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Three-dimensional Finite Element Buckling Analysis of Honeycomb Sandwich Composite Shells with Cutouts
Corresponding author. Department of Engineering Mechanics, Tsinghua University, Beijing, 100084, P. R. China Tel.: +86-10-62772902; fax: +86-10-62781824; E-mail address: xuemd@mail.tsinghua.edu.cn
Computers, Materials & Continua 2005, 2(2), 139-150. https://doi.org/10.3970/cmc.2005.002.139
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This paper investigates the buckling response of honeycomb sandwich composite shells with cutouts under axial compression. The Wilson's incompatible solid Finite Element (FE) is used around cutouts to obtain the detail stress distribution there. While to reduce the computational expense, a special multilayered relative degrees-of-freedom (DOF) shell FE is used to model the regions far from the cutouts. The efficiency and accuracy of this modeling scheme are illustrated by two benchmarks. Then parametric studies are carried out to reveal how the buckling response is influenced by the area, the shape and the orientation of cutouts.Keywords
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APA Style
Li, J., Xiang, Z.H., Xue, M.D. (2005). Three-dimensional finite element buckling analysis of honeycomb sandwich composite shells with cutouts. Computers, Materials & Continua, 2(2), 139-150. https://doi.org/10.3970/cmc.2005.002.139
Vancouver Style
Li J, Xiang ZH, Xue MD. Three-dimensional finite element buckling analysis of honeycomb sandwich composite shells with cutouts. Comput Mater Contin. 2005;2(2):139-150 https://doi.org/10.3970/cmc.2005.002.139
IEEE Style
J. Li, Z.H. Xiang, and M.D. Xue "Three-dimensional Finite Element Buckling Analysis of Honeycomb Sandwich Composite Shells with Cutouts," Comput. Mater. Contin., vol. 2, no. 2, pp. 139-150. 2005. https://doi.org/10.3970/cmc.2005.002.139
This work is licensed under a Creative Commons Attribution 4.0 International License , which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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