Enviar artigo por via de e-mail Nonlinear Deformation and Stability of Discrete-Reinforced Elliptical Cylindrical Composite Shells under Torsion and Internal Pressure
- Autores: Zheleznov L.1, Kabanov V.1, Boiko D.1
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Afiliações:
- Chaplygin Aeronautical Research Institute (SibNIA)
- Edição: Volume 61, Nº 2 (2018)
- Páginas: 175-182
- Seção: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230472
- DOI: https://doi.org/10.3103/S1068799818020046
- ID: 230472
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Resumo
The problem of strength and stability of shells under torsion and internal pressure was solved. It was found out the influence of the internal pressure, ellipticity and nonlinearity of deformation on the critical buckling load of the shell.
Sobre autores
L. Zheleznov
Chaplygin Aeronautical Research Institute (SibNIA)
Autor responsável pela correspondência
Email: lev.sheleznov@ocrv.ru
Rússia, ul. Polzunova 21, Novosibirsk, 630051
V. Kabanov
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Rússia, ul. Polzunova 21, Novosibirsk, 630051
D. Boiko
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Rússia, ul. Polzunova 21, Novosibirsk, 630051
