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

Аuthors

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

*e-mail: moiseev.1946@bk.ru
**e-mail: gi@mai.ru

Abstract

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.

Keywords:

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