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Journals / Iğdır Üniversitesi Fen Bilimleri Enstitüsü Dergisi / 2020 / Cilt: 10 - Sayı: 1

Non-linear analysis of composite parts jointed with embedded adhesive under tensile load

İsmail Yasin SÜLÜ
Pages
465–476
Publication Date
2020-03-01
DOI
—
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AI Summary & Key Takeaways

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

Furthermore, it is stated that embedded adhesive connection is important for industrial applications.

📌 3 Key Takeaways

🎯
Objective & Hypothesis:In this study, the composite parts subjected to tensile load were combined with a double-acting adhesive connection and analyzed using the 3D finite element method (FEM).
📊
Key Findings & Data:In the analysis, carbon / epoxy (AS4 / 3501-6) composite parts with different orientation angles were used and DP410 was used as adhesive.
💡
Conclusion & Impact:Furthermore, it is stated that embedded adhesive connection is important for industrial applications.
🔬Design:Modeling & Simulation
📍Scope:Comprehensive Sample
⚙️Variables:Non-linear analysis · finite element method (FEM) · joint design

Abstract

In this study, the composite parts subjected to tensile load were combined with a double-acting adhesive connection and analyzed using the 3D finite element method (FEM). The joint design is important to ensure that the joint is durable, does not take up too much space and has a long service life. In the analysis, carbon / epoxy (AS4 / 3501-6) composite parts with different orientation angles were used and DP410 was used as adhesive. Models for numerical analysis were created using ANSYS 14.5 package program. Finite element analyzes were performed to determine the damage loads. In general, because the damages occur in the adhesive region, the stresses in all directions on the adhesive, shear stresses, von-Mises stress and peel stresses were obtained at the specified failure loads. As a result, the effects of orientation angles, overlap dimensions of the bonded area and adhesive layer were investigated. The most effective parameters were determined for the composite parts joined with embedded double-acting adhesive. Furthermore, it is stated that embedded adhesive connection is important for industrial applications.

Özet

In this study, the composite parts subjected to tensile load were combined with a double-acting adhesive connection and analyzed using the 3D finite element method (FEM). The joint design is important to ensure that the joint is durable, does not take up too much space and has a long service life. In the analysis, carbon / epoxy (AS4 / 3501-6) composite parts with different orientation angles were used and DP410 was used as adhesive. Models for numerical analysis were created using ANSYS 14.5 package program. Finite element analyzes were performed to determine the damage loads. In general, because the damages occur in the adhesive region, the stresses in all directions on the adhesive, shear stresses, von-Mises stress and peel stresses were obtained at the specified failure loads. As a result, the effects of orientation angles, overlap dimensions of the bonded area and adhesive layer were investigated. The most effective parameters were determined for the composite parts joined with embedded double-acting adhesive. Furthermore, it is stated that embedded adhesive connection is important for industrial applications.

🔖

Cite This Article

SÜLÜ, İ. Y. (2020). Non-linear analysis of composite parts jointed with embedded adhesive under tensile load. Iğdır Üniversitesi Fen Bilimleri Enstitüsü Dergisi, Cilt: 10 - Sayı: 1, 465–476. https://ajindex.com/articles/256998

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References (13)

  1. Abdi H, Papadopoulos J, Nayeb-Hashemi H, Vaziri A, 2017. Enhanced elastic-foundation analysis of balanced single lap adhesive joints. International Journal of Adhesion & Adhesives, 72: 80–91.
  2. Stein N, Mardani H, Becker W, 2016. An efficient analysis model for functionally graded adhesive single lap joints. International Journal of Adhesion & Adhesives, 70: 117–125.
  3. Guin W E, Wang J, 2016. Theoretical model of adhesively bonded single lap joints with functionally graded adherents. Engineering Structures, 124: 316–332.
  4. Ribeiro T E A, Campilho R D S G, da Silva L FM, Goglio L, 2016. Damage analysis of composite–aluminium adhesively-bonded single-lap joints. Composite Structures, 136: 25–33.
  5. Sülü İsmail Yasin, Şahinaslan Apdulmutalip, 2016. Experimental failure testing and repair of internal pressurized composite pipes using different fracture models. Materials Testing, 58- 9: 788-793. Sülü İsmail Yasin, 2017. Mechanical behavior of internal pressurized composite pipes jointed with embedded tubular sleeves. Materials Testing,59-3: 272-277.
  6. Tang J H, Sridhar I, Srikanth N, 2013. Static and fatigue failure analysis of adhesively bonded thick composite single lap joints. Composites Science and Technology, 86: 18–25.
  7. Kim K S, Yi Y M, Cho G R, Kim C G, 2008. Failure prediction and strength improvement of uni-directional composite single lap bonded joints. Composite Structures, 82: 513–520.
  8. Katnam K B, Comer A J, Stanley W F, Buggy M, Ellingboe A R, Young T M, 2011.Characterisingprepreg and non-crimp-fabric composite single lap bonded joints. International Journal of Adhesion & Adhesives, 31: 679–686.
  9. Khalili S M R, Jafarkarimi M H, Abdollahi M A, 2009. Creep analysis of fibre reinforced adhesives in single lap joints—Experimental study. International Journal of Adhesion & Adhesives, 29: 656–661.
  10. Ariaee S, Tutunchi A, Kianvash A, Entezami A A, 2014. Modeling and optimization of mechanical behavior of bonded composite–steel single lap joints by response surface methodology. International Journal of Adhesion & Adhesives, 54: 30–39.
  11. Reis P N B, Antunes F J V, Ferreira J A M, 2005. Influence of superposition length on mechanical resistance of single-lap adhesive joints. Composite Structures, 67: 125–133.
  12. Fawzia Sabrina, Al-Mahaidi Riadh, Zhao Xiao-Ling, 2006. Experimental and finite element analysis of a double strap joint between steel plates and normal modulus CFRP. Composite Structures, 75: 156–162.
  13. Fawzia Sabrina, Zhao Xiao-Ling, Al-Mahaidi Riadh, 2010. Bond–slip mod