Мақаланы E-mail арқылы жіберу Nonlinear Deformation and Stability of Discrete-Reinforced Elliptical Cylindrical Composite Shells under Torsion and Internal Pressure
- Авторлар: Zheleznov L.1, Kabanov V.1, Boiko D.1
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Мекемелер:
- Chaplygin Aeronautical Research Institute (SibNIA)
- Шығарылым: Том 61, № 2 (2018)
- Беттер: 175-182
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
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.
Авторлар туралы
L. Zheleznov
Chaplygin Aeronautical Research Institute (SibNIA)
Хат алмасуға жауапты Автор.
Email: lev.sheleznov@ocrv.ru
Ресей, ul. Polzunova 21, Novosibirsk, 630051
V. Kabanov
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Ресей, ul. Polzunova 21, Novosibirsk, 630051
D. Boiko
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
Ресей, ul. Polzunova 21, Novosibirsk, 630051
