International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110317 - 110317
Опубликована: Май 1, 2025
Язык: Английский
International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110317 - 110317
Опубликована: Май 1, 2025
Язык: Английский
Thin-Walled Structures, Год журнала: 2025, Номер 210, С. 113062 - 113062
Опубликована: Фев. 7, 2025
Язык: Английский
Процитировано
3International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110123 - 110123
Опубликована: Март 1, 2025
Язык: Английский
Процитировано
3Advanced Engineering Materials, Год журнала: 2025, Номер unknown
Опубликована: Апрель 8, 2025
This study investigates the mechanical performance of continuous carbon fiber reinforced composite (CCFRC) honeycomb structures with varying Poisson's ratios, fabricated using fused filament fabrication (FFF) technique. Three designs—star shaped (SS), concave hexagonal (CHH), and zero ratio (ZPR)—are evaluated through static compression experiments finite element simulations. The results show that SS a negative exhibits higher yield strength, faster densification, greater total energy absorption. In contrast, positive (PPR) demonstrates larger specific absorption, while ZPR are more stable in deformation. Notably, for same ratio, outperforms CHH terms mass increases 98.58% 101%, respectively. Scanning electron microscopy (SEM) analysis damage mechanisms during highlights influence unit cell design printing path planning on properties CCFRC components. These findings suggest behavior is highly dependent print planning, tensile failure typically leading to brittle fracture.
Язык: Английский
Процитировано
0International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110317 - 110317
Опубликована: Май 1, 2025
Язык: Английский
Процитировано
0