Burhan CETINKAYA

Mr. Burhan CETINKAYA

orcid

Research Focus & Metrics

Academic Career Length

8Years (2019-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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27 December 2019 in Mühendis ve Makina
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Journal Article
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Orhan GülcanOrhan Gülcan
Orhan Gülcan
KTKazım TEKKANAT
Kazım TEKKANAT
BCBurhan CETINKAYA
Burhan CETINKAYA
In todays competitive aerospace environment, it is very important to design and produce aircrafts with high performance and lightweights and in this context, to find new production processes and new production materials. Forth is reason, Fiber metal laminates (FML) developed by Delft University, are special composite materials that can be used as an alternative to the conventional aluminium materials used in aircrafts for their high fatigue resistance. The aim of this study is to provide a broad literature review about the history of FML, their usage areas, variants and properties (static, fatigue, impact, corrosion and thermal resistance) and to suggest research areas in the future.

Verified
Journal Article
Open access
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BCBurhan CETINKAYA
Burhan CETINKAYA
EYErdem YILMAZ
Erdem YILMAZ
IOIbrahim OZKOL
Ibrahim OZKOL
İŞİlhan Şen
İlhan Şen
Tamer - SARAÇYAKUPOĞLUTamer - SARAÇYAKUPOĞLU
Tamer - SARAÇYAKUPOĞLU
In today’s aviation industry, research and studies are carried out to manufacture and design lightweight, high-performance materials. One of the materials developed in line with this goal is glass laminate aluminum-reinforced epoxy (GLARE), which consists of thin aluminum sheets and S2-glass/epoxy layers. Because of its high impact resistance and excellent fatigue and damage tolerance properties, GLARE is used in different aircraft parts, such as the wing, fuselage, empennage skins, and cargo floors. In this study, a survey was carried out and a low-velocity impact model for GLARE materials was developed using the ABAQUS (2014) version V6.14 software and compared with the results of low-velocity impact tests performed according to the American Society for Testing and Materials (ASTM) D7136 standard. This article introduces a novel integrated approach that combines detailed numerical modeling with experimental validation of GLARE 4A FMLs under low-velocity impact. Leveraging ABAQUS, a robust FEM featuring explicit analysis, cohesive resin interfaces, and custom VUMAT subroutines was developed to accurately simulate energy absorption, dent depth, and delamination. The precise model’s predictions align well with test results performed according to ASTM D7136 standards, exhibiting less than a 0.1% deviation in the displacement (dent depth)–time response, along with deviations of 4.3% in impact energy–time and 5.2% in velocity–time trends at 5.5 ms.