电邮这篇文章 Research on Nonlinear Deformation and Stability of an Advanced Aircraft Fuselage Composite Section under Pure Bending
- 作者: Belov V.1, Zheleznov L.1, Ognyanova T.1
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隶属关系:
- S. A. Chaplygin Aeronautical Research Institute (SibNIA)
- 期: 卷 60, 编号 4 (2017)
- 页面: 514-522
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230272
- DOI: https://doi.org/10.3103/S1068799817040067
- ID: 230272
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详细
The finite element algorithm developed by the authors has been used for solving the strength and stability problems of shells. The effect of deformation nonlinearity, stiffness of stringer set, shell thickness on critical loads has been determined.
作者简介
V. Belov
S. A. Chaplygin Aeronautical Research Institute (SibNIA)
Email: to19@list.ru
俄罗斯联邦, ul. Polzunova 21, Novosibirsk, 630051
L. Zheleznov
S. A. Chaplygin Aeronautical Research Institute (SibNIA)
Email: to19@list.ru
俄罗斯联邦, ul. Polzunova 21, Novosibirsk, 630051
T. Ognyanova
S. A. Chaplygin Aeronautical Research Institute (SibNIA)
编辑信件的主要联系方式.
Email: to19@list.ru
俄罗斯联邦, ul. Polzunova 21, Novosibirsk, 630051
