Implementation of integrated approach to winged missile transport loads assignment.

Space technics and technology


Аuthors

Aleksushin S. V.

State Engineering Design Bureau “Raduga” named after AY Bereznyak, 2а, Zhukovskogo str., Dubna, Moscow region, 141980, Russia

e-mail: serg_al@inbox.ru

Abstract

Complex procedures and programs, realizing unified loads assignment approach for structure fatigue evaluation and transport bench test conditions setting, are presented. Flying vehicles transport loads evaluation methods are considered. The methods include simulation of moving on random road profile and determinate road irregularities. Corresponding evaluation examples presented. Cyclic loads evaluation technique with use of dynamic simulation and in-situ loads measurements are suggested.

Keywords:

loads; dynamics; transport; flying vehicle; durability.


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