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Numerical analysis of the patch shape effects on the performances of bonded composite repair in aircraft structures

โœ Scribed by Mhamdia Rachid; B. Serier; B. Bachir Bouiadjra; M. Belhouari

Book ID
113552024
Publisher
Elsevier Science
Year
2012
Tongue
English
Weight
676 KB
Volume
43
Category
Article
ISSN
1359-8368

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Numerical analysis of the effect of thermal residual stresses on the performances of bonded composite repairs in aircraft structures
โœ A. Albedah; B. Bachir Bouiadjra; L. Aminallah; M. Es-Saheb; F. Benyahia ๐Ÿ“‚ Article ๐Ÿ“… 2011 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 590 KB

In this study the finite element method is used to analyse the effect of the thermal residual stresses resulting from adhesive curing on the performances of the bonded composite repair in aircraft structures. The stress-intensity factor at the crack tip is chosen as fracture criterion in order to es