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Torsional buckling of functionally graded graphene reinforced composite laminated cylindrical panel

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Abstract

In this study, torsional buckling behavior of a laminated composite cylindrical shell panel reinforced with graphene nano-sheets is analyzed. Using the theory of linear three-dimensional elasticity and based on the principle of virtual work and finite element method, equilibrium equations are extracted. Buckling loads are obtained based on a generalized geometric stiffness concept. Halpin-Sai equations are also used to obtain the mechanical properties of the composite material. The effects of weight fractions and graphene distribution pattern along the thickness of the shell, and zigzag and armchair layup of graphene platelets on the torsional buckling loads are investigated. Five graphene distribution patterns FG-X, FG-O, FG-Ʌ, FG-V and UD are utilized in this study. The 15 models of GPL distribution and arrangement of composite layers are investigated.

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Authors and Affiliations

  1. Department of Civil Engineering, University of Bonab, Bonab, East Azerbaijan, Iran

    Somayeh Mollaei

  2. Department of Mechanical Engineering, University of Eyvanekey, Eyvanekey, Semnan, Iran

    Masoud Babaei

  3. Department of Mechanical Engineering, Islamic Azad University, North Tehran Branch, Tehran, Iran

    Kamran Asemi

Authors
  1. Somayeh Mollaei
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  2. Masoud Babaei
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  3. Kamran Asemi
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Correspondence to Somayeh Mollaei or Kamran Asemi.

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Mollaei, S., Babaei, M. & Asemi, K. Torsional buckling of functionally graded graphene reinforced composite laminated cylindrical panel. Arch Appl Mech 93, 427–435 (2023). https://doi.org/10.1007/s00419-022-02132-2

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  • DOI: https://doi.org/10.1007/s00419-022-02132-2

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