Coupled thermoelasticity of shells of revolution: Effect of normal stress and coupling

Citation
Mr. Eslami et al., Coupled thermoelasticity of shells of revolution: Effect of normal stress and coupling, AIAA J, 37(4), 1999, pp. 496-504
Citations number
16
Categorie Soggetti
Aereospace Engineering
Journal title
AIAA JOURNAL
ISSN journal
00011452 → ACNP
Volume
37
Issue
4
Year of publication
1999
Pages
496 - 504
Database
ISI
SICI code
0001-1452(199904)37:4<496:CTOSOR>2.0.ZU;2-0
Abstract
The coupled thermoelasticity of shells of revolution, based on second-order shell theory, is considered, and the governing equations including normal stress and strain as well as the transverse shear and rotary inertia are co nsidered. The coupled energy equation based on the assumption of Lord and S hulman (Lord, H. W., and Shulman, Y., "A Generalized Dynamical Theory of Th ermoelasticity,'' Journal of Mechanics and Physics of Solids, Vol. 15, No. 5, 1967, pp. 299-309) is further considered, and the total system of equati ons is served by means of Galerkin finite element method. it is concluded t hat the inclusion of normal stress in the coupled equation is significant a nd for thin shells can result in a noticeable difference in shelf response compared to unassumed conditions.