Comparison of mixed mode fracture criteria in finite element analysis for matrix crack density estimation of laminated composites
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, China
2. School of Materials Science and Engineering, Beihang University, China
3. Shanghai Institute of Aerospace System Engineering, China
Abstract
Funder
Shanghai Aerospace Science and Technology Innovation Foundation
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
http://journals.sagepub.com/doi/pdf/10.1177/0021998320948246
Reference28 articles.
1. Analysis and Experiment of Gas Leakage Through Composite Laminates for Propellant Tanks
2. Modeling of permeation and damage in graphite/epoxy laminates for cryogenic fuel storage
3. Modeling of permeation and damage in graphite/epoxy laminates for cryogenic tanks in the presence of delaminations and stitch cracks
4. Evaluation of gas leakage through composite laminates with multilayer matrix cracks: Cracking angle effects
5. Semi‐Empirical Modeling of Gas Permeability Induced by Multilayer Matrix Cracks in Composite Laminates
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1. Enhancing the ability of strain energy release rate criterion for fracture assessment of orthotropic materials under mixed-mode I/II loading considering the effect of crack tip damage zone;STEEL COMPOS STRUCT;2022
2. Numerical Method for Predicting Permeability of Laminated Composites at Cryogenic Temperature;AIAA Journal;2021-07
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