The technique of definition of critical dynamic loading of a cylindrical composite environment in conditions of complex temperature and force loading

Aviation technics and technology


Аuthors

Larichev E. A.*, Safronov V. S.**, Turkin I. K.***

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: evgenij-tarichev@rambler.ru
**e-mail: v.s.safronov@mail.ru
***e-mail: kafedra_602@mail.ru

Abstract

This article is devoted to the technique of definition of critical dynamic loading of a cylindrical composite environment in conditions of complex temperature and force loading. Results of the numerical decision of the differential equations of research of dynamic behaviour of cylindrical environments from composite materials are submitted.


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