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Comparison of double and single bonded repairs to symmetric composite structures: a numerical analysis

โœ Scribed by M Belhouari; B Bachir Bouiadjra; A Megueni; K Kaddouri


Book ID
108104690
Publisher
Elsevier Science
Year
2004
Tongue
English
Weight
395 KB
Volume
65
Category
Article
ISSN
0263-8223

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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