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- W2119128105 abstract "A closed form solution is presented that predicts the response of filament wound composite shells subjected to internal pressure. The material of the shell is assumed to be general cylindrically anisotropic. Based on the theory of cylindrical anisotropic elasticity coupled differential equations are developed using Lekhnitskii's stress function approach. Two composite systems, graphite/epoxy and glass/epoxy, are selected to demonstrate the influence of degree of material anisotropy and fiber orientations on the axial and induced twisting deformation. Detailed stress distributions of (45) off-axis unidirectional and (45/-45)s symmetric angle-ply fiber-reinforced laminated shells are shown to illustrate the effect of radius-to-thickness ratio and stacking sequence." @default.
- W2119128105 created "2016-06-24" @default.
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- W2119128105 date "1991-04-08" @default.
- W2119128105 modified "2023-09-22" @default.
- W2119128105 title "Analysis of laminated composite shells under internal pressure" @default.
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- W2119128105 doi "https://doi.org/10.2514/6.1991-958" @default.
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