Virtual Investigation on the Response of Glare to Low Velocity Impact

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dc.contributor.authorDag, Tolunay
dc.contributor.authorYildirim, Nur
dc.contributor.authorSenturk, Gokhan
dc.contributor.authorDurmazoglu, Metin
dc.contributor.authorYildirim, Serap
dc.contributor.authorUyaner, Mesut
dc.date.accessioned2024-02-23T14:23:53Z
dc.date.available2024-02-23T14:23:53Z
dc.date.issued2023
dc.departmentNEÜen_US
dc.description10th International Conference on Recent Advances in Air and Space Technologies (RAST) -- JUN 07-09, 2023 -- Istanbul, TURKEYen_US
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.description.sponsorshipIEEE,NDU Turkish AF Acad,AIAA,AESS,IEEE Geoscience & Remote Sensing Soc,ISPRS,Univ Space Engn Consortium Global,Bayker,Rokestan,ALP Aviat,Aselsan,Bites,Havelsan,EHSIM,MIA Teknoloji,TEI,Turksat,Minist Natl Def Turkey,Turkish AF,Turkish Natl Def Univ,Turkish AF Acaden_US
dc.identifier.doi10.1109/RAST57548.2023.10198016
dc.identifier.isbn979-8-3503-2302-3
dc.identifier.scopus2-s2.0-85168418108en_US
dc.identifier.urihttps://doi.org/10.1109/RAST57548.2023.10198016
dc.identifier.urihttps://hdl.handle.net/20.500.12452/13739
dc.identifier.wosWOS:001055074600179en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherIEEEen_US
dc.relation.ispartof2023 10th International Conference On Recent Advances In Air And Space Technologies, Rasten_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_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.titleVirtual Investigation on the Response of Glare to Low Velocity Impacten_US
dc.typeConference Objecten_US

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