Journals / European Mechanical Science / 2021 / Cilt: 5 - Sayı: 4

Numerical Investigation of Fatigue Behavior of Non-patched and Patched Aluminum/Composite Plates

Pages
168–176
Publication Date
2022-10-12
DOI
—
🏛️Bibliographic metadata and full text access for this article are provided via DergiPark.
DergiPark Record ↗
✨

AI Summary & Key Takeaways

AI Insight
⚡ TL;DR(Too Long; Didn't Read)

Thus, the study revealed that the composite patch's contribution is very important.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:In this study, the fatigue behavior of composite patched and non-patched Al 5083 aluminum plates was numerically investigated.
📊
Key Findings & Data:Al 5083 Aluminum plates with semi-circular notched (2, 3 and 4 mm long cracked) and "V" notched (30°, 45° and 60° angled) were used in the analyzes.
💡
Conclusion & Impact:Thus, the study revealed that the composite patch's contribution is very important.
🔬Design:Research Article
📍Scope:Comprehensive Sample
⚙️Variables:Aluminum · Composite · Patch

Abstract

In this study, the fatigue behavior of composite patched and non-patched Al 5083 aluminum plates was numerically investigated. Al 5083 Aluminum plates with semi-circular notched (2, 3 and 4 mm long cracked) and "V" notched (30°, 45° and 60° angled) were used in the analyzes. Mechanical properties of Al 5083 Aluminum plate, DP460 type adhesive of produced by 3M and [0°]8 glass fiber reinforced composite patch material was used for the study. The Finite Element Method was applied for numerical study. Numerical analyzes were performed with the Ansys version 15.0 Workbench Package program. As a result of the numerical study, the highest fatigue life (1593.2 N) is seen on the 30° angled "V" notched and patched specimen. However, the fatigue life in non-patched specimen (30° angled "V" notched) was found to be 277.69 N. Thus, the study revealed that the composite patch's contribution is very important.

🔖

Cite This Article

ADİN, H., ADİN, M. Ş., SAĞLAM, Z. (2022). Numerical Investigation of Fatigue Behavior of Non-patched and Patched Aluminum/Composite Plates. European Mechanical Science, Cilt: 5 - Sayı: 4, 168–176. https://ajindex.com/articles/512393

📄 Full Text PDF Viewer

📄

PDF görüntüleyici hazırlanıyor...

References (13)

  1. Carbas, R., Marques, E., da Silva, L., (2021). The influence of epoxy adhesive toughness on the strength of hybrid laminate adhesive joints. Applied Adhesion Science, vol. 9, no. 1, pp. 1-14
  2. Deghoul, N., Errouane, H., Sereir, Z., Chateauneuf, A., Amziane, S., (2019). Effect of temperature on the probability and cost analysis of mixed-mode fatigue crack propagation in patched aluminium plate. International Journal of Adhesion and Adhesives, vol. 94, pp. 53-63
  3. Ergün, R.K., Adin, H., Şişman, A., Temiz, Ş., (2018). Repair of an aluminum plate with an elliptical hole using a composite patch. Materials Testing, vol. 60, no. 11, pp. 1104-1110
  4. Wu, C., Gunnion, A.J., Chen, B., Yan, W., (2015). Fatigue damage tolerance of two tapered composite patch configurations. Composite Structures, vol. 134, pp. 654-662
  5. Gong, X.-J., Cheng, P., Aivazzadeh, S., Xiao, X., (2015). Design and optimization of bonded patch repairs of laminated composite structures. Composite Structures, vol. 123, pp. 292-300
  6. Jian-Bin, H., Xu-Dong, L., Zhi-Tao, M., (2015). Fatigue behavior of thick center cracked aluminum plates repaired by two-sided composite patching. Materials & Design, vol. 88, pp. 331-335
  7. Saraç, İ., Adin, H., Temiz, Ş., (2018). Experimental determination of the static and fatigue strength of the adhesive joints bonded by epoxy adhesive including different particles. Composites Part B: Engineering, vol. 155, pp. 92-103
  8. Chung, K.-H., Yang, W.-H., (2003). A study on the fatigue crack growth behavior of thick aluminum panels repaired with a composite patch. Composite Structures, vol. 60, no. 1, pp. 1-7
  9. Maligno, A., Soutis, C., Silberschmidt, V., (2013). An advanced numerical tool to study fatigue crack propagation in aluminium plates repaired with a composite patch. Engineering Fracture Mechanics, vol. 99, pp. 62-78
  10. Fekirini, H., Bouiadjra, B.B., Belhouari, M., Boutabout, B., Serier, B., (2008). Numerical analysis of the performances of bonded composite repair with two adhesive bands in aircraft structures. Composite structures, vol. 82, no. 1, pp. 84-89
  11. Adin, M.Ş., Kılıçkap, E., (2021). Strength of double-reinforced adhesive joints. Materials Testing, vol. 63, no. 2, pp. 176-181
  12. Canbolat, C., (2018). Repairement of Al 2024 T3 plates by means of fiberglass composite patches, Master thesis, Kahramanmaras Sutcu Imam University, Turkey
  13. Saylık, A., (2016). The stress analysis of aluminum plates repaired with composite pat