1. MSD crack propagation on a repaired aeronautic panel by DBEM;Citarella;Adv Eng Softw,2011
2. Non linear MSD crack growth by DBEM for a riveted aeronautic reinforcement;Citarella;Adv Eng Softw,2009
3. Baker AA, Jones R, editors. Bonded repair of aircraft structures. Martinus Nijhoff Publishers; 1988.
4. Baker AA, Chester RJ. Recent advances in bonded composite repair technology for metallic aircraft components. In: Proceeding of the international conference on advanced composite materials; 1993. p. 45–9.
5. Baker AA. Fatigue studies related to the certification of composite crack patching for primary metallic aircraft structure. In: FAA-NASA Symposium on continued airworthiness of aircraft structures. Atlanta, 28–30 August 1996.