Investigation of Impact Resistance of Laminated Composites

Hakan Burak KARADAĞ, Şerafettin ÇETİN

  •  Year : 2023
  •  Vol : 2
  •  No : 2
  •  Page : 114-127
In this study, a sandwich panel that can be used as an internal structural material in aircraft and other transportation vehicles has been produced. The core of this sandwich panel was obtained by baking neat EVA sheets without reinforcement and with three rows of steel wire reinforcement at 180 ˚C for 30 minutes. On the upper and lower surfaces of these cores, 0.5 mm thick 5457 aluminum sheets were adhered with polyurethane adhesive and thus composite panels were obtained. The sandwich panels were subjected to impact tests at various levels (20J, 30J, 40J and 50J). After the tests, force-time and force-displacement graphs of the specimens corresponding to different energy values were obtained. It was observed that as the wire reinforcement increases, the elasticity of the material decreases and the strength of the material increases, and accordingly, the maximum displacement generally decreases.
Cite this Article As : Çetin, Ş, & Karadağ, H. B. (2023). Tabakalı kompozitlerin darbe direncinin incelenmesi. Aerospace Research Letters (ASREL) Dergisi, 2(2), 114-127. http://dx.doi.org/10.56753/ASREL.2023.2.5

Description : Yazarların hiçbiri, bu makalede bahsedilen herhangi bir ürün, aygıt veya ilaç ile ilgili maddi çıkar ilişkisine sahip değildir. Araştırma, herhangi bir dış organizasyon tarafından desteklenmedi.Yazarlar çalışmanın birincil verilerine tam erişim izni vermek ve derginin talep ettiği takdirde verileri incelemesine izin vermeyi kabul etmektedirler. None of the authors, any product mentioned in this article, does not have a material interest in the device or drug. Research, not supported by any external organization. grant full access to the primary data and, if requested by the magazine they agree to allow the examination of data.
Investigation of Impact Resistance of Laminated Composites, Araştırma Makalesi,
, Vol. 2 (2)
Received : 23.11.2023, Accepted : 24.12.2023 , Published Online : 31.12.2023
Asrel Aerospace Research Letters
ISSN: ;
E-ISSN: 2980-0064 ;
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