Fatigue simulation for titanium/CFRP hybrid laminates using cohesive elements

Author:

Yamaguchi T.,Okabe T.,Yashiro S.

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference10 articles.

1. Development of fibre metal laminates for advanced aerospace structures;Vogelesang;J Mater Process Technol,2000

2. Fatigue damage mechanisms in advanced hybrid titanium composite laminates;Rhymer;Int J Fatigue,2002

3. Modeling of facesheet crack growth in titanium–graphite hybrid laminates, Part I;Burianek;Eng Fract Mech,2003

4. Modeling of facesheet crack growth in titanium–graphite hybrid laminates. Part II: experimental results;Burianek;Eng Fract Mech,2003

5. Okabe T, Yashiro S. Numerical simulation for predicting fatigue damage progress in notched CFRP cross-ply laminates by using cohesive elements. Trans Jpn Soc Mech Eng, 2009;751:304–9 [in Japanese].

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