Prediction of compression after impact strength from surface profile of low-velocity impact damaged CFRP laminates using machine learning

被引:1
作者
Hasebe, Saki [1 ]
Higuchi, Ryo [1 ]
Yokozeki, Tomohiro [1 ]
Takeda, Shin-ichi [2 ]
机构
[1] Univ Tokyo, Dept Aeronaut & Astronaut, Bunkyo Ku, Tokyo 1138656, Japan
[2] Japan Aerosp Explorat Agcy JAXA, Aviat Technol Directorate, Mitaka, Tokyo 1810015, Japan
关键词
A. carbon fiber; A; laminate; B. compression after impact; COMPOSITES; BEHAVIOR; SIMULATION; PLATES;
D O I
10.1016/j.compositesa.2024.108560
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Recently, Composite materials have been increasingly used in various actual structures, leading to active research on their damage and residual material properties. Therefore, the residual compressive strength of carbon fiber reinforced plastic subjected to low-velocity impacts has been considered. In particular, we determined the complexity of impact conditions that can occur in practical applications and the difficulty of obtaining internal damage information from experimental specimens. In addition, we applied machine learning to investigate the essential features calculated from surface profile data after the impact tests. This learning revealed that features representing changes in the contour of the specimen surface had high contributions. Therefore, the surface damages, such as fiber breakage and major matrix cracks, also influence the CAI strength.
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页数:10
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