Investigation of Buckling Behavior for Thin-Walled Bearing Aircraft Structural Elements with Cutouts by Means of Numerical Simulation
- 作者: Dmitriev V.G.1, Egorova O.V.1, Zhavoronok S.I.2, Rabinskii L.N.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- Institute of Applied Mechanics
- 期: 卷 61, 编号 2 (2018)
- 页面: 165-174
- 栏目: 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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详细
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.
作者简介
V. Dmitriev
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: vgd2105@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
O. Egorova
Moscow Aviation Institute (National Research University)
Email: vgd2105@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
S. Zhavoronok
Institute of Applied Mechanics
Email: vgd2105@mail.ru
俄罗斯联邦, Leningradskii pr. 7, Moscow, 125040
L. Rabinskii
Moscow Aviation Institute (National Research University)
Email: vgd2105@mail.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
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