Abstract
The nonaxisymmetric thermally stressed state of laminar bodies of revolution made of isotropic and orthotropic materials is considered. The procedure used is based on the semi-analytical finite-element method and the method of successive approximations. The results from calculations for the stressed state of a structural element are reported. The structure has layers of isotropic and orthotropic materials with principal axes of anisotropy that coincide with the directions of the axes of the cylindrical and Cartesian coordinate systems.
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