journal article·2013-11

Open hole flexural and izod impact strength of unidirectional flax yarn reinforced polypropylene composites as a function of laminate lay‐up

T. Gobi Kannan, Chang Mou Wu, Kuo Bing Cheng

Polymer Composites· Volume 34· Issue 11
Publisher page

Abstract

An open hole flexural strength and impact energy of flax yarn‐reinforced polypropylene (PP) composites were studied in this work. Highest flexural strength and strength retention were observed for axial (06) and cross‐ply (0/90/0)s laminates, respectively, while also examining the influence of laminate lay‐up and open hole size on flexural strength. It was found that maleic anhydride‐grafted polypropylene (MAPP)‐treated composite laminates achieved marginal improvement on flexural strength for all kinds of laminate lay‐up. Off‐axial laminates (±456) showed a good strength retention for open hole laminates after MAPP treatment. The fractography study confirmed microbuckling and matrix crack propagation over the compressive and tensile side of the laminate, respectively. Furthermore, severe surface damage was detected over the tensile side of 8‐mm hole size laminates. Impact test of the flax/PP laminates showed slight improvement by MAPP treatment. High‐ and low‐impact energy was experienced for axial and off‐axial laminates. The damaged impact sample shows evidence of fiber pull‐out for untreated flax yarn reinforced laminates. POLYM. COMPOS., 34:1912–1920, 2013. © 2013 Society of Plastics Engineers
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Natural Fiber Reinforced Composites · Mechanical Behavior of Composites · Textile materials and evaluations

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

Affiliations

Department of Fiber and Composite Materials Feng Chia University Taichung 40724 Taiwan, R.O.C.

Department of Materials Science and Engineering National Taiwan University of Science and Technology Taipei 10607 Taiwan, R.O.C

References (24)

Show source-provided references
1. 10.1002/app.2071210.1002/app.20712 ↗
2. 10.1016/j.indcrop.2011.05.02010.1016/j.indcrop.2011.05.020 ↗
3. 10.1016/S1359-835X(01)00116-610.1016/S1359-835X(01)00116-6 ↗
4. 10.1016/S0924-0136(03)00195-X10.1016/S0924-0136(03)00195-X ↗
5. 10.1002/app.1286610.1002/app.12866 ↗
6. 10.1016/j.compositesa.2003.09.01410.1016/j.compositesa.2003.09.014 ↗
7. 10.1002/pen.2132810.1002/pen.21328 ↗
8. 10.1002/pc.2004010.1002/pc.20040 ↗
9. 10.1016/S0266-3538(03)00094-010.1016/S0266-3538(03)00094-0 ↗
10. 10.1016/S0021-9797(03)00294-710.1016/S0021-9797(03)00294-7 ↗
11. 10.1177/073168440403286810.1177/0731684404032868 ↗
12. 10.1016/j.compscitech.2009.09.01610.1016/j.compscitech.2009.09.016 ↗
13. 10.1016/j.compscitech.2011.08.00110.1016/j.compscitech.2011.08.001 ↗
14. 10.1016/j.compstruct.2003.09.01810.1016/j.compstruct.2003.09.018 ↗
15. 10.1016/j.compositesa.2006.07.00810.1016/j.compositesa.2006.07.008 ↗
16. 10.1016/S0266-3538(98)00154-710.1016/S0266-3538(98)00154-7 ↗
17. 10.1016/S0266-3538(01)00201-910.1016/S0266-3538(01)00201-9 ↗
18. 10.1016/j.compscitech.2005.10.00610.1016/j.compscitech.2005.10.006 ↗
19. 10.1016/S0266-3538(03)00261-610.1016/S0266-3538(03)00261-6 ↗
20. 10.1016/j.compositesb.2012.04.04710.1016/j.compositesb.2012.04.047 ↗
21. 10.1177/152808371244269510.1177/1528083712442695 ↗
22. 10.1002/mame.20030004010.1002/mame.200300040 ↗
23. 10.1016/j.compscitech.2005.01.01610.1016/j.compscitech.2005.01.016 ↗
24. 10.3144/expresspolymlett.2011.2210.3144/expresspolymlett.2011.22 ↗