Progressive failure analysis of fiber-reinforced laminated composites containing a hole
Source abstract
Abstract
The present work aims to obtain failure loads for open-hole unidirectional composite plates under tensile loading. For this purpose, a user-defined material model in the finite element analysis package, ABAQUS, was developed to predict the failure load of the open-hole composite laminates using progressive failure analysis. Hashin and modified Yamanda-Sun’s failure criteria with complete and Camanho’s material degradation model are studied. In order to achieve the most accurate predictions, the influence of failure criteria and property degradation rules are investigated and failure loads and failure modes of the composites are compared with the same experimental test results from literature. A good agreement between experimental results and numerical predictions was observed.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Composite Structure Analysis and Optimization · Fatigue and fracture mechanics
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Automotive Engineering, Iran University of Science and Technology, Iran
Impact and Composite Laboratory, Faculty of Mechanical Engineering, Tarbiat Modares University, Iran
Polymer Engineering Group, Faculty of Chemical Engineering, Tarbiat Modares University, Iran
References (27)
Show source-provided references
1. Afrouzian A, Movahhedi Aleni H, Liaghat G, et al. (2017) Effect of nano-particles on the tensile, flexural and perforation properties of the glass/epoxy composites. Journal of Reinforced Plastics and Composites . 1 January. DOI: 0731684417694753.10.1177/0731684417694753 ↗
2. 10.1177/00219983990330240210.1177/002199839903302402 ↗
3. 10.1177/00219983870210090410.1177/002199838702100904 ↗
4. 10.1177/00219983870210090310.1177/002199838702100903 ↗
5. 10.1007/s11029-014-9414-210.1007/s11029-014-9414-2 ↗
6. 10.1016/j.compstruct.2006.02.02410.1016/j.compstruct.2006.02.024 ↗
7. 10.1115/1.301382210.1115/1.3013822 ↗
8. 10.1115/1.315366410.1115/1.3153664 ↗
9. 10.1177/105678951557686310.1177/1056789515576863 ↗
10. 10.1177/105678951558143310.1177/1056789515581433 ↗
11. 10.1177/002199831246489110.1177/0021998312464891 ↗
12. 10.1016/j.compstruct.2009.04.04310.1016/j.compstruct.2009.04.043 ↗
13. Knight NF Jr and Reeder JR (2006) User-defined material model for progressive failure analysis. NASA technical report server, NASA Langley Research Center; Hampton, VA, US.
14. 10.1007/s11029-016-9540-010.1007/s11029-016-9540-0 ↗
15. 10.1177/002199830707413110.1177/0021998307074131 ↗
16. 10.1177/105678951557390010.1177/1056789515573900 ↗
17. 10.1023/B:MOCM.0000039744.98869.0d10.1023/B:MOCM.0000039744.98869.0d ↗
18. 10.1177/00219983960300070510.1177/002199839603000705 ↗
19. Taheri-Behrooz F and Bakhshan H (2016) Characteristic length determination of notched woven composites. Advanced Composite Materials . 28 September. DOI: 10.1080/09243046.2016.1232007.10.1080/09243046.2016.1232007 ↗
20. 10.1177/00219983910250050510.1177/002199839102500505 ↗
21. 10.1177/00219983710050010610.1177/002199837100500106 ↗
22. 10.1016/S1359-8368(02)00033-110.1016/S1359-8368(02)00033-1 ↗
23. 10.1046/j.1460-2695.2001.00424.x10.1046/j.1460-2695.2001.00424.x ↗
24. 10.1177/105678951350412310.1177/1056789513504123 ↗
25. 10.1177/00219983780120030510.1177/002199837801200305 ↗
26. 10.1016/j.compstruct.2013.10.02610.1016/j.compstruct.2013.10.026 ↗
27. 10.1177/002199831665977610.1177/0021998316659776 ↗