Dynamics of a discretely reinforced cylindrical shell under live load
- 作者: Antuf’ev B.1
-
隶属关系:
- Moscow Aviation Institute
- 期: 卷 59, 编号 3 (2016)
- 页面: 303-307
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/229735
- DOI: https://doi.org/10.3103/S1068799816030028
- ID: 229735
如何引用文章
详细
This study proposes an approximate solution to a contact problem of dynamic deformation of a cyclically symmetrical discretely ring-stiffened cylindrical shell, the side surface of which is subjected to an evenly distributed inertia live load. The solution of the problem assumes the quasistatic mode of deformation of the structure. Several critical velocities of the live load have been found. A number of examples are presented.
作者简介
B. Antuf’ev
Moscow Aviation Institute
编辑信件的主要联系方式.
Email: antufjev.bor@yandex.ru
俄罗斯联邦, Volokolamskoe shosse 4, Moscow, 125993