Crack density estimation method for composite laminates based on discrete form stiffness degradation models

被引:1
作者
Ye, Jinrui [1 ]
Yuan, Mingqing [2 ]
Chen, Xin [3 ]
Liu, Zhendong [1 ]
Yang, Wei [3 ]
Zhao, Haitao [2 ]
Chen, Jian [2 ]
机构
[1] Beijing Inst Technol, Sch Aerosp Engn, Beijing, Peoples R China
[2] Shanghai Jiao Tong Univ, Sch Aeronaut & Astronaut, 800 Dongchuan Rd, Shanghai 200240, Peoples R China
[3] Global Energy Interconnect Res Inst Co Ltd, State Key Lab Adv Power Transmiss Technol, North Yingcai St Two, Beijing 100192, Peoples R China
关键词
Composite laminates; matrix cracking; crack density prediction; data-driven; stiffness degradation; MATRIX CRACKING; MECHANICAL-PROPERTIES; FRACTURE-TOUGHNESS; TRANSVERSE; DAMAGE; PREDICTION; REDUCTION; EVOLUTION; PERMEABILITY; STRESS;
D O I
10.1080/15376494.2023.2248132
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Matrix cracking of composite laminates leads to stiffness degradation and dominates the medium leakage of liner-less composite vessels. A stiffness degradation model can be established through the machine learning method, which provides only discrete form equivalent moduli data without explicit analytical results. This paper further explored the use of the discrete form data set of stiffness degradation in the crack density estimation for composite laminates by using an iterative process. Furthermore, different mixed-mode fracture criteria were discussed. The results showed that Benzeggagh-Kenane (B-K) criterion and the power law criterion are more appropriate in mixed-mode crack density analyses.
引用
收藏
页码:7631 / 7644
页数:14
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