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Analysis of the distribution of thermal residual stresses in bonded composite repair of metallic aircraft structures

โœ Scribed by L. Aminallah; T. Achour; B. Bachir Bouiadjra; B. Serier; A. Amrouche; X. Feaugas; N. Benssediq

Book ID
116375436
Publisher
Elsevier Science
Year
2009
Tongue
English
Weight
522 KB
Volume
46
Category
Article
ISSN
0927-0256

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Numerical analysis of the effect of ther
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