电邮这篇文章 Hybrid laminated materials with slow fatigue-crack development
- 作者: Antipov V.V.1, Serebrennikova N.Y.1, Senatorova O.G.1, Morozova L.V.1, Lukina N.F.1, Nefedova Y.N.1
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隶属关系:
- Russian State Institute of Aviation Materials
- 期: 卷 37, 编号 3 (2017)
- 页面: 195-199
- 栏目: Article
- URL: https://journals.rcsi.science/1068-798X/article/view/227248
- DOI: https://doi.org/10.3103/S1068798X17030030
- ID: 227248
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详细
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.
作者简介
V. Antipov
Russian State Institute of Aviation Materials
Email: serebrusha@mail.ru
俄罗斯联邦, Moscow
N. Serebrennikova
Russian State Institute of Aviation Materials
编辑信件的主要联系方式.
Email: serebrusha@mail.ru
俄罗斯联邦, Moscow
O. Senatorova
Russian State Institute of Aviation Materials
Email: serebrusha@mail.ru
俄罗斯联邦, Moscow
L. Morozova
Russian State Institute of Aviation Materials
Email: serebrusha@mail.ru
俄罗斯联邦, Moscow
N. Lukina
Russian State Institute of Aviation Materials
Email: serebrusha@mail.ru
俄罗斯联邦, Moscow
Yu. Nefedova
Russian State Institute of Aviation Materials
Email: serebrusha@mail.ru
俄罗斯联邦, Moscow
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