๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Bonded boron-epoxy composite repair and reinforcement of cracked aluminium structures

โœ Scribed by T.E. Tay; F.S. Chau; C.J. Er

Publisher
Elsevier Science
Year
1996
Tongue
English
Weight
859 KB
Volume
34
Category
Article
ISSN
0263-8223

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

Finite element analysis of cracks in agi
Finite element analysis of cracks in aging aircraft structures with bonded composite-patch repairs
โœ Linxia Gu; Ananth Ram Mahanth Kasavajhala; Shijia Zhao ๐Ÿ“‚ Article ๐Ÿ“… 2011 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 609 KB

Bonded composite-patch repair has been used to transfer load from cracked structures to the reinforcement such that subsequent crack propagation is reduced. In this study, the mechanical behavior of a single edge v-notch Al7075-T6 plate repaired with 1-ply and 4-ply composite patches was investigate

Mixed-mode numerical and experimental fa
Mixed-mode numerical and experimental fatigue crack growth analyses of thick aluminium panels repaired with composite patches
โœ H. Hosseini-Toudeshky; B. Mohammadi ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 873 KB

In this paper, fatigue crack growth of repaired thick aluminium panels containing a central inclined crack is studied. The cracked panels were repaired on one side with glass/epoxy composite patches. Effects of patch lay-up configuration on starting the crack growth after bonding and crack growth ra