Comparison of bushing applications in composite structures in aerospace industry
Is this your thesis?
This record came from a bulk archive import. If it’s yours, link it to your profile.
Abstract (EN)
In this study, four different bushing applications on carbon-epoxy prepreg laminated composite plate are investigated experimentally and theoretically.The composite specimens having bushing application is loaded perpendicular to its plane and the strength of the assembly in this direction is investigated. These applications are compared by using the results of the experiments. Bushing application methodology is determined for the most durable assembly.The generated finite element model makes contribution to the design by the help of finite element analysis.While MSC/PATRAN is used for the finite element model generation, MSC/NASTRAN is used for the finite element analysis.
Author
Gazi Serten Bakır
How to Cite
Gazi Serten Bakır (Master Thesis). Comparison of bushing applications in composite structures in aerospace industry, 2012, Gazi University.
Keywords
License
Tüm Hakları Saklıdır
This work is shared under the specified license terms.
More theses from Gazi University
- Occupational accident analysis and modelling in oil and gas drilling sector Turkey(2021)
- XVI. yüzyıl Anadolu'sunda Oğuzların Karkın Boyu(2004)
- Experimental development of the interfacial bond-slip model between textile reinforced mortar strips and masonry walls(2025)
- Sharing of real life geometry samples via a social learning environment: A case study(2021)
- Evaluatıon of calcium hydroxide removal efficiency of two different irrigation activation techniques from artificial internal resorption cavities prepared at different root levels(2021)
- The use of verbal memory in the context of sustainability and power at the museums of Turk(2010)