Effect of interfacial fibre orientation and PPS veil density on delamination resistance of 5HS woven CFRP laminates under mode II loading
Source abstract
Abstract
Abstract This paper presents an experimental study on the effect of interfacial fibre orientation and interleaved thermoplastic veil on Mode II interlaminar fracture toughness of 5-harness satin woven carbon fibre reinforced polymer composite laminates. Three-point End-Notched Flexure tests were carried out to determine delamination resistance, GIIC, of specimens with five fibre orientation biases and two veil densities at the midplane. Results show that delamination resistance of 5-harness satin woven laminates depends on the layup configurations at the midplane with 90/45 fibre orientation bias exhibiting the greatest resistance. The delamination resistance enhancement from polyphenylene sulfide (PPS) veil interleaves is also fibre orientation dependent but a further increase of the veil density from 10 gm−2 to 20 gm−2 offers little extra benefit. Fracture surface morphologies were examined under SEM to understand the failure mechanism and fracture process of the woven laminate under the combined effects of the interfacial fibre orientation and the veil density. Fibre orientation relative to the delamination path, surface texture misfit, and veil density are the three main contributors identified for the variation of delamination resistance of 5HS woven laminates.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Mechanical Behavior of Composites · Fiber-reinforced polymer composites · Mechanical stress and fatigue analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (32)
Show source-provided references
1. Low-velocity impact behaviour of woven laminate plates with fire retardant resin10.1016/j.compositesb.2019.04.023 ↗
2. Progressive failure behaviours of 2D woven composites10.1177/0021998303037014002 ↗
3. An investigation of the damage tolerance of carbon/Benzoxazine composites with a thermoplastic toughening interlayer10.1016/j.compstruct.2016.03.015 ↗
4. The influence of the nonwoven veil architectures on interlaminar fracture toughness of interleaved composites10.1016/j.compscitech.2015.01.016 ↗
5. Electrospun nanofibers as reinforcement for composite laminates materials – a review10.1016/j.compstruct.2017.09.021 ↗
6. Toughening of thermosetting composites with thermoplastic fibres10.1016/j.msea.2005.08.028 ↗
7. Nanofibre bridging as a toughening mechanism in carbon/epoxy composite laminates interleaved with electrospun polyamide nanofibrous veils10.1016/j.compscitech.2015.06.021 ↗
8. Mode i and Mode II interlaminar fracture toughness of composite laminates interleaved with electrospun nanofibre veils10.1016/j.compositesa.2015.01.028 ↗
9. Comparison of intralaminar and interlaminar mode-I fracture toughness of unidirectional IM7/8552 graphite/epoxy composite
10. Damage control using discrete thermoplastic film inserts10.1016/j.compositesa.2012.01.011 ↗
11. Mode I interfacial toughening through discontinuous interleaves for damage suppression and control10.1016/j.compositesa.2011.10.009 ↗
12. Influence of interleaved films on the mechanical properties of carbon fiber fabric/polypropylene thermoplastic composites
13. On consideration the mode I fracture response of CFRP composite interleaved by composite nanofibers10.1016/j.mspro.2014.06.213 ↗
14. The influence of a thermoplastic toughening interlayer and hydrothermal conditioning on the Mode-II interlaminar fracture toughness of Carbon/Benzoxazine composites10.1016/j.compositesa.2015.11.010 ↗
15. Simultaneously improving mode I and mode II fracture toughness of the carbon fiber/epoxy composite laminates via interleaved with uniformly aligned PES fiber webs10.1016/j.compositesa.2019.105696 ↗
16. Using aligned nanofibres for identifying the toughening micromechanisms in nanofibre interleaved laminates10.1016/j.compscitech.2015.11.021 ↗
17. Strain rate dependence of mode II delamination resistance in through thickness reinforced laminated composites10.1016/j.ijimpeng.2017.05.003 ↗
18. Delamination migration in CFRP laminates under mode I loading10.1016/j.compscitech.2020.108067 ↗
19. Mode-II fracture behaviour of aerospace-grade carbon fibre/epoxy composites interleaved with thermoplastic veils10.1016/j.compscitech.2020.108065 ↗
20. Modeling delamination migration in cross-ply tape laminates10.1016/j.compositesa.2015.01.021 ↗
21. Interface fracture toughness of a multi-directional woven composite10.1007/s10704-013-9868-6 ↗
22. Effect of variation in fibre volume fraction on modes I and II delamination behaviour of 5HS woven composites manufactured by RTM10.1016/j.compscitech.2009.02.008 ↗
23. Damage development in woven carbon fibre thermoplastic laminates with PPS and PEEK matrices: a comparative study10.1177/0021998316653460 ↗
24. 2012 · 1
25. 2015 · 1
26. Standard test method for determination of the mode II interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites
27. Enhancing the fracture toughness of carbon fibre/epoxy composites by interleaving hybrid meltable/non-meltable thermoplastic veils10.1016/j.compstruct.2020.112699 ↗
28. The influence of interlayer/epoxy adhesion on the mode-I and mode-II fracture response of carbon fibre/epoxy composites interleaved with thermoplastic veils10.1016/j.matdes.2020.108781 ↗
29. Interlaminar to intralaminar mode I and II crack bifurcation due to aligned carbon nanotube reinforcement of aerospace-grade advanced composites10.1016/j.compscitech.2020.108014 ↗
30. Interdiffusing core-shell nanofiber interleaved composites for excellent Mode I and Mode II delamination resistance10.1016/j.compscitech.2019.03.019 ↗
31. Stress fluctuation, crack renucleation and toughening in layered materials10.1016/j.jmps.2018.04.011 ↗
32. Delamination migration in multidirectional composite laminates under mode I quasi-static and fatigue loading10.1016/j.compstruct.2018.01.074 ↗