The flexural fatigue behavior of honeycomb sandwich composites following low velocity impacts

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dc.authorid0000-0001-6650-8067en_US
dc.contributor.authorTopkaya, Tolga
dc.contributor.authorSolmaz, Murat Yavuz
dc.date.accessioned2021-11-24T06:37:39Z
dc.date.available2021-11-24T06:37:39Z
dc.date.issued2020-01-13en_US
dc.departmentBatman Üniversitesi Mühendislik - Mimarlık Fakültesi Makine Mühendisliği Bölümüen_US
dc.description.abstractThis study experimentally investigated the flexural fatigue behaviors of honeycomb sandwich composites subjected to low velocity impact damage by considering the type and thickness of the face sheet material, the cell size and the core height parameters. Carbon-fiber reinforced composite and the aluminum alloy was used as the face sheet material. First, the static strength of undamaged and damaged specimens was determined by three-point bending loads. Secondly, the fatigue behaviors of the damaged and undamaged specimens were determined. Low velocity impact damage decreased the flexural strength and fatigue lives but increased the damping ratio for all specimens. Maximum damping ratio values were observed on specimens with a aluminum face sheet.en_US
dc.identifier.citationTopkaya, T., Solmaz, M.Y. (2020). The flexural fatigue behavior of honeycomb sandwich composites following low velocity impacts. Applied Sciences-Basel, 10 (20), pp.1-14. DOI:https://dx.doi.org/10.3390/app10207262en_US
dc.identifier.endpage14en_US
dc.identifier.issn2076-3417
dc.identifier.issue20en_US
dc.identifier.scopusqualityQ2en_US
dc.identifier.startpage1en_US
dc.identifier.urihttps://dx.doi.org/10.3390/app10207262
dc.identifier.urihttps://hdl.handle.net/20.500.12402/4053
dc.identifier.volume10en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherMDPIen_US
dc.relation.isversionof10.3390/app10207262en_US
dc.relation.journalApplied Sciences-Baselen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.rightsAttribution-NonCommercial-ShareAlike 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/3.0/us/*
dc.subjectHoneycomb Sandwich Compositesen_US
dc.subjectFlexural Testen_US
dc.subjectLow Velocity İmpacten_US
dc.subjectFatigueen_US
dc.titleThe flexural fatigue behavior of honeycomb sandwich composites following low velocity impactsen_US
dc.title.alternativeDüşük hızlı darbeleri takiben petek yapılı sandviç kompozitlerin eğilme yorulma davranışıen_US
dc.typeArticleen_US

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