Fatigue behavior of honeycomb sandwich composites under flexural and buckling loading

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dc.contributor.authorTopkaya, Tolga
dc.contributor.authorSolmaz, Murat Yavuz
dc.date.accessioned2026-08-12T16:09:04Z
dc.date.issued2016
dc.departmentFırat Üniversitesi
dc.description6th International Conference on Advanced Materials and Systems, ICAMS 2016 -- 20 October 2016 through 22 October 2016 -- Bucharest -- 139798
dc.description.abstractThis study experimentally investigated the fatigue behaviors of honeycomb-sandwich composites under buckling and three-point bending loads. The ASTM C 365 and ASTM C 393 standards were used as references to prepare test specimens and conduct experiments. The investigation looked at how the cell diameter, core thickness and thickness of the skin material affected the fatigue behavior. It was observed that the most significant parameter affecting fatigue under buckling loads was the cell diameter, and the least significant parameter affecting fatigue under three-point loads was the thickness of the skin material. © 2016 Certex, INCDTP-ICPI.
dc.identifier.doi10.24264/icams-2016.i.27
dc.identifier.isbn978-194358012-5
dc.identifier.issn2068-0783
dc.identifier.scopus2-s2.0-85047635071
dc.identifier.scopusqualityN/A
dc.identifier.urihttps://doi.org/10.24264/icams-2016.i.27
dc.identifier.urihttps://hdl.handle.net/11508/41561
dc.identifier.volume0
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherCertex, INCDTP-ICPI
dc.relation.ispartofICAMS Proceedings of the International Conference on Advanced Materials and Systems
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_Scopus_20260511
dc.subjectFatigue; Honeycomb; Sandwich composites
dc.titleFatigue behavior of honeycomb sandwich composites under flexural and buckling loading
dc.typeConference Object

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