Method of evaluating the dynamics of cylindrical shells under the influence on them of the internal changing pressure

Applied Mathematics, Mechanics and Physics


Moiseev K. A.1*, Panov Y. N.2**

1. Peter the Great Strategic Missile Troops Academy, 17, Brigadnaya str., Serpukhov, Moscow region, 142210, Russia
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia



In the article is used original approach to a study of the dynamic behavior of the cylindrical shell, when it is not possible to use a condition of the orthogonality of the natural modes of vibration of shell for solving the partial differential equations.


thin circular anisotropic cylindrical shell, excess pressure, uniform acceleration, the average speed, natural modes of vibration, dynamicity coefficient — informational site of MAI

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