Dynamic deformation of a design of the aviation products at joint operation with the carrier
Aviation technics and technology
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
AbstractThe 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.
Keywords:aeronautical engineering; load-carrying surface; damping; oscillations; dynamic analysis; vibration accelerations; vibration stresses.