Fatigue crack growth prediction in GLARE hybrid laminates

Author:

Shim D.J.,Alderliesten R.C.,Spearing S.M.,Burianek D.A.

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference14 articles.

1. Fibre metal laminates: an introduction;Vlot,2001

2. Low-fatigue material saves weight in A380;Dornheim;Aviation Week & Space Technology,1995

3. Takamatsu T, Matsumura T, Ogura N, Shimokawa T, Kakuta Y. Fatigue crack growth properties of a fiber/metal laminate Glare. Fatigue '99: Proceedings of the Seventh International Fatigue Congress. Beijing, China: 1999; p. 1725–30.

4. A theoretical model for predicting fatigue crack growth rates in fibre-reinforced metal laminates;Guo;Fatigue and Fracture of Engineering Materials and Structures,1998

5. Delamination growth and its effect on crack propagation in carbon fiber reinforced aluminum laminates under fatigue loading;Lin;Acta Mater.,1996

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