A numerical model for the accumulation of transverse cracks in a composite laminate subjected to tensile fatigue loading-Reference-Cited by-同舟云学术

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A numerical model for the accumulation of transverse cracks in a composite laminate subjected to tensile fatigue loading

Published:1994-01 Issue:3 Volume:50 Page:285-291
ISSN:0266-3538
Container-title:Composites Science and Technology
language:en
Short-container-title:Composites Science and Technology

Author:

Gamby D.

Publisher

Elsevier BV

Subject

General Engineering,Ceramics and Composites

Reference16 articles.

1. Influence of the stacking sequence on fatigue transverse ply cracking in cross-ply laminates;Hénaff-Gardin,1992

2. Application of the Paris equation to the fatigue growth of transverse ply cracks;Boniface;J. Comp. Mater.,1989

3. Formation and growth of 90° ply fatigue cracks in carbon/epoxy laminates;Lafarie-Frenot;Comp. Sci. & Technol.,1991

4. On the development of transverse ply cracks during fatigue loading;Ogin,1987

5. Elastic-plastic stress waves;Nicholas,1982

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Dynamic Damage Problems of Damaged Materials;Continuum Damage Mechanics and Numerical Applications;2010

2. Propagation of edge cracking towards the centre of laminated composite plates subjected to fatigue loading;Composite Structures;2002-05

3. Fatigue behavior of textile composite materials subjected to tension-tension loads;Polymer Composites;2001-12

4. Modelling of fatigue microcracking kinetics in crossply composites and experimental validation;Composites Science and Technology;1999-07

5. Kinematic Waves and Nonuniform Damage Development in Composite Laminates;International Journal of Damage Mechanics;1997-01

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