Abstract
Numerical results obtained based on the equations for the general theory of physically orthotropic shells are presented. These results illustrate the influence of anisotropy for mechanical and physical characteristics of material on stressed state.
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Original Russian Text © B.V. Nerubailo, Vu Ba Zui, 2013, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2013, No.3, pp. 15–18.
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Nerubailo, B.V., Zui, V.B. Thermoelastic problem for a physically orthotropic cylindrical shell at localized temperature. Russ. Aeronaut. 56, 229–233 (2013). https://doi.org/10.3103/S1068799813030045
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DOI: https://doi.org/10.3103/S1068799813030045