Translaminar fracture toughness and fatigue crack growth characterization of carbon‐epoxy plain weave laminates
Author:
Affiliation:
1. Department of Aeronautical EngineeringTechnological Institute of Aeronautics, Praça Marechal do Ar Eduardo Gomes São Paulo Brazil
2. Lightweight Structures LaboratoryTechnology Park, Estrada Dr. Altino Bondensan São Paulo Brazil
Funder
Conselho Nacional de Desenvolvimento Científico e Tecnológico
Publisher
Wiley
Subject
Materials Chemistry,Polymers and Plastics,General Chemistry,Ceramics and Composites
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/pc.25247
Reference30 articles.
1. A Comparison of the Fracture Behavior of Thick Laminated Composites Utilizing Compact Tension, Three-Point Bend, and Center-Cracked Tension Specimens
2. The interlaminar and intralaminar fracture toughness of carbon-fibre/polymer composites: The effect of temperature
3. Developing a four point bend specimen to measure the mode I intralaminar fracture toughness of unidirectional laminated composites
4. Intralaminar fracture toughness of a cross-ply laminate and its constituent sub-laminates
5. Mode-I fracture toughness testing of thick section FRP composites using the ESE(T) specimen
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