2010
DOI: 10.1007/s12541-010-0110-4
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Buckling analysis of filament-wound thick composite cylinder under hydrostatic pressure

Abstract: NOMENCLATURE E1,E2,E2 = Elastic Modulus G12,G23,G13 = Shear Modulus v12 ,v23, v13 = Poisson's ratio IntroductionUnderwater vehicles, that operate in deep water, are subjected to high external hydrostatic pressure. In general, the pressure hull of an underwater vehicle has a stiffened cylindrical shell structure, and the spherical or elliptic shells are attached to both ends. Shell is the structure often found in vessels, submarines, aircrafts, and buildings. Accordingly, there have been many studies on the ana… Show more

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Cited by 17 publications
(11 citation statements)
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“…Li and Lin (2010) calculated the nonlinear buckling and post-buckling of a moderately thick anisotropic laminated cylindrical shell based on a higher-order shear deformation shell theory. Hur et al (2008), Moon et al (2010), and Kim et al (2010) investigated the post-buckling behavior and failure of filament-wound composite cylinders using the nonlinear finite element method (NLFEM) and experiments. Deyet al (2014) numerically analyzed the post-buckling characteristics of moderately thick-walled composite cylinders using NLFEM.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Li and Lin (2010) calculated the nonlinear buckling and post-buckling of a moderately thick anisotropic laminated cylindrical shell based on a higher-order shear deformation shell theory. Hur et al (2008), Moon et al (2010), and Kim et al (2010) investigated the post-buckling behavior and failure of filament-wound composite cylinders using the nonlinear finite element method (NLFEM) and experiments. Deyet al (2014) numerically analyzed the post-buckling characteristics of moderately thick-walled composite cylinders using NLFEM.…”
Section: Introductionmentioning
confidence: 99%
“…Messager et al (2002) later developed an analytical buckling shell model based on third-order shear deformable theory and compared the results with NLFEM and experimental results. Kim et al (2010) and Jung et al (2012) compared two analytical buckling pressure formulations, i.e., the ASME and NASA formulas, with NLFEM or experimental results. Rao Yarrapragada et al (2012) used the Windenburg equation, which was developed for homogeneous materials, to predict the critical buckling pressure of composite shells with equivalent stiffness moduli, and compared the results with NLFEM.…”
Section: Introductionmentioning
confidence: 99%
“…Kim et al. 23 developed the finite element technique to analyze the buckling of a filament-wound thick composite cylinder and performed a hydrostatic pressure experiment. Messager et al.…”
Section: Introductionmentioning
confidence: 99%
“…Lee and Bang developed an approach for estimation of lateral buckling of a wind turbine tower with a thin circular wall through finite element (FE) analysis to ensure structure safety [8]. Kim et al carried out a buckling analysis of filament-wound composite cylinder subject to deep water high hydrostatic pressure [9], and so forth.…”
Section: Introductionmentioning
confidence: 99%