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Structural Analysis of Glass Fiber / Epoxy and Basalt Fiber / Epoxy Lap Joint Specimens Using FEA

Received: 7 June 2017     Accepted: 30 June 2017     Published: 1 August 2017
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Abstract

The aim of this work is to predict the crack initiation and failure based on the Von Mises stress distributions at the edge of the overlap region. Finite Element Analysis (FEA) software is used to investigate the stress distribution under tensile loading on composite lap joints. From the Von Mises stresses results, the bonded joint and hybrid joint of basalt-fiber reinforced plastic (BFRP) specimen’s produces higher results than bonded joint and hybrid joint of glass-fiber reinforced plastic (GFRP) specimens due to higher interfacial bonding strength. A well-designed bonded joint of BFRP laminates is very efficient for composite lap joint structures compared to hybrid (boned/riveted) joints. It is suggested that the application of basalt/epoxy laminate as a strengthening material is useful for joining of composite structural members in the engineering fields.

Published in Colloid and Surface Science (Volume 2, Issue 3)
DOI 10.11648/j.css.20170203.14
Page(s) 114-117
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2017. Published by Science Publishing Group

Keywords

Composite Lap Joints, FEA Ansys, Stress Distribution, Displacement

References
[1] Mokhtari, M, Madani, K, Belhouari, M, Touzain, S, Feaugas, X, Ratwani, M, ‘Effects of composite adherend properties on stresses in double lap bonded joints’, Journal of Materials and Design, 2013, vol. 44, pp. 633-639.
[2] Banea, MD, Da Silva, LFM, ‘Adhesively bonded joints in composite materials: An overview’, Journal of Materials, Design and Applications, 2009, vol. 223, pp. 91-102.
[3] Camanho, PP, Matthews, ‘Stress analysis and strength prediction of mechanically fastened joints in FRP. A review’, Composites Part A, 1997, vol. 28, pp. 529-547.
[4] Chan, WS, V edhagiri, S, ‘Analysis of composite bonded/bolted joints used in repairing’, Journal of Composite Materials, 2001, vol. 35, pp. 1045-1061.
[5] Chang, DJ, Muki, R, ‘Stress distribution in a lap joint under tension – shear’, International Journal of Solids Structures, 1974, vol. 10, pp. 503-517.
[6] Mohamed Bak, K, Kalai Chelvan, K, ‘Parametric study of bonded, riveted and hybrid joints using FEA’, Journal of Applied Sciences, 2012, vol. 12, pp. 1058.
[7] Hart-Smith, LJ, ‘Bonded-bolted composite joints’, Journal of Aircraft, 1985, vol. 22, pp. 993-1000.
[8] Kelly, G, ‘Load Transfer in hybrid (bonded/bolted) composite single lap joints’, Composite Structures, 2005, vol. 69, pp. 35-43.
[9] Kim, KS, Yoo, JS, Kim, CG, Yi, YM, ‘Failure mode and strength of uni-directional composite single lap bonded joints with different bonding methods’, Journal of Composite Structures, 2006, vol. 72, pp. 477– 485.
[10] Jancar, J, ‘Effect of interfacial shear strength on the mechanical response of polycarbonate and PP reinforced with basalt fibres’, Journal of Composite Interface, 2006, vol. 13, pp. 853–864.
[11] Liu, Q, Shaw, TM, Parnas, RS, ‘Investigation of basalt fiber composite mechanical properties for applications in transportation’, Journal of Polymer Composites, 2006, vol. 10, pp. 41-48.
[12] Lopresto, V, Leone, C, De Iorio, I, ‘Mechanical characterization of basalt fiber reinforced plastics’, Composites: Part B, 2011, vol. 42, pp. 717–723.
[13] Mohamed Bak, K, Kalai Chelvan, K, Arumugam, V, ‘A Novel approach for classification of failure modes on single lap joints using acoustic emission data’, Journal of Composite Materials, 2014, vol. 48, pp. 3003-3017.
[14] Mohamed Bak. K, Kalai Chelvan. K “Acoustic emission characterization of failure modes of bonded, riveted, and hybrid single lap joints in GFRP laminate” Journal of Composite materials, 2016, vol. 50 pp. 3-23.
[15] Mohamed Bak. K, Kalai Chelvan. K, Vijaya Raghavan G. K, Arumugam V “Study on effect of adhesive thickness of single lap joints in composite laminate using AE and FEA” BINDT-an International journal, Insight - Non-Destructive Testing and Condition Monitoring, Volume 55, 2013, pp. 35-41.
Cite This Article
  • APA Style

