BUCKLING ANALYSIS OF LAMINATED COMPOSITE PLATES

Authors

  • Gordana Tošić University of Banja Luka, Faculty of Mechanical Engineering, Banja Luka, Republic of Srpska, B&H
  • Vladimir Milovanović University of Kragujevac, Faculty of Engineering, Kragujevac, Serbia
  • Miroslav Živković University of Kragujevac, Faculty of Engineering, Kragujevac, Serbia
  • Bojana Grujić University of Banja Luka, Faculty of Architecture, Civil Engineering and Geodesy, Banja Luka, Republic of Srpska, B&H
  • Dragomir Miljanić University of Donja Gorica, Faculty of Polytechnics, Podgorica, Montenegro

DOI:

https://doi.org/10.7251/COMEN2501066T

Abstract

This paper deals with laminated plates subjected to uniaxial compression. The effects of lamination scheme and material properties on the critical loads are considered, as well as variations of boundary conditions and direction of the acting loads. The buckling analysis was conducted using the finite elements method implemented in the Simcenter Femap software package. The obtained results were compared with the already available ones.

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Published

2025-06-23

Issue

Vol. 16 No. 1 (2025): Contemporary Materials XVI‒1

Section

Articles