Quantifying the delamination of L-shaped composite laminates under low velocity impact using x-ray computed tomography

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dc.authorscopusid57214703253
dc.authorscopusid6601970288
dc.authorscopusid56258316400
dc.authorscopusid6602432376
dc.contributor.authorÇınar, Kenan
dc.contributor.authorGüven, İbrahim
dc.contributor.authorÖz, Fatih E.
dc.contributor.authorErsoy, N.
dc.date.accessioned2022-05-11T14:26:47Z
dc.date.available2022-05-11T14:26:47Z
dc.date.issued2018
dc.departmentFakülteler, Çorlu Mühendislik Fakültesi, Makine Mühendisliği Bölümü
dc.description33rd Technical Conference of the American Society for Composites 2018 -- 24 September 2018 through 27 September 2018 -- -- 142871
dc.description.abstractLow velocity impact response and failure behavior of L-shaped composite laminates were investigated. The composite laminates with variable thickness, stacking sequences, and corner radius were manufactured using autoclave manufacturing method. Tests were conducted on a custom low velocity impact test set-up. In order to investigate and quantify the internal damage of the samples, x-ray micro-computed tomography technique was used. The results showed that the deflection of cross-ply samples was higher than the unidirectional ones, and as the thickness decreases deflection increases for the same loading conditions. In addition, as the corner radius decreased, the deflection was more pronounced. Delamination migration was observed at the mid-plane of the corner in unidirectional samples while delamination planes largely remained separate and parallel to each other in the cross-ply samples. © Copyright© (2018) by DEStech Publications, Inc. All rights reserved.
dc.identifier.endpage576
dc.identifier.isbn978-1510872073
dc.identifier.scopus2-s2.0-85059310886
dc.identifier.startpage561
dc.identifier.urihttps://hdl.handle.net/20.500.11776/6597
dc.identifier.volume1
dc.indekslendigikaynakScopus
dc.institutionauthorÇınar, Kenan
dc.language.isoen
dc.publisherDEStech Publications Inc.
dc.relation.ispartof33rd Technical Conference of the American Society for Composites 2018
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectComputerized tomography
dc.subjectX rays
dc.subjectComposite laminate
dc.subjectLoading condition
dc.subjectLow velocity impact
dc.subjectLow velocity impact test
dc.subjectManufacturing methods
dc.subjectVariable thickness
dc.subjectX ray micro-computed tomography
dc.subjectX-ray computed tomography
dc.subjectLaminated composites
dc.titleQuantifying the delamination of L-shaped composite laminates under low velocity impact using x-ray computed tomography
dc.typeConference Object

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