Influence of matrix ductility on the high-temperature fatigue behaviour of notched and unnotched thermoplastic and thermoset laminates
Author:
Affiliation:
1. INSA Rouen – Groupe de Physique des Matériaux, UMR, CNRS, France
2. Université de Toulouse, INSA, UPS, Mines Albi – ICA/ISAE, Toulouse, France
Abstract
Publisher
SAGE Publications
Subject
Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/0731684415597074
Reference36 articles.
1. Thermoplastic vs. thermosetting structural composites
2. The experience of thermoplastic structural composites during processing
3. Influence of matrix ductility on the high-temperature fatigue behavior of off-axis woven-ply thermoplastic and thermoset laminates
4. About the creep-fatigue interaction on the fatigue behaviour of off-axis woven-ply thermoplastic laminates at temperatures higher than Tg
5. Influence of matrix ductility on the high-temperature fatigue behaviour of quasi-isotropic woven-ply thermoplastic and thermoset laminates
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1. Meso-structure-based thermomechanical modelling of thermoplastic-based laminates subjected to combined mechanical loading and severe thermal gradients;Composites Part A: Applied Science and Manufacturing;2022-11
2. High-temperature fatigue behavior of woven-ply thermoplastic composites;Fatigue Life Prediction of Composites and Composite Structures;2020
3. Modelling the deformation of continuous fibre-reinforced thermoplastics subjected to hygrothermal loading;Journal of Reinforced Plastics and Composites;2018-02-28
4. Fatigue accumulated damage in notched quasi-isotropic composites under high-temperature conditions: A discussion on the influence of matrix nature on the stress energy release rate;Journal of Composite Materials;2017-12-07
5. High-temperature fatigue behaviour of notched quasi-isotropic thermoplastic and thermoset laminates: Influence of matrix ductility on damage mechanisms and stress distribution;Composite Structures;2016-10
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