Email this article Dynamic Stability of an Orthotropic Cylindrical Shell of Piecewise Constant Thickness under the Action of External Pulsating Pressure
- Authors: Bakulin V.N.1, Nedbai A.Y.2, Shepeleva I.O.2
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Affiliations:
- Institute of Applied Mechanics
- AO Corporation Moscow Institute of Heat Technology
- Issue: Vol 62, No 2 (2019)
- Pages: 192-198
- Section: 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
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Abstract
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.
About the authors
V. N. Bakulin
Institute of Applied Mechanics
Author for correspondence.
Email: vbak@yandex.ru
Russian Federation, pr. Leningradskii 7, Moscow, 125040
A. Ya. Nedbai
AO Corporation Moscow Institute of Heat Technology
Email: vbak@yandex.ru
Russian Federation, alleya Berezovaya 10, Moscow, 127273
I. O. Shepeleva
AO Corporation Moscow Institute of Heat Technology
Email: vbak@yandex.ru
Russian Federation, alleya Berezovaya 10, Moscow, 127273
