Отправить статью по E-mail Investigation of Buckling Behavior for Thin-Walled Bearing Aircraft Structural Elements with Cutouts by Means of Numerical Simulation
- Авторы: Dmitriev V.G.1, Egorova O.V.1, Zhavoronok S.I.2, Rabinskii L.N.1
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Учреждения:
- Moscow Aviation Institute (National Research University)
- Institute of Applied Mechanics
- Выпуск: Том 61, № 2 (2018)
- Страницы: 165-174
- Раздел: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230468
- DOI: https://doi.org/10.3103/S1068799818020034
- ID: 230468
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Аннотация
In this paper, we develop the consistent mathematical models and appropriate lowconsuming numerical methods for investigating the nonlinear strain and buckling behavior of statically loaded thin-walled structures with cutouts. The numerical simulation allowed us to study the effects of the dimensions of rectangular cutouts on the buckling of cylindrical shells loaded by the external pressure.
Об авторах
V. Dmitriev
Moscow Aviation Institute (National Research University)
Автор, ответственный за переписку.
Email: vgd2105@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
O. Egorova
Moscow Aviation Institute (National Research University)
Email: vgd2105@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
S. Zhavoronok
Institute of Applied Mechanics
Email: vgd2105@mail.ru
Россия, Leningradskii pr. 7, Moscow, 125040
L. Rabinskii
Moscow Aviation Institute (National Research University)
Email: vgd2105@mail.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
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