Отправить статью по E-mail Dynamic Stability of an Orthotropic Cylindrical Shell of Piecewise Constant Thickness under the Action of External Pulsating Pressure
- Авторы: Bakulin V.1, Nedbai A.2, Shepeleva I.2
-
Учреждения:
- Institute of Applied Mechanics
- AO Corporation Moscow Institute of Heat Technology
- Выпуск: Том 62, № 2 (2019)
- Страницы: 192-198
- Раздел: 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
Цитировать
Открытый доступ
Доступ предоставлен
Только для подписчиков
Аннотация
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.
Об авторах
V. Bakulin
Institute of Applied Mechanics
Автор, ответственный за переписку.
Email: vbak@yandex.ru
Россия, pr. Leningradskii 7, Moscow, 125040
A. Nedbai
AO Corporation Moscow Institute of Heat Technology
Email: vbak@yandex.ru
Россия, alleya Berezovaya 10, Moscow, 127273
I. Shepeleva
AO Corporation Moscow Institute of Heat Technology
Email: vbak@yandex.ru
Россия, alleya Berezovaya 10, Moscow, 127273
