Buckling analysis of laminated cylindrical composite shell panel under mechanical and hygrothermal loads

Tran Ich Thinh, Le Kim Ngoc
Author affiliations

Authors

  • Tran Ich Thinh Hanoi University of Technology
  • Le Kim Ngoc Hanoi University of Technology

DOI:

https://doi.org/10.15625/0866-7136/27/1/5709

Keywords:

buckling, composite shell panels, hygrothermal effects, finite element, first-order shear deformation theory

Abstract

This paper deals with buckling of analysis multilaminated cylindrical shell panels subjected to axial and hygrothermal loadings. The geometrical non-linear analysis is carried out using the Finite Element Method based on a single layer first shear deformation theory. A nine-nodal isoparametric element with 5 degrees of freedom per node is considered. The effects of different number of layers, lamination angles, length to width ratios and hygrothermal effects are studied.

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Published

31-03-2005

How to Cite

[1]
T. I. Thinh and L. K. Ngoc, Buckling analysis of laminated cylindrical composite shell panel under mechanical and hygrothermal loads, Vietnam J. Mech. 27 (2005) 1–12. DOI: https://doi.org/10.15625/0866-7136/27/1/5709.

Issue

Vol. 27 No. 1 (2005)

Section

Research Article

License

Creative Commons License

This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.

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