电邮这篇文章 Nonlinear Deformation and Stability of Discrete-Reinforced Elliptical Cylindrical Composite Shells under Torsion and Internal Pressure
- 作者: Zheleznov L.1, Kabanov V.1, Boiko D.1
-
隶属关系:
- Chaplygin Aeronautical Research Institute (SibNIA)
- 期: 卷 61, 编号 2 (2018)
- 页面: 175-182
- 栏目: 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
如何引用文章
开放存取
##reader.subscriptionAccessGranted##
订阅存取
详细
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.
作者简介
L. Zheleznov
Chaplygin Aeronautical Research Institute (SibNIA)
编辑信件的主要联系方式.
Email: lev.sheleznov@ocrv.ru
俄罗斯联邦, ul. Polzunova 21, Novosibirsk, 630051
V. Kabanov
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
俄罗斯联邦, ul. Polzunova 21, Novosibirsk, 630051
D. Boiko
Chaplygin Aeronautical Research Institute (SibNIA)
Email: lev.sheleznov@ocrv.ru
俄罗斯联邦, ul. Polzunova 21, Novosibirsk, 630051
