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- W2321837609 abstract "Linear formulations are insufficient to take into account the effect of large deflections that occur after initial buckling. This effect can only be considered in the non-linear buckling analysis. In the present work, the non-linear analysis is carried out using the finite element method based on first-order shear deformation shell theories. Two non-linear shell theories, Donnel’s and Sanders’ theories, are used in the analysis. Based on the first-ply failure analysis and non-linear buckling analysis, the critical sizes and parameters of the tapered curved plates that will not fail before global buckling are determined. A parametric study that encompasses the effects of taper angle, critical length-to-height ratio, radius, radius-to-thickness ratio and geometric parameters of the plates is conducted." @default.
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- W2321837609 date "2011-01-01" @default.
- W2321837609 modified "2023-09-28" @default.
- W2321837609 title "Non-linear buckling analysis of tapered curved composite plates" @default.
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- W2321837609 doi "https://doi.org/10.1515/secm.2011.026" @default.
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