Please use this identifier to cite or link to this item:
https://hdl.handle.net/20.500.11851/11261
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Tezel, Muhammet Cihan | - |
dc.contributor.author | Yamaner, Yusuf | - |
dc.contributor.author | Acar, Erdem | - |
dc.contributor.author | Çoğuz, Bilge Aziz | - |
dc.date.accessioned | 2024-04-06T08:09:49Z | - |
dc.date.available | 2024-04-06T08:09:49Z | - |
dc.date.issued | 2021 | - |
dc.identifier.isbn | 9786057171900 | - |
dc.identifier.uri | http://aiac.ae.metu.edu.tr/2021/program/papers.html | - |
dc.identifier.uri | https://hdl.handle.net/20.500.11851/11261 | - |
dc.description.abstract | This study investigates the effects of bird strike to the wing leading edge of a trainer aircraft in accordance with the EASA CS-23 standards, and compares various options for design of energy absorbing support structures. In this study, bird models with hemispherical-ended cylindrical geometry are simulated using the Smooth Particle Hydrodynamics (SPH) finite element approach. After validating the impact of the bird model with a rigid plate, the bird strike on the wing leading edge is modelled, and the results are compared with the existing experimental and simulation data available in literature. Finally, different design options for support structures of the wing leading edge are evaluated and the results are compared. It is found that honeycomb sandwich panel support structure displays the best collusion and weight performance. | en_US |
dc.language.iso | en | en_US |
dc.publisher | METU Aerospace Engineering | en_US |
dc.relation.ispartof | 11th Ankara International Aerospace Conference AIAC-2021-153 8-10 September 2021 - METU, Ankara Turkey | en_US |
dc.rights | info:eu-repo/semantics/openAccess | en_US |
dc.subject | Bird strike analysis | en_US |
dc.subject | Wing leading edge | en_US |
dc.subject | Smooth Particle Hydrodynamics (SPH) method | en_US |
dc.subject | Honeycomb | en_US |
dc.subject | Triangular reinforcement structures | en_US |
dc.title | Evaluation of Various Design Options for Wing Leading Edge Against Bird Strike | en_US |
dc.type | Conference Object | en_US |
dc.department | TOBB ETU Mechanical Engineering | en_US |
dc.identifier.startpage | 1 | en_US |
dc.identifier.endpage | 22 | en_US |
dc.authorid | 0000-0003-4734-2625 | - |
dc.institutionauthor | Acar, Erdem | - |
dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US |
item.openairetype | Conference Object | - |
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: | Makine Mühendisliği Bölümü / Department of Mechanical Engineering |
CORE Recommender
Items in GCRIS Repository are protected by copyright, with all rights reserved, unless otherwise indicated.