Numerical analysis of the performances of the bonded composite patch for reducing stress concentration and repairing cracks at notch

Author:

Achour T,Bouiadjra B.Bachir,Serier B

Publisher

Elsevier BV

Subject

Computational Mathematics,General Physics and Astronomy,Mechanics of Materials,General Materials Science,General Chemistry,General Computer Science

Reference20 articles.

1. Bonded Repair of Aircraft Structures,1988

2. A.A. Baker, R.J. Chester, Recent advances in bonded composite repair technology for metallic aircraft components, in: Proceeding of the International Conference on Advanced Composite Materials, 1993, pp. 45–49

3. A.A. Baker, Fatigue studies related to the certification of composite crack patching for primary metallic aircraft structure, FAA-NASA Symposium on Continued Airworthiness of Aircraft Structures, Atlanta, 28–30 August 1996

4. A.A. Baker, On the certification of bonded composite repairs primary aircraft structures, in: Proceeding of the Eleventh International of composite Materials (ICCM-11). Gold Coast, Australia, 1997

5. Repair of mirage iii aircraft using BFRP crack patching technology;Baker;Theoretical and Applied Fracture Mechanics,1984

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