Email this article Dynamics of a discretely reinforced cylindrical shell under live load
- Authors: Antuf’ev B.A.1
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Affiliations:
- Moscow Aviation Institute
- Issue: Vol 59, No 3 (2016)
- Pages: 303-307
- Section: 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
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Abstract
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.
About the authors
B. A. Antuf’ev
Moscow Aviation Institute
Author for correspondence.
Email: antufjev.bor@yandex.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
