๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Finite element analysis of crack growth in adhesively bonded joints

โœ Scribed by S.C. Pradhan; N.G.R. Iyengar; N.N. Kishore


Publisher
Elsevier Science
Year
1995
Tongue
English
Weight
748 KB
Volume
15
Category
Article
ISSN
0143-7496

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Boundary element analysis of adhesively
โœ Madhukar Vable; JaiHind Reddy Maddi ๐Ÿ“‚ Article ๐Ÿ“… 2006 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 385 KB

Boundary element method has proven to have very good resolution of large stress gradients, yet its application in analysis of bonded joints is practically non-existent even though large stress gradients exist in the bonded region and bonded joints are one of the critical technology in modern design.

Finite element analysis of slow crack gr
โœ Shanyi Du; James D. Lee ๐Ÿ“‚ Article ๐Ÿ“… 1982 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 645 KB

finite element analysis of the process of slow crack growth is made for center-cracked specimens subjected to monotonically increasing load until the point of fast fracture is reached. The formulation is based on an incremental theory of plasticity with isotropic hardening. Numerical results and exp

Bonded joints with composite adherends.
โœ Abdelaziz A. Taib; Rachid Boukhili; Said Achiou; Hychem Boukehili ๐Ÿ“‚ Article ๐Ÿ“… 2006 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 743 KB

This paper describes a finite element analysis of two adhesive bonded joint configurations, namely single lap joint and joggle lap joint, for which an extensive experimental analysis had been made previously. The adherends were assumed to behave as linearly elastic materials, while the adhesive laye

Prediction of fatigue crack growth rates
โœ Hassan Alizadeh; Sarinova Simandjuntak; David Smith; Martyn Pavier ๐Ÿ“‚ Article ๐Ÿ“… 2007 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 177 KB

A three-dimensional finite element fatigue crack closure model of a corner crack and of a through thickness crack has been developed to evaluate the range of effective stress intensity factor from the distribution of the range of stress ahead of the crack tip. The corresponding fatigue crack growth