journal article·2023-09Open access

The influence of yarn fiber volume fraction, shear angle, and yarn spacing on crack propagation resistance of plain‐woven fabric‐reinforced epoxy composites

Volkan Arikan

Polymer Composites· Volume 44· Issue 9

Abstract

Abstract This study investigated the effect of fabric parameters on crack propagation in plain‐woven e‐glass reinforced epoxy composite plates. Through numerical analyses, the study contributes to understanding the effect of fabric structure on crack propagation and adopting a more precise approach in the design of composite materials. The yarn fiber volume fraction, shear angle, and yarn spacing parameters were selected as variables for the plain‐woven fabric, and material properties were determined for each parameter using the composite homogenization method. A finite element model was created using the Ansys software package, and stress intensity factors (SIFs) and tear stress values were obtained under mode I loading to investigate the effects of fabric structure on crack propagation. The results showed that as the yarn fiber volume fraction ratio increased, the SIF values decreased and the T‐stress values increased. When evaluated according to the shear angle of the yarn, the lowest SIF value was obtained for the 0‐degree shear angle. The same was observed for T‐stress values as well. Additionally, compared to the fabric structure aligned along the X‐axis, a significant decrease occurred in the SIF value due to the perpendicular fiber density increase to the crack propagation direction with symmetric orientation.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Vibration and Dynamic Analysis · Composite Structure Analysis and Optimization

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Mechanical Engineering Osmaniye Korkut Ata University Osmaniye Turkey

References (34)

Show source-provided references
1. 10.1177/147592172092292210.1177/1475921720922922 ↗
2. 10.1016/j.polymertesting.2018.10.03910.1016/j.polymertesting.2018.10.039 ↗
3. 10.1088/1757‐899X/788/1/01200410.1088/1757‐899X/788/1/012004 ↗
4. 10.3390/polym1318312910.3390/polym13183129 ↗
5. 10.1111/ffe.1212010.1111/ffe.12120 ↗
6. 10.1016/j.jmrt.2020.04.08310.1016/j.jmrt.2020.04.083 ↗
7. 10.1016/j.engfracmech.2016.08.01510.1016/j.engfracmech.2016.08.015 ↗
8. 10.1016/0013‐7944(74)90007‐110.1016/0013‐7944(74)90007‐1 ↗
9. 10.1016/j.engfracmech.2022.10853310.1016/j.engfracmech.2022.108533 ↗
10. 10.1016/S0013‐7944(02)00099‐110.1016/S0013‐7944(02)00099‐1 ↗
11. SukumarN SrolovitzDJ.Finite element‐based model for crack propagation in polycrystalline materials.2004.10.1590/S1807-03022004000200014 ↗
12. 10.1016/j.ijsolstr.2003.08.00110.1016/j.ijsolstr.2003.08.001 ↗
13. 10.1002/pc.2706510.1002/pc.27065 ↗
14. 10.1016/j.engfracmech.2016.11.02710.1016/j.engfracmech.2016.11.027 ↗
15. 10.1016/j.engfracmech.2006.12.02710.1016/j.engfracmech.2006.12.027 ↗
16. 10.1016/0020‐7683(92)90138‐J10.1016/0020‐7683(92)90138‐J ↗
17. 10.4028/www.scientific.net/AMR.772.17310.4028/www.scientific.net/AMR.772.173 ↗
18. 10.17577/IJERTV9IS06024310.17577/IJERTV9IS060243 ↗
19. 10.1002/pc.1052310.1002/pc.10523 ↗
20. 10.1002/pc.2078510.1002/pc.20785 ↗
21. 10.1177/152808371143391210.1177/1528083711433912 ↗
22. 10.3390/textiles102002010.3390/textiles1020020 ↗
23. 10.1088/1757‐899X/477/1/01205510.1088/1757‐899X/477/1/012055 ↗
24. 10.1002/pc.2229410.1002/pc.22294 ↗
25. Voyiadjis GZ · 2005 · 193
26. The determination of the elastic field of an ellipsoidal inclusion, and related problems
27. 10.1016/j.compstruct.2022.11556010.1016/j.compstruct.2022.115560 ↗
28. 10.1016/j.compstruct.2022.11649610.1016/j.compstruct.2022.116496 ↗
29. 10.1016/j.compstruct.2023.11707010.1016/j.compstruct.2023.117070 ↗
30. 10.1177/108128651880552110.1177/1081286518805521 ↗
31. 10.1533/9780857092502.1.9110.1533/9780857092502.1.91 ↗
32. 10.1016/B978-0-12-814191-5.00009-710.1016/B978-0-12-814191-5.00009-7 ↗
33. 10.1016/j.compstruct.2022.11614010.1016/j.compstruct.2022.116140 ↗
34. 2022