Optimisation of structure of hybrid composition materials for aircraft

Lavrov A.V., Erasov V.S., Podzhivotov N.Y., Avtaev V.V.
UDC
539.3
DOI
10.18577/2307-6046-2016-0-11-7-7
Article PDF (Russian) (596.55 KB)
How to cite
Lavrov A.V., Erasov V.S., Podzhivotov N.Y., Avtaev V.V. Optimisation of structure of hybrid composition materials for aircraft // Proceedings of VIAM. 2016. No. 11. DOI: 10.18577/2307-6046-2016-0-11-7-7. URL: https://test.viam.ru/en/journal/2016/11/7
Keywords
composition laminate materials, hybrid composition materials.
Abstract

Layered hybrid metal-plastic composite materials are considered in the article from the point of view of optimisation of their composition for various conditions of functioning. Positioning and thickness influence of high-rigid layers on cylindrical rigidity of the composite is shown at a symmetric and asymmetric (unilateral) bend. Recommendations for choice of hybrid composites for various kinds of loads are given. The work is executed within the implementation of the complex scientific direction 6. «Layered metal-plastic, bimetallic and hybrid materials» («The strategic directions of development of materials and technologies of their processing for the period till 2030»)

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