A modelling technique for calculating stress intensity factors for structures reinforced by bonded straps. Part I: Mechanisms and formulation

Author:

Boscolo M.,Zhang X.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference51 articles.

1. Schmidt HJ, Voto C, Hansson J. Tango metallic fuselage barrel validation of advanced technologies. In: Rouchon J, editor. Proceedings of the 21st symposium of the international committee on aeronautical fatigue, ICAF, Cepadues Editionss; 2001. p. 273–88.

2. Schmidt HJ, Schmidt-Brandecker B. Damage tolerance design and analysis of current and future aircraft structure. In: AIAA/ICAS international air and space symposium and exposition: the next 100 years, Dayton, Ohio; 2003 [aIAA 2003-2784].

3. Pacchione M, Telgkamp J. Challenges of the metallic fusolage. In: 25th ICAS conference, Hamburg; 2006.

4. Crack stoppers and arall laminates;Schijve;Engng Fract Mech,1990

5. Heinimann MB, Bucci RJ, Kulak M, Garratt M. Improving damage tolerance of aircraft structures through the use of selective reinforcement. In: Proceedings 23rd symposium of international committee on aeronautical fatigue (ICAF), Hamburg; 2005. p. 197–208.

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