dc.contributor.author | Dağ, Tolunay | |
dc.contributor.author | Yıldırım, Nur | |
dc.contributor.author | Şentürk, Gökhan | |
dc.contributor.author | Durmazoğlu, Metin | |
dc.contributor.author | Yıldırım, Serap | |
dc.contributor.author | Uyaner, Mesut | |
dc.date.accessioned | 2023-12-11T13:05:04Z | |
dc.date.available | 2023-12-11T13:05:04Z | |
dc.date.issued | 2023 | en_US |
dc.identifier.citation | Dag, 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.isbn | 979-835032302-3 | |
dc.identifier.uri | https://hdl.handle.net/20.500.12508/2625 | |
dc.description.abstract | Due 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.iso | eng | en_US |
dc.publisher | Institute of Electrical and Electronics Engineers Inc. | en_US |
dc.relation.isversionof | 10.1109/RAST57548.2023.10198016 | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | Composite | en_US |
dc.subject | Fiber metal laminates | en_US |
dc.subject | Glare | en_US |
dc.subject | Low velocity impact | en_US |
dc.subject | ls-dyna | en_US |
dc.subject.classification | Metal Fibers | |
dc.subject.classification | Laminates | |
dc.subject.classification | Aluminum | |
dc.subject.classification | Engineering & Materials Science - Mechanics - Delamination | |
dc.subject.other | Computer software | |
dc.subject.other | Laminated composites | |
dc.subject.other | Virtual reality | |
dc.subject.other | 2024-T3 aluminium | |
dc.subject.other | 2024-T3 aluminum | |
dc.subject.other | Fibre metal laminates | |
dc.subject.other | Glass epoxy | |
dc.subject.other | Impact simulation | |
dc.subject.other | Impactors | |
dc.subject.other | Increasing costs | |
dc.subject.other | Low velocity impact | |
dc.subject.other | LS-DYNA | |
dc.subject.other | Virtual tests | |
dc.title | Virtual Investigation on the Response of Glare to Low Velocity Impact | en_US |
dc.type | conferenceObject | en_US |
dc.relation.journal | Proceedings of 10th International Conference on Recent Advances in Air and Space Technologies, RAST 2023 | en_US |
dc.contributor.department | Havacılık ve Uzay Bilimleri Fakültesi -- Havacılık ve Uzay Mühendisliği Bölümü | en_US |
dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US |
dc.contributor.isteauthor | Dağ, Tolunay | |
dc.relation.index | Web of Science - Scopus | en_US |
dc.relation.index | Web of Science Core Collection - Conference Proceedings Citation Index – Science | |