institutionUniversity of Aberdeen.Centre for Micro- and Nanomechanics (CEMINACS)en
dc.date.accessioned2017-12-06T17:33:10Z
dc.date.available2017-12-06T17:33:10Z
dc.date.issued2013-09-01
dc.descriptionFunding This research arises from work carried out under EPSRC/GR/L51348 grant. Acknowledgments Financial support from UK’s Engineering and Physical Sciences Research Council is gratefully acknowledged.en
dc.description.statusPeer revieweden
dc.format.extent12
dc.format.extent203364
dc.identifier29869994
dc.identifier7cd7c1f8-1058-49ba-9a94-1aa57f152726
dc.identifier84884584362
dc.identifier.citationKashtalyan, M & Soutis, C 2013, 'Predicting residual stiffness of cracked composite laminates subjected to multi-axial inplane loading', Journal of Composite Materials, vol. 47, no. 20-21, pp. 2513-2524. https://doi.org/10.1177/0021998313488809en
dc.identifier.doi10.1177/0021998313488809
dc.identifier.iss20en
dc.identifier.issn0021-9983
dc.identifier.urihttp://hdl.handle.net/2164/9652
dc.identifier.vol47en
dc.language.isoeng
dc.relation.ispartofJournal of Composite Materialsen
dc.subjectpolymer-matrix composites (PMCs)en
dc.subjectmatrix crackingen
dc.subjectdamage mechanicsen
dc.subjecttransverse crackingen
dc.subjectTA Engineering (General). Civil engineering (General)en
dc.subjectEngineering and Physical Sciences Research Council (EPSRC)en
dc.subjectEPSRC/GR/L51348en
dc.subject.lccTAen
dc.titlePredicting residual stiffness of cracked composite laminates subjected to multi-axial inplane loadingen
dc.typeJournal articleen

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