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Stress distribution in continuously heterogeneous thick laminated pressure vessels

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dc.contributor.author Verijenko, Viktor E.
dc.contributor.author Adali, Sarp
dc.contributor.author Tabakov, Pavel Y.
dc.date.accessioned 2011-08-01T07:31:19Z
dc.date.available 2011-08-01T07:31:19Z
dc.date.issued 2001
dc.identifier.uri http://hdl.handle.net/10321/642
dc.description Originally published in: Composite Structures, Vol. 54, No. 2-3, 2001. en_US
dc.description.abstract Stress analysis of multilayered pressure vessels possessing cylindrical anisotropy and under internal, external and interlaminar pressures is given. The special case when the axis of anisotropy coincides with the axis of symmetry Oz and the stresses do not vary along the generator is investigated. In this case there exists a plane of elastic symmetry normal to this axis at every point of the cylinder so that each layer may be considered as orthotropic. However, elastic properties can vary through the thickness of a layer. Exact elasticity solutions are obtained for both open-ended and closed-ended cylinders using a stress function approach. The method of solution allows the forces on the layer interfaces to be taken into account with relative ease. Numerical results are presented for thick cylinders with isotropic and orthotropic layers, and stress distributions across the thickness are shown. en_US
dc.format.extent pp. 371-377 (7 p.) en_US
dc.language.iso en en_US
dc.publisher Elsevier en_US
dc.rights The electronic version of the article published in Composite Structures 2001, 54(2-3): 371-377 © 2001 copyright Elsevier. Composite Structures available online at: http://www.sciencedirect.com/science/article/pii/S026382230100112X en_US
dc.subject Anisotropic cylinder en_US
dc.subject Laminated pressure vessel en_US
dc.subject Stress analysis of heterogenous cylinders en_US
dc.title Stress distribution in continuously heterogeneous thick laminated pressure vessels en_US
dc.type Article en_US
dc.publisher.uri http://dx.doi.org/10.1016/S0263-8223(01)00112-X en_US


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