Exact solution for laminated continuous open cylindrical shells

Abstract

Discarding any assumption about displacement models and stress distribution and introducing d-function into the present study, we established the state equation for the continuous orthotropic open cylindrical shells. An identical exact solution is presented for the itatics of thin, moderately. thick and thick laminated continuous open cylindrical shells. NumericaI results are obtained and compared with those calculated using SAPS.

Review of elasto-static models for three-dimensional analysis of thick-walled anisotropic tubes

“…In the research group surrounding Fan, Sheng and Ye, numerous publications were developed to the state-space approach of thick-walled plates, shells or cylindrical shells (tubes), see i. a. Fan and Sheng 63 and Sheng and Le. 64 In Fan and Ding, 65 a pipe or closed cylindrical shell clamped on both sides under internal pressure is analytically described.…”

Finite element formulation of a heat transfer problem for an axisymmetric composite structure

“…On one hand, many researchers [1,[4][5][6][7] pay their attention to the determination of thermal transfer properties of orthotropic materials. On the other hand, a lot of scholars deal with analysis for temperature fields and thermal stresses in composite structures, for example, see Ref [8][9][10][11][12][13][14].…”

Transient Thermoelastic Problem of Angle-Ply Laminated Cylindrical Panel due to Nonuniform Heat Supply

“…Therefore the thermoelastic problems of anisotropic cylindrical panel with curvature are important as well as those of plate models in the design board. Though there are several exact analysis for the isothermal problems of anisotropic laminated cylindrical panel [3][4][5][6][7], there are only a few exact analyses concerned with the thermoelastic problems of anisotropic laminated cylindrical panel taking into account transverse stress components. For example, Huang and Tauchert treated exactly a cross-ply cylindrical panel [8] and a doubly-curved cross-ply laminate [9] with simply supported edges as a three-dimensional thermoelastic problem.…”