РОЗРАХУНОК ЗУСИЛЬ ФОРМОУТВОРЕННЯ ПАНЕЛЕЙ ПОВІТРЯНОГО СУДНА ПРИ ПОСЛІДОВНОМУ ВІЛЬНОМУ ГНУТТІ НА СПЕЦІАЛІЗОВАНОМУ ОБЛАДНАННІ
Published in Open Information and Computer Integrated Technologies • Jul 29, 2019
NobleIDNI9P83W63R16S23
Authors:,,
С. А. Бычков
Б. В. Лупкин
А. А. Павленко
Abstract
The design of a modern aircraft provides for a high degree of panelizing of outline elements which can reach up to 80...85%. This allows to increase strength and rigidity with a simultaneous reduction in weight and improved flight performance of the product by reducing the number of fasteners and ri...
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