Comparison between rectangular and trapezoidal bonded composite repairs in aircraft structures: A numerical analysis

Author:

Bachir Bouiadjra B.,Fari Bouanani M.,Albedah A.,Benyahia F.,Es-Saheb M.

Publisher

Elsevier BV

Subject

Applied Mathematics,General Mathematics

Reference26 articles.

1. Composites repairs to rib stiffened panels;Ting;J Compos Struct,1999

2. Baker A. 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; 1996. p. 28–30.

3. Repair of cracked or defective metallic aircraft components with advanced fiber composites—an overview of Australian work;Baker;J Compos Struct,1984

4. Baker A. Bonded composite repair of metallic aircraft components overview of Australian activities. In: AGARD-CP-550; 1995. p. 1–14.

5. Bonded composite repair of fatigue-cracked primary aircraft structure;Baker;J Compos Struct,1999

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