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Comparison between rectangular and trapezoidal bonded composite repairs in aircraft structures: A numerical analysis

โœ Scribed by B. Bachir Bouiadjra; M. Fari Bouanani; A. Albedah; F. Benyahia; M. Es-Saheb


Publisher
Elsevier Science
Year
2011
Weight
753 KB
Volume
32
Category
Article
ISSN
0261-3069

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Numerical analysis of the effect of ther
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