Nonlinear Deformation and Stability of Discrete-Reinforced Elliptical Cylindrical Composite Shells under Torsion and Internal Pressure
- Авторы: Zheleznov L.P.1, Kabanov V.V.1, Boiko D.V.1
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Учреждения:
- Chaplygin Aeronautical Research Institute (SibNIA)
- Выпуск: Том 61, № 2 (2018)
- Страницы: 175-182
- Раздел: 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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Аннотация
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.
Об авторах
L. Zheleznov
Chaplygin Aeronautical Research Institute (SibNIA)
Автор, ответственный за переписку.
Email: lev.sheleznov@ocrv.ru
Россия, ul. Polzunova 21, Novosibirsk, 630051
V. Kabanov
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Россия, ul. Polzunova 21, Novosibirsk, 630051
D. Boiko
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Россия, ul. Polzunova 21, Novosibirsk, 630051
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