Dynamics of a discretely reinforced cylindrical shell under live load
- Авторлар: Antuf’ev B.A.1
-
Мекемелер:
- Moscow Aviation Institute
- Шығарылым: Том 59, № 3 (2016)
- Беттер: 303-307
- Бөлім: 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
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
B. Antuf’ev
Moscow Aviation Institute
Хат алмасуға жауапты Автор.
Email: antufjev.bor@yandex.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
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