Hybrid laminated materials with slow fatigue-crack development

V. V. Antipov; N. Yu. Serebrennikova; O. G. Senatorova; L. V. Morozova; N. F. Lukina; Yu. N. Nefedova

doi:10.3103/S1068798X17030030

Hybrid laminated materials with slow fatigue-crack development

Authors: Antipov V.V.¹, Serebrennikova N.Y.¹, Senatorova O.G.¹, Morozova L.V.¹, Lukina N.F.¹, Nefedova Y.N.¹
Affiliations:
1. Russian State Institute of Aviation Materials
Issue: Vol 37, No 3 (2017)
Pages: 195-199
Section: Article
URL: https://journal-vniispk.ru/1068-798X/article/view/227248
DOI: https://doi.org/10.3103/S1068798X17030030
ID: 227248

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Abstract

The use of light aluminum–lithium alloys with high elastic moduli in hybrid laminated materials for the production of skin panels in airplane wings is considered.