Dynamic Stability of an Orthotropic Cylindrical Shell of Piecewise Constant Thickness under the Action of External Pulsating Pressure
- 作者: Bakulin V.1, Nedbai A.2, Shepeleva I.2
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隶属关系:
- Institute of Applied Mechanics
- AO Corporation Moscow Institute of Heat Technology
- 期: 卷 62, 编号 2 (2019)
- 页面: 192-198
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230912
- DOI: https://doi.org/10.3103/S106879981902003X
- ID: 230912
如何引用文章
详细
For a shell with three sections, dependences of the critical frequency on the different thicknesses of these sections are obtained. The error of the assumptions accepted at constructing the mathematical model of a shell is evaluated.
作者简介
V. Bakulin
Institute of Applied Mechanics
编辑信件的主要联系方式.
Email: vbak@yandex.ru
俄罗斯联邦, pr. Leningradskii 7, Moscow, 125040
A. Nedbai
AO Corporation Moscow Institute of Heat Technology
Email: vbak@yandex.ru
俄罗斯联邦, alleya Berezovaya 10, Moscow, 127273
I. Shepeleva
AO Corporation Moscow Institute of Heat Technology
Email: vbak@yandex.ru
俄罗斯联邦, alleya Berezovaya 10, Moscow, 127273