Thermoelastic problem for a physically orthotropic cylindrical shell at localized temperature

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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Bibliographic Details
Published in:Russian aeronautics 2013-07, Vol.56 (3), p.229-233
Main Authors: Nerubailo, B. V., Zui, Vu Ba
Format: Article
Language:English
Subjects:
Anisotropy
Automotive Engineering
Engineering
Structural Mechanics and Strength of Flight Vehicles
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Description
Summary: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.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799813030045