Bonded fiber-composite doublers are increasingly being used to reinforce and/or repair damaged or underdesigned metallic aircraft structure. This trend will continue as the average age of Australian civilian and military aircraft increases. Two mathematical models of the stress state in bonded doublers are presented in this report: the end-tapered double-lap joint and the stepped double-lap joint. The mathematical development of the two models is detailed and the fidelity of the predicted stress states compared with that obtained from finite element analyses and experiment.... Aircraft repair, Fatigue damage repair, Bonded composite repairs, Doublers (repair).
Mathematical Modelling of Bonded Fibre-Composite Repairs to Aircraft
1993
35 pages
Report
No indication
English
On the Certification of Bonded Repairs to Primary Composite Aircraft Components
Tema Archive | 2015
|On the certification of bonded composite repairs to primary aircraft structure
Tema Archive | 1997
|Fatigue Damage Prediction for Bonded Composite Repairs Applied to Metallic Aircraft Structures
SAE Technical Papers | 2001
|Bonded Composite Repairs for Aging Commercial Aircraft - A Multi-National Research Effort
British Library Conference Proceedings | 1999
|