Tensile Properties of Z-pins Reinforced Laminates
Source abstract
Abstract
The delamination toughness of Z-pins reinforced laminates could be improved significantly and in-plane mechanical properties of the laminates were degraded with a few of Z-pins inserted in the through-thickness direction. The influence of Z-pin inserted parameters and moisture absorption condition on the tensile properties of the laminates was experimentally studied. The results showed that Z-pins can change microstructure and the original stress-strain state of the Z-pinned laminates, and the tensile strength and modulus of the laminates were obviously influenced. The tensile modulus of the Z-pinned laminates decreased with the increasing of Z-pins’ diameter and volume content, while it increased with that of Z-pins’ angle. The moisture absorption rate and balanced moisture content of Z-pinned laminates increased due to Z-pin inserted, which eventually resulted in accelerating degradation of performance of composites laminates.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Textile materials and evaluations · Composite Structure Analysis and Optimization
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016
References (19)
Show source-provided references
1. Yi X.S. · 2006
2. Chen X.B. · 2006
3. Chen X.B. · J. Materials China · 2009 · 28 · 2
4. Chen S.J. · Chinese Journal of Aeronautics · 2008 · 29 · 605
5. Liu D.J. · J. Journal of Materials Engineering · 2008 · 194
6. Sun X.N. · J. Chinese Journal of Aeronautics · 2006 · 27 · 1194
7. 10.1007/BF0054065210.1007/BF00540652 ↗
8. Joshi S.P. · Journal of Material Science · 1985 · 51
9. DelBrey J. · 1991
10. Huang S.L. · Proceedings of the American Society of Mechanical Engineers · 1978 · 10
11. BoyceJ.S., FreitasG.A., MageeC.L. , Ultrasonic fastening system and method P., S Patent, WO 98/29243, 1998.
12. Frietas G. · Proceedings of the 9th DoD/NASA/FAA conference on fibrous composites C · 1991
13. 10.1016/S1359-835X(04)00180-010.1016/S1359-835X(04)00180-0 ↗
14. 10.1016/j.compscitech.2006.02.02910.1016/j.compscitech.2006.02.029 ↗
15. 10.1016/j.compositesa.2005.11.01310.1016/j.compositesa.2005.11.013 ↗
16. 10.1016/j.compositesa.2006.05.00410.1016/j.compositesa.2006.05.004 ↗
17. 10.1016/j.compscitech.2007.04.01710.1016/j.compscitech.2007.04.017 ↗
18. Sun X.N. · Chinese Journal of Aeronautics · 2009 · 26 · 186
19. Sun X.N. · Chinese Journal of Aeronautics · 2009 · 26 · 193