Dynamic deformation of a design of the aviation products at joint operation with the carrier

Aviation technics and technology


Loshkarev A. N.1*, Sidorenko A. S.2**

1. Research and Production Association “BAZALT”, 32, Velyaminovskaya str., Moscow, 105318, Russia
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: cheraken@mail.ru
**e-mail: k906@mai.ru


The procedure and results of the of the stress-strain state’s numerical analysis of elements of an aeronautical engineering’s structure at dynamic loading in the conditions of joint operation with the carrier are presented. Working out of the final-element model of a structure with the account of a structural features and loading conditions is executed. On the basis of computational researches dynamic characteristics and the maximum stresses for a bearing surface of an aeronautical engineering are defined.


aeronautical engineering; load-carrying surface; damping; oscillations; dynamic analysis; vibration accelerations; vibration stresses.


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