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dc.contributor.authorDağ, Tolunay
dc.contributor.authorYıldırım, Nur
dc.contributor.authorŞentürk, Gökhan
dc.contributor.authorDurmazoğlu, Metin
dc.contributor.authorYıldırım, Serap
dc.contributor.authorUyaner, Mesut
dc.date.accessioned2023-12-11T13:05:04Z
dc.date.available2023-12-11T13:05:04Z
dc.date.issued2023en_US
dc.identifier.citationDag, T., Yildirim, N., Senturk, G., Durmazoglu, M., Yildirim, S., Uyaner, M. (2023). Virtual Investigation on the Response of Glare to Low Velocity Impact. Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST.en_US
dc.identifier.isbn979-835032302-3
dc.identifier.urihttps://hdl.handle.net/20.500.12508/2625
dc.description.abstractDue to the increasing cost of experiments and the increased time required to complete the experimental process, it is more economical to conduct experiments in the form of virtual tests. Therefore, low velocity impact simulation was carried out on fiber metal laminates, FMLs with an impactor with various weights in our study. LS-DYNA software was selected to perform the simulation. Fiber metal laminate is composed of 2024-T3 Aluminum and Glass/Epoxy layers. The layers are modeled as isotropic, and anisotropic material. The stacking sequence of FML is (Al/0/90/Al). Two opposite sides of the square shaped FML are fixed and the other sides are left free. Steel strikers with masses of 0.15 kg, 0.30 kg and 0.45 kg were used in the analyses, respectively. The speed of the striker at first contact with the FML is 10 mm/ms. As a result of the tests, force-time, force-displacement, velocity-time and energy - time variations were also obtained. The results were presented as graphs. It has been found that the FML structure absorbs an average of 73.4% of the impact energy because of the low-velocity impact, thus preserving the integrity and functionality of the designed structure. Thanks to such numerical experiments carried out before production, the mechanical properties of the designed structure can be evaluated.en_US
dc.language.isoengen_US
dc.publisherInstitute of Electrical and Electronics Engineers Inc.en_US
dc.relation.isversionof10.1109/RAST57548.2023.10198016en_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectCompositeen_US
dc.subjectFiber metal laminatesen_US
dc.subjectGlareen_US
dc.subjectLow velocity impacten_US
dc.subjectls-dynaen_US
dc.subject.classificationMetal Fibers
dc.subject.classificationLaminates
dc.subject.classificationAluminum
dc.subject.classificationEngineering & Materials Science - Mechanics - Delamination
dc.subject.otherComputer software
dc.subject.otherLaminated composites
dc.subject.otherVirtual reality
dc.subject.other2024-T3 aluminium
dc.subject.other2024-T3 aluminum
dc.subject.otherFibre metal laminates
dc.subject.otherGlass epoxy
dc.subject.otherImpact simulation
dc.subject.otherImpactors
dc.subject.otherIncreasing costs
dc.subject.otherLow velocity impact
dc.subject.otherLS-DYNA
dc.subject.otherVirtual tests
dc.titleVirtual Investigation on the Response of Glare to Low Velocity Impacten_US
dc.typeconferenceObjecten_US
dc.relation.journalProceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023en_US
dc.contributor.departmentHavacılık ve Uzay Bilimleri Fakültesi -- Havacılık ve Uzay Mühendisliği Bölümüen_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.contributor.isteauthorDağ, Tolunay
dc.relation.indexWeb of Science - Scopusen_US
dc.relation.indexWeb of Science Core Collection - Conference Proceedings Citation Index – Science


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