Numerical analysis of the effect of thermal residual stresses on the performances of bonded composite repairs in aircraft structures

Author:

Albedah A.,Bachir Bouiadjra B.,Aminallah L.,Es-Saheb M.,Benyahia F.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference24 articles.

1. Advances in the bonded composite repair of metallic aircraft structures;Baker,2002

2. Baker AA. Fatigue studies related to the certification of composite crack patching for primary metallic aircraft structure. In Presented at FAA-NASA symposium on continued airworthiness of aircraft structures. Atlanta; 28–30 August 1996.

3. Baker AA. 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.

4. Joining and repair of aircraft composite structures;Baker,1997

5. Thermal stresses in plate with a circular reinforcement;Wang;Int J Solids Struct,2000

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