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Buckling Analysis of Folded Composite Plate Subjected to In-Plane Loading Condition

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Advanced Materials

Part of the book series: Springer Proceedings in Materials ((SPM,volume 6))

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Abstract

This paper presents some numerical results of buckling analysis of a folded laminate composite plate using finite element method. The effects of fiber orientations, folding angle on buckling loads, and the corresponding mode shapes under in-plane loading condition were considered. Matlab programming using nine nodded rectangular isoparametric plate element with five degree of freedom per node based on Mindlin plate theory was built to solve the problems. A good agreement is found between the results of this technique and other published results available in the literature.

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Author information

Authors and Affiliations

  1. University of Power Electric, Hanoi, Viet Nam

    Bui Van Binh & Le Thuong Hien

Authors
  1. Bui Van Binh
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  2. Le Thuong Hien
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Corresponding author

Correspondence to Bui Van Binh .

Editor information

Editors and Affiliations

  1. I. I. Vorovich Mathematics, Mechanics and Computer Sciences Institute, Southern Federal University, Rostov-on-Don, Russia

    Ivan A. Parinov

  2. Department of Microelectronics Engineering, National Kaohsiung University of Science and Technology, Kaohsiung, Taiwan

    Shun-Hsyung Chang

  3. School of Mechanical Engineering, Hanoi University of Science and Technology, Hanoi, Vietnam

    Banh Tien Long

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Van Binh, B., Hien, L.T. (2020). Buckling Analysis of Folded Composite Plate Subjected to In-Plane Loading Condition. In: Parinov, I., Chang, SH., Long, B. (eds) Advanced Materials. Springer Proceedings in Materials, vol 6. Springer, Cham. https://doi.org/10.1007/978-3-030-45120-2_10

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