Please use this identifier to cite or link to this item:
https://hdl.handle.net/20.500.11851/10408
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Cihan Tezel, Muhammed | - |
dc.contributor.author | Yamaner, Yusuf | - |
dc.contributor.author | Aziz Çoğuz, Bilge | - |
dc.contributor.author | Acar, Erdem | - |
dc.date.accessioned | 2023-04-16T10:02:16Z | - |
dc.date.available | 2023-04-16T10:02:16Z | - |
dc.date.issued | 2023 | - |
dc.identifier.issn | 0021-8669 | - |
dc.identifier.uri | https://doi.org/10.2514/1.C036753 | - |
dc.identifier.uri | https://hdl.handle.net/20.500.11851/10408 | - |
dc.description.abstract | This study investigates the effects of bird strike on the wing leading edge of a trainer aircraft in accordance with the European Aviation Safety Agency’s CS-23 standards (“Normal, Utility, Aerobatic and Commuter Aeroplanes,” Certification Specifications, Part 23, Occupant Physical Environment), and it compares various options for the design of energy-absorbing support structures. In this study, the bird model with hemispherical-ended cylindrical geometry is simulated using the smoothed particle hydrodynamics finite element approach. After validating the impact of the bird model on a rigid plate, a bird strike on the wing leading edge is modeled; and the results are compared with the existing experimental and simulation data available in the literature. Finally, different design options for the support structure configurations of the wing leading edge (including traditional rib design, honeycomb sandwich, triangular reinforcement, and negative Poisson ratio structures) are evaluated, and the results are compared. It is found that a honeycomb sandwich panel support structure provides the best collision and weight performance. © 2023, AIAA International. All rights reserved. | en_US |
dc.description.sponsorship | 2020/2021; Türkiye Bilimsel ve Teknolojik Araştırma Kurumu, TÜBİTAK: 20AG001, 20AG027 | en_US |
dc.description.sponsorship | This study was supported by the Scientific and Technological Research Council of Turkey (TUBITAK) project no. 20AG027 under program no. 20AG001, the TUBITAK Bilim İnsanı Destek Program-ları Başkanlığı (BIDEB) 2209-B Undergraduate Research Project Support Program for Industry 2020/1, and the Turkish Aerospace Industry under the Lift-Up Program 2020/2021. | en_US |
dc.language.iso | en | en_US |
dc.publisher | AIAA International | en_US |
dc.relation.ispartof | Journal of Aircraft | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.subject | Aircraft accidents | en_US |
dc.subject | Cylinders (shapes) | en_US |
dc.subject | Honeycomb structures | en_US |
dc.subject | Hydrodynamics | en_US |
dc.subject | Structural design | en_US |
dc.subject | Wings | en_US |
dc.subject | Bird strike | en_US |
dc.subject | Cylindrical geometry | en_US |
dc.subject | Design option | en_US |
dc.subject | Energy absorbing supports | en_US |
dc.subject | European Aviation Safety Agency | en_US |
dc.subject | Physical environments | en_US |
dc.subject | Smoothed particle hydrodynamics | en_US |
dc.subject | Support structures | en_US |
dc.subject | Trainer aircrafts | en_US |
dc.subject | Wing leading edges | en_US |
dc.subject | Birds | en_US |
dc.title | Exploring Design Options for Wing Leading Edge Against Bird Strike | en_US |
dc.type | Article | en_US |
dc.department | TOBB ETÜ | en_US |
dc.identifier.volume | 60 | en_US |
dc.identifier.issue | 1 | en_US |
dc.identifier.startpage | 66 | en_US |
dc.identifier.endpage | 80 | en_US |
dc.identifier.wos | WOS:000834263200001 | en_US |
dc.identifier.scopus | 2-s2.0-85150387580 | en_US |
dc.institutionauthor | … | - |
dc.identifier.doi | 10.2514/1.C036753 | - |
dc.authorscopusid | 58147739500 | - |
dc.authorscopusid | 57354674000 | - |
dc.authorscopusid | 58147604900 | - |
dc.authorscopusid | 55308448100 | - |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı | en_US |
dc.identifier.scopusquality | Q1 | - |
item.openairetype | Article | - |
item.languageiso639-1 | en | - |
item.grantfulltext | none | - |
item.fulltext | No Fulltext | - |
item.openairecristype | http://purl.org/coar/resource_type/c_18cf | - |
item.cerifentitytype | Publications | - |
crisitem.author.dept | 02.7. 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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