The method of estimation of dynamics of cylindrical shells under impact

Mathematics. Physics. Mechanics


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

The article uses a combined method of investigation of the dynamic behavior of anisotropic cylindrical shell reinforced by irregular set of circular ribs, which allows to obtained an analytical solution for a system of different eguations in partial derivaties.

Keywords:

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


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