2006
DOI: 10.1007/s10778-006-0134-8
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Axisymmetric thermoelastoplastic stress-strain state of transversely isotropic laminated shells

Abstract: The method of successive approximations is used to determine the thermoelastoplastic stress-strain state of isotropic and transversally isotropic laminated shells of revolution under axisymmetric loading. Hill's theory of plasticity with isotropic hardening is used to describe the deformation of transversely isotropic materials, while the theory of deformation along paths of small curvature is used to describe the deformation of isotropic materials. The elastoplastic stress-strain state of a two-layer cylindri… Show more

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Cited by 10 publications
(11 citation statements)
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“…The system of governing equations (3.9) is solved by a numerical time-stepping method and by the method of successive approximations at each step, satisfying prescribed boundary conditions [5][6][7][8]. An algorithm to solve this system of equations may be the following.…”
mentioning
confidence: 99%
“…The system of governing equations (3.9) is solved by a numerical time-stepping method and by the method of successive approximations at each step, satisfying prescribed boundary conditions [5][6][7][8]. An algorithm to solve this system of equations may be the following.…”
mentioning
confidence: 99%
“…However, no numerical data are available on the stress-strain state (SSS) of such shells subject to nonuniform heating. The paper [1] reports on the results from an axisymmetric thermoelastoplastic stress-strain analysis of laminated isotropic and transversely isotropic shells subject to nonuniform heating. These results were obtained using a technique [8] based on the Kirchhoff-Love hypotheses and a geometrically linear formulation, and the effect of temperature on stresses and strains in these shells was evaluated.…”
Section: Introductionmentioning
confidence: 99%
“…Expanding upon the studies [1,8], the present paper generalizes the technique outlined therein to axisymmetric geometrically nonlinear problems of thermoplasticity for transversely isotropic shells and discusses numerical results.…”
Section: Introductionmentioning
confidence: 99%
“…] and beyond [5,6,[12][13][14] the elasticity limits. The tensile and compressive moduli of these materials were assumed to be equal.…”
Section: Introductionmentioning
confidence: 99%
“…Methods for analysis of the axisymmetric thermoelastoplastic stress-strain state (SSS) of laminated shells of revolution have been developed for isotropic and anisotropic inelastic materials deforming within [3, 4, 11, 16, etc.] and beyond [5,6,[12][13][14] the elasticity limits. The tensile and compressive moduli of these materials were assumed to be equal.…”
mentioning
confidence: 99%