Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/10455
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dc.contributor.authorMert, Sinem K.-
dc.contributor.authorGüler, Mehmet Ali-
dc.contributor.authorAltın, Murat-
dc.contributor.authorAcar, Erdem-
dc.contributor.authorÇiçek, Adem-
dc.date.accessioned2023-07-14T20:17:03Z-
dc.date.available2023-07-14T20:17:03Z-
dc.date.issued2023-
dc.identifier.issn1678-5878-
dc.identifier.issn1806-3691-
dc.identifier.urihttps://doi.org/10.1007/s40430-023-04180-3-
dc.identifier.urihttps://hdl.handle.net/20.500.11851/10455-
dc.description.abstractMetal/composite hybrid tubes are potential candidates for crashworthy products having less weight and low cost compared to conventional crash boxes. The crashworthiness of Al/GFRP tubes created by wrapping an aluminum 6082 tube in glass fiber-reinforced plastic is the subject of this investigation. To compare the crush behavior of the empty GFRP/hybrid and honeycomb-filled hybrid circular tubes, quasi-static tests were conducted. Bundles and cracks were observed during the tests of composite and hybrid tubes. Energy absorption parameters of the numerical model were compared with the results of experiments. The crushing behavior of the GFRP and hybrid specimens was simulated using a numerical approach based on the Chang-Chang damage criteria. It is found that trigger mechanisms performed in the FE analysis can effectively model the crashing behavior of GFRP/hybrid specimens. The CFE and SEA of the empty composite tube are 95% and 29% greater than the empty hybrid tube, respectively. The effect of honeycomb filling on the energy absorption capabilities of hybrid tubes is investigated. The CFE of the honeycomb-filled hybrid tube is found to be 4.5% greater than the CFE of the empty hybrid tube.en_US
dc.description.sponsorshipAnkara Yildirim Beyazit University, Department of Scientific Research Projects [5582]en_US
dc.description.sponsorshipThe authors acknowledge the financial support provided by Ankara Yildirim Beyazit University, Department of Scientific Research Projects under Project No: 5582. The authors would like to express their gratitude to Hexagon Space Aviation Trade Ltd. for providing honeycomb aluminum fillers and Prof. Dr. Metin Tanoglu and Murat Aydin for their contribution to characterization tests. Also, we would like to express our gratitude to Ameen Topa for his valuable, constructive criticisms during the modeling.en_US
dc.language.isoenen_US
dc.publisherSpringer Heidelbergen_US
dc.relation.ispartofJournal of the Brazilian Society of Mechanical Sciences and Engineeringen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectCrashworthinessen_US
dc.subjectEnergy absorptionen_US
dc.subjectAlen_US
dc.subjectGFRP hybrid tubeen_US
dc.subjectHoneycomb fillingen_US
dc.subjectEnergy-Absorption Capabilityen_US
dc.subjectAxial Crushing Responseen_US
dc.subjectCfrp Tubesen_US
dc.subjectNumerical-Analysisen_US
dc.subjectImpact Behavioren_US
dc.subjectCollapseen_US
dc.subjectPerformanceen_US
dc.subjectMechanismsen_US
dc.titleCrashworthiness Evaluation of Hybrid Tubes Made of Gfrp Composite and Aluminum Tubes Filled With Honeycomb Structuresen_US
dc.typeArticleen_US
dc.departmentTOBB ETÜen_US
dc.identifier.volume45en_US
dc.identifier.issue6en_US
dc.authoridGuler, Mehmet A./0000-0002-1159-556X-
dc.authoridAltin, Murat/0000-0002-2404-2614-
dc.identifier.wosWOS:000983313600002en_US
dc.identifier.scopus2-s2.0-85159858529en_US
dc.institutionauthor-
dc.identifier.doi10.1007/s40430-023-04180-3-
dc.authorwosidGuler, Mehmet A./AAB-8799-2019-
dc.authorwosidcicek, adem/HRD-0662-2023-
dc.authorwosidAltin, Murat/Z-1986-2018-
dc.authorscopusid57194850535-
dc.authorscopusid12787816400-
dc.authorscopusid55754304700-
dc.authorscopusid55308448100-
dc.authorscopusid8840024800-
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.identifier.scopusqualityQ2-
item.openairetypeArticle-
item.languageiso639-1en-
item.grantfulltextnone-
item.fulltextNo Fulltext-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.cerifentitytypePublications-
crisitem.author.dept02.7. Department of Mechanical Engineering-
crisitem.author.dept02.7. Department of Mechanical Engineering-
Appears in Collections:Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection
WoS İndeksli Yayınlar Koleksiyonu / WoS Indexed Publications Collection
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