journal article·2018-03

Mixed-mode fracture of sandwich composites: Performance improvement with multiwalled carbon nanotube sonicated resin

Alak K Patra, Nilanjan Mitra

Publisher page

Abstract

An experimental investigation on sandwich composite materials composed of glass-fiber face sheet and polyvinyl-chloride foam core has been carried out. The research demonstrates improvement in mixed-mode delamination fracture toughness values of samples under mixed-mode bending condition. The improvement is recorded with addition of a certain percentage by weight of multiwalled carbon nanotubes in comparison to conventional samples. An easy and cost-effective methodology of multiwalled carbon nanotube insertion through sonication of epoxy resin followed by mixing with hardener and vacuum resin infusion technology for manufacturing of sandwich composites has been utilized in this study. The study also identifies the optimum weight percentage of multiwalled carbon nanotube addition in the resin system for maximum performance gain in mixed-mode fracture toughness. The results of observations in this study have been supported by field emission scanning electron microscope studies as well as high-resolution transmission electron microscope analysis.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Carbon Nanotubes in Composites · Mechanical Behavior of Composites · Smart Materials for Construction

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

Affiliations

Department of Civil Engineering, Indian Institute of Technology, Kharagpur, India

References (43)

Show source-provided references
1. 10.1016/j.compstruct.2009.10.00510.1016/j.compstruct.2009.10.005 ↗
2. 10.1016/j.compositesb.2011.11.03910.1016/j.compositesb.2011.11.039 ↗
3. 10.1016/S1359-835X(97)00057-210.1016/S1359-835X(97)00057-2 ↗
4. 10.1016/0266-3538(96)00052-810.1016/0266-3538(96)00052-8 ↗
5. 10.1016/S0263-8223(00)00019-210.1016/S0263-8223(00)00019-2 ↗
6. 10.1016/S1359-8368(01)00015-410.1016/S1359-8368(01)00015-4 ↗
7. Freitas G · J Adv Mater · 1994 · 25 · 36
8. 10.1016/S0263-8223(98)00110-X10.1016/S0263-8223(98)00110-X ↗
9. 10.1016/S0263-8223(01)00033-210.1016/S0263-8223(01)00033-2 ↗
10. 10.1016/S0266-3538(03)00273-210.1016/S0266-3538(03)00273-2 ↗
11. 10.1007/s10853-006-0114-810.1007/s10853-006-0114-8 ↗
12. 10.1016/j.compositesa.2007.08.01610.1016/j.compositesa.2007.08.016 ↗
13. 10.1016/S0266-3538(01)00052-510.1016/S0266-3538(01)00052-5 ↗
14. 10.1177/002199830404247510.1177/0021998304042475 ↗
15. 10.1016/j.compositesa.2010.07.00310.1016/j.compositesa.2010.07.003 ↗
16. 10.1039/c000041h10.1039/c000041h ↗
17. 10.1038/354056a010.1038/354056a0 ↗
18. 10.1038/4471066a10.1038/4471066a ↗
19. 10.1016/j.compscitech.2004.11.00310.1016/j.compscitech.2004.11.003 ↗
20. 10.1016/j.carbon.2012.01.05910.1016/j.carbon.2012.01.059 ↗
21. 10.1016/j.compscitech.2013.06.02110.1016/j.compscitech.2013.06.021 ↗
22. 10.1016/j.compscitech.2009.09.00110.1016/j.compscitech.2009.09.001 ↗
23. 10.1016/j.matdes.2013.07.08110.1016/j.matdes.2013.07.081 ↗
24. 10.1016/j.compscitech.2014.07.00610.1016/j.compscitech.2014.07.006 ↗
25. 10.1016/j.carbon.2009.06.03910.1016/j.carbon.2009.06.039 ↗
26. 10.1016/j.compositesa.2007.11.01310.1016/j.compositesa.2007.11.013 ↗
27. 10.1016/j.compscitech.2005.01.01410.1016/j.compscitech.2005.01.014 ↗
28. 10.1016/j.msea.2007.04.04310.1016/j.msea.2007.04.043 ↗
29. 10.1016/j.compositesb.2011.11.02010.1016/j.compositesb.2011.11.020 ↗
30. 10.1016/j.compositesb.2010.06.00110.1016/j.compositesb.2010.06.001 ↗
31. 10.1177/002199831141047210.1177/0021998311410472 ↗
32. 10.1016/j.engfracmech.2006.05.01510.1016/j.engfracmech.2006.05.015 ↗
33. 10.1016/j.compscitech.2013.10.01310.1016/j.compscitech.2013.10.013 ↗
34. 10.1016/j.engfracmech.2008.08.00310.1016/j.engfracmech.2008.08.003 ↗
35. 10.1177/002199830809773510.1177/0021998308097735 ↗
36. 10.1016/j.compositesa.2008.03.01110.1016/j.compositesa.2008.03.011 ↗
37. 10.1016/j.engfracmech.2011.06.02110.1016/j.engfracmech.2011.06.021 ↗
38. 10.2514/3.2520410.2514/3.25204 ↗
39. 10.1016/0266-3538(93)90031-B10.1016/0266-3538(93)90031-B ↗
40. ASTM Standard D6671/D6671M − 13 ɛ1 . Standard test method for mixed mode I-mode II interlaminar fracture toughness of unidirectional fiber reinforced polymer matrix composites 1 , 2013.
41. 10.1016/j.engfracmech.2008.12.00810.1016/j.engfracmech.2008.12.008 ↗
42. 10.1177/109963620910453310.1177/1099636209104533 ↗
43. 10.1016/j.compositesa.2009.08.02310.1016/j.compositesa.2009.08.023 ↗