Author:
Bachir Bouiadjra B.,Fari Bouanani M.,Albedah A.,Benyahia F.,Es-Saheb M.
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
Cited by
36 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献