Stress analysis of laminates of carbon fiber reinforced plastics, containing transverse cracks, considering free-edge effect and residual thermal stress-Reference-Cited by-同舟云学术

Stress analysis of laminates of carbon fiber reinforced plastics, containing transverse cracks, considering free-edge effect and residual thermal stress

Published:2008-12 Issue:1-2 Volume:498 Page:69-75
ISSN:0921-5093
Container-title:Materials Science and Engineering: A
language:en
Short-container-title:Materials Science and Engineering: A

Author:

Hosoi Atsushi,Kawada Hiroyuki

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Reference14 articles.

1. High-cycle fatigue characteristics of quasi-isotropic CFRP laminates

2. The initiation and growth of delaminations induced by matrix microcracks in laminated composites

3. Initiation and growth of delamination from the tips of transverse cracks in CFRP cross-ply laminates

4. The effect of delaminations induced by transverse cracks and splits on stiffness properties of composite laminates

5. Delaminations induced by constrained transverse cracking in symmetric composite laminates

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1. Free-Edge Effects in Composite Laminates—A Review of Recent Developments 2005–2020;Applied Mechanics Reviews;2022-01-01

2. Semi-analytical Model for the Close-Range Stress Analysis of Transverse Cracks in Composite Plates;Recent Approaches in the Theory of Plates and Plate-Like Structures;2021-12-30

3. Semi‐analytical method for the stress analysis of transverse cracks in composite structures;PAMM;2021-12

4. In-situ Tensile and Fatigue Testing for Detection of Interfacial Debonding between Carbon Fibers and Epoxy Matrix by Synchrotron Radiation X-ray Nano-CT;Journal of the Japan Society for Composite Materials;2021-09-15

5. Effect of fatigue loading on stiffness degradation, energy dissipation, and matrix cracking damage of CFRP [±45] 3S composite laminate;Fatigue & Fracture of Engineering Materials & Structures;2019-06-19