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Numerical analysis of the beneficial effect of the double symmetric patch repair compared to single one in aircraft structures

✍ Scribed by B. Bachir Bouiadjra; H. Fekirini; B. Serier; M. Benguediab


Book ID
116374719
Publisher
Elsevier Science
Year
2007
Tongue
English
Weight
295 KB
Volume
38
Category
Article
ISSN
0927-0256

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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