Buckling analysis of laminated cylindrical composite shell panel under mechanical and hygrothermal loads
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DOI:
https://doi.org/10.15625/0866-7136/27/1/5709Keywords:
buckling, composite shell panels, hygrothermal effects, finite element, first-order shear deformation theoryAbstract
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
Thinh, T. I., & Ngoc, L. K. (2005). Buckling analysis of laminated cylindrical composite shell panel under mechanical and hygrothermal loads. Vietnam Journal of Mechanics, 27(1), 1–12. https://doi.org/10.15625/0866-7136/27/1/5709
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