    Mohamed Bak Kamaludeen, Kalaichelvan Kani. (2017). Structural Analysis of Glass Fiber / Epoxy and Basalt Fiber / Epoxy Lap Joint Specimens Using FEA. Colloid and Surface Science, 2(3), 114-117. https://doi.org/10.11648/j.css.20170203.14

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    ACS Style

    Mohamed Bak Kamaludeen; Kalaichelvan Kani. Structural Analysis of Glass Fiber / Epoxy and Basalt Fiber / Epoxy Lap Joint Specimens Using FEA. Colloid Surf. Sci. 2017, 2(3), 114-117. doi: 10.11648/j.css.20170203.14

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    AMA Style

    Mohamed Bak Kamaludeen, Kalaichelvan Kani. Structural Analysis of Glass Fiber / Epoxy and Basalt Fiber / Epoxy Lap Joint Specimens Using FEA. Colloid Surf Sci. 2017;2(3):114-117. doi: 10.11648/j.css.20170203.14

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  • @article{10.11648/j.css.20170203.14,
      author = {Mohamed Bak Kamaludeen and Kalaichelvan Kani},
      title = {Structural Analysis of Glass Fiber / Epoxy and Basalt Fiber / Epoxy Lap Joint Specimens Using FEA},
      journal = {Colloid and Surface Science},
      volume = {2},
      number = {3},
      pages = {114-117},
      doi = {10.11648/j.css.20170203.14},
      url = {https://doi.org/10.11648/j.css.20170203.14},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.css.20170203.14},
      abstract = {The aim of this work is to predict the crack initiation and failure based on the Von Mises stress distributions at the edge of the overlap region. Finite Element Analysis (FEA) software is used to investigate the stress distribution under tensile loading on composite lap joints. From the Von Mises stresses results, the bonded joint and hybrid joint of basalt-fiber reinforced plastic (BFRP) specimen’s produces higher results than bonded joint and hybrid joint of glass-fiber reinforced plastic (GFRP) specimens due to higher interfacial bonding strength. A well-designed bonded joint of BFRP laminates is very efficient for composite lap joint structures compared to hybrid (boned/riveted) joints. It is suggested that the application of basalt/epoxy laminate as a strengthening material is useful for joining of composite structural members in the engineering fields.},
     year = {2017}
    }
    

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    T1  - Structural Analysis of Glass Fiber / Epoxy and Basalt Fiber / Epoxy Lap Joint Specimens Using FEA
    AU  - Mohamed Bak Kamaludeen
    AU  - Kalaichelvan Kani
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    DO  - 10.11648/j.css.20170203.14
    T2  - Colloid and Surface Science
    JF  - Colloid and Surface Science
    JO  - Colloid and Surface Science
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    EP  - 117
    PB  - Science Publishing Group
    SN  - 2578-9236
    UR  - https://doi.org/10.11648/j.css.20170203.14
    AB  - The aim of this work is to predict the crack initiation and failure based on the Von Mises stress distributions at the edge of the overlap region. Finite Element Analysis (FEA) software is used to investigate the stress distribution under tensile loading on composite lap joints. From the Von Mises stresses results, the bonded joint and hybrid joint of basalt-fiber reinforced plastic (BFRP) specimen’s produces higher results than bonded joint and hybrid joint of glass-fiber reinforced plastic (GFRP) specimens due to higher interfacial bonding strength. A well-designed bonded joint of BFRP laminates is very efficient for composite lap joint structures compared to hybrid (boned/riveted) joints. It is suggested that the application of basalt/epoxy laminate as a strengthening material is useful for joining of composite structural members in the engineering fields.
    VL  - 2
    IS  - 3
    ER  - 

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Author Information
  • Department of Mechanical Engineering, Sri Shakthi Institute of Engineering and Technology, Coimbatore, India

  • Department of Ceramic Technology, Alagappa Chettiar Technology Campus, Anna University, Chennai, India

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