ContactISSN:e-ISSN: 2980-0064
Author Sign-inReviewer Sign-inRegister
TürkçeEnglish
HomeAim and ScopeABOUTGUIDE FOR AUTHORSSend ArticleLatest IssueArchiveContact Us

Low Velocity Impact Behavior of Al Wire Reinforced Layered Composite

Mehmet Cihad ŞAHİN,Hakan Burak KARADAĞ,Mesut UYANER

  • Mehmet Cihad ŞAHİN: Necmettin Erbakan Üniversitesi Fen Bilimleri Enstitüsü
  • Hakan Burak KARADAĞ: NECMETTİN ERBAKAN ÜNİVERSİTESİ Mühendislik Fakültesi
  • Mesut UYANER: Necmettin Erbakan Üniversitesi Havacılık ve Uzay Bilimleri Fakültesi
  •  Year : 2024
  •  Vol : 3
  •  Issue : 1
  •  Page : 1-14
Traditional materials are being replaced by advanced technology materials. Especially in the defense industry, aerospace and aviation, armored vehicles and automobile sector, especially in the military field, researches to increase ballistic and impact resistance and the detection of damage to the material and the optimization of new designs are focused on. Composite materials are also used in secondary structural parts of the aircraft, which are considered to be able to continue their flight partially in case of damage. A comprehensive study of the deformations that occur in the material as a result of impact is important as a contribution to the literature and as a reference for aviation maintenance personnel. In high-tech sectors, especially in the aerospace industry, composite materials with aluminum layers are preferred for payload weight compared to conventional materials. Aluminum-containing composites and aluminum-containing materials, due to their high strength to weight ratio, are vital in many sectors where payload weight is important, especially in the aerospace industry. Rubber-blend PU polymer was cured in a customized mold together with 1050 Al sheets to create the layered composite. The polymer layer was strengthened using different rows of Al wire screen. A novel approach to fabricate a reinforced composite panel in one spot was introduced. A specifically made drop weight apparatus was used to conduct a low velocity impact test. Drop weight tests were carried out at five distinct energy levels (40J, 60J, 80J, 100J and 120J) to examine the impact behavior of the specimens. Force-time histories were saved for each event. The "energy-time" and "force-displacement" variations were also obtained by kinematic analysis performed in accordance with ASTM D7136/D7136M-12 standard. No puncture occurred in any specimen. Since the specimens were layered, penetration was observed only in the top layer. In addition, the peak forces, the absorbed energy and the impact tip’s indentation are also presented. Damage to the layered composite structures after impact was investigated. No significant effect of Al sieve reinforcement in the polymer layer was observed on the low velocity impact response, except for the tests at 120 J.
Cite this Article As : Karadağ, H. B., Şahin, M. C., & Uyaner, M. (2024). Al tel takviyeli tabakalı kompozitin düşük hızlı darbe davranışı. Aerospace Research Letters (ASREL), 3(1), 1-14. https://doi.org/10.56753/ASREL.2024.3.4

Conflict of interest : The authors declare that they have no conflict of interest.

This article is published under the CC BY-NC 4.0 license.
Asrel Aerospace Research Letters
2024, Vol3, Issue1
E-ISSN: 2980-0064
Received : , Accepted : , Published Online :

References

  1. Alcock, B., Cabrera, N., Barkoula, N., & Peijs, T. (2006). Low velocity impact performance of recyclable all-polypropylene composites. Composites Science and Technology, 66(11-12), 1724-1737. https://doi.org/10.1016/j.compscitech.2005.11.010
  2. Al-Rubaye, M. M. J. (2018). Low Velocity Impact Behavior of Glass Fiber and Carbon Fiber Reinforced Composites [MSc.]. Erciyes Üniversitesi, Fen Bilimleri Enstitüsü.
  3. Bieniaś, J., & Jakubczak, P. (2012). Low velocity impact resistance of aluminium/carbon-epoxy fiber metal laminates. Composites Theory and Practice, 12(3), 193-197.
  4. Çetin, Ş., & Karadağ, H. B. (2023). Tabakalı kompozitlerin darbe direncinin incelenmesi. Aerospace Research Letters (ASREL) Dergisi, 2(2), 114-127. https://doi.org/10.56753/ASREL.2023.2.5
  5. Dağ, T., Yıldırım, N., Kepir, Y., & Uyaner, M. (2022). E/cam epoksi laminelerin üzerine uygulanan düşük hızlı darbe davranışının sayısal simülasyonu. Aerospace Research Letters (ASREL) Dergisi, 1(1), 1-10. https://doi.org/10.56753/ASREL.2022.1.1
  6. Dağ, T., Yıldırım, N., Şentürk, G., Durmazoğlu, M., Yıldırım, S., & Uyaner, M. (2023). Virtual investigation on the response of Glare to low velocity impact. 2023 10th International Conference on Recent Advances in Air and Space Technologies (RAST), 1-5. https://doi.org/10.1109/RAST57548.2023.10198016
  7. Hussin, R., Ismail, N., & Mustapa, S. (2016). A study of foreign object damage (FOD) and prevention method at the airport and aircraft maintenance area. IOP Conference Series: Materials Science and Engineering, 152(1). https://doi.org/10.1088/1757-899X/152/1/012038
  8. Koçhan, C. (2019). Low velocity impact behaviour of recycled mussel shell particles reinforced epoxy composites. Materials Research Express, 6(8), 85105. https://doi.org/10.1088/2053-1591/ab21ff
  9. Kumar Dhananjayan, V. (2013). Design and Analysis of a Compression Molded Carbon Composite Wheel Center [Yüksek Lisans]. The University of Texas at Arlington, Faculty of the Graduate School.
  10. Masniza, Y., Zulfabli, H. M., Amarul, T., Khairunnisa, S. N., Zilawati, N. A. R. N. N., Nazera, D., & Ismalina, H. N. (2019). Potential FOD defects on the composite material. AIP Conference Proceedings: 5th International Conference on Green Design and Manufacture (IConGDM 2019), 2129(July). https://doi.org/10.1063/1.5118064
  11. Moriniere, F. D. (2014). Low-velocity impact on fibre-metal laminates (C. 2, Sayı 2012). https://doi.org/doi.org/10.4233/uuid:022e1a88-f48e-493e-805e-014f396a05dc
  12. Uyaner, M. (2021). Test to graph. Mendeley Data, Elsevier Ltd. https://doi.org/10.17632/gydhpktxjk.2
  13. Vaidya, U. K. (2011). Impact Response of Laminated and Sandwich Composites. Içinde S. Abrate (Ed.), Impact Engineering of Composite Structures (ss. 97-191). Springer Vienna. https://doi.org/10.1007/978-3-7091-0523-8_4