Progressive fatigue damage analysis of composite bolted joint using equivalent stress model
Author:
Affiliation:
1. College of Civil Engineering, Xijing University, Xi’an, China
2. Shaanxi Key Laboratory of Safety and Durability of Concrete Structures, Xijing University, Xi’an, China
Abstract
Funder
Fundamental Research Fund of Xijing University
Fund of Education Department of Shaanxi province
Publisher
SAGE Publications
Subject
Multidisciplinary
Link
http://journals.sagepub.com/doi/pdf/10.1177/0036850419874234
Reference23 articles.
1. Assessment of the fundamentals of failure theories for composite materials
2. Recommendations for designers and researchers resulting from the world-wide failure exercise
3. Progressive failure analysis of bolted single-lap composite joint based on extended finite element method
4. Experimental and numerical investigation on bolted composite joint made by vacuum assisted resin injection
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1. Progressive fatigue damage modeling of laminated composites using strain-based failure criteria;Journal of Composite Materials;2024-01-11
2. Uncertainty evaluation for bearing fatigue property of CFRP double-lap, single-bolt joints;Chinese Journal of Aeronautics;2022-03
3. Fracture analysis of fuselage wing joint developed by aerodynamic structural materials;Materials Today: Proceedings;2021
4. Revealing the competitive fatigue failure behaviour of CFRP-aluminum two-bolt, double-lap joints;Composite Structures;2020-07
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