journal article·2022-10Open access

Decomposing the coupling damage in mode I multidirectional delamination

Ping Hu, Ran Tao, Xiaole Li, Gilles Lubineau

Abstract

The mode I delamination properties between carbon fiber reinforced polymer (CFRP) plies are difficult to measure because the coupling between the intralaminar and interlaminar damage makes delamination properties sensitive to the orientation of surrounding plies. In this study, we use an edge effect mitigator to better isolate the role of the coupling effect that mainly originates from interactions among transverse cracking, local delamination, and fiber bridging. Three samples (i.e., 90//90, 60//60, and 30//30) with and without the edge effect mitigator are evaluated by utilizing the double cantilever beam (DCB) test in the mode I fracture. A baseline unidirectional (UD) DCB test is performed for comparison. The experimental results reveal that for all orientations, the edge effect mitigator confines the delamination crack at the designed interface by limiting the formation of a large fiber bridging zone, thus allowing a more objective evaluation of the delamination properties. However, local crack branching or migration is observed in addition to the primary crack, which is responsible for the fiber orientation-dependent extra dissipation. According to the X-ray scan images obtained in the crack tip, a higher mismatch angle between the fiber orientation and the delamination direction is responsible for the stronger local coupling. The samples without a mitigator illustrate the effect of a fully developed fiber bridging on the apparent toughness in the mode I fracture behavior. The edge effect mitigator demonstrates its potential in a more precise identification of interfacial properties. ; The research reported in this publication was supported by funding from King Abdullah University of Science and Technology (KAUST) Baseline Research Funds, under award number BAS/1/1315-01-01.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Ultrasonics and Acoustic Wave Propagation · Smart Materials for Construction

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

References (40)

Show source-provided references
1. The role of delamination in failure of fibre-reinforced composites
2. Experimental study on delamination migration in multidirectional laminates under mode II static and fatigue loading, with comparison to mode I10.1016/j.compstruct.2018.06.081 ↗
3. A numerical and experimental investigation of delamination behaviour in the DCB specimen10.1016/S0266-3538(99)00113-X ↗
4. On the determination of delamination toughness by using multidirectional DCB specimens10.1016/j.polymertesting.2010.04.007 ↗
5. Delamination propagation criterion including the effect of fiber bridging for mixed-mode I/II delamination in CFRP multidirectional laminates10.1016/j.compscitech.2017.09.002 ↗
6. Influence of interface ply orientation on delamination growth in composite laminates10.1177/00219983211031636 ↗
7. 2013
8. 2014
9. 2013
10. A fractographic analysis of delamination within multidirectional carbon/epoxy laminates10.1016/0266-3538(95)00099-2 ↗
11. Influence of curved delamination front on toughness of multidirectional DCB specimens10.1016/j.compstruct.2011.11.035 ↗
12. Simulation of delamination growth in multidirectional laminates under mode I and mixed mode I/II loadings using cohesive elements10.1016/j.compstruct.2014.05.042 ↗
13. An experimental study on the influence of intralaminar damage on interlaminar delamination properties of laminated composites10.1016/j.compositesa.2020.105783 ↗
14. Experimental study on delamination migration in composite laminates10.1016/j.compositesa.2015.02.018 ↗
15. The relationship between mixed-mode II/III delamination and delamination migration in composite laminates10.1016/j.compscitech.2014.10.001 ↗
16. 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 ↗
17. Delamination fracture of multidirectional carbon-fiber/epoxy composites under mode I, mode II and mixed-mode I/II loading10.1177/002199839903300105 ↗
18. Delamination migration in multidirectional composite laminates under mode I quasi-static and fatigue loading10.1016/j.compstruct.2018.01.074 ↗
19. Large-scale bridging in composites: R-curves and bridging laws10.1016/S1359-835X(98)00025-6 ↗
20. Simulation of mode I delamination propagation in multidirectional composites with R-curve effects using VCCT method10.1016/j.commatsci.2012.06.025 ↗
21. Influence of intralaminar cracking on the apparent interlaminar mode I fracture toughness of cross-ply laminates10.1111/j.1460-2695.2004.00739.x ↗
22. Experimental study of the influence of ply orientation on DCB mode-I delamination behavior by using multidirectional fully isotropic carbon/epoxy laminates10.1016/j.compstruct.2016.11.036 ↗
23. An interface-dependent model of plateau fracture toughness in multidirectional CFRP laminates under mode I loading10.1016/j.compositesb.2017.07.077 ↗
24. Mixed-mode fracture response of anti-symmetric laminates: experiments and modelling10.1016/j.compositesb.2020.108089 ↗
25. Finite element modeling of mode I delamination growth in laminated DCB specimens with R-curve effects10.1016/j.compositesb.2012.09.051 ↗
26. A damage model for the simulation of delamination in advanced composites under variable-mode loading10.1016/j.mechmat.2005.10.003 ↗
27. Accurate simulation of delamination growth under mixed-mode loading using cohesive elements: Definition of interlaminar strengths and elastic stiffness10.1016/j.compstruct.2010.01.012 ↗
28. Modelling delamination migration in angle-ply laminates10.1016/j.compscitech.2017.02.010 ↗
29. A discrete crack informed 3d continuum damage model and its application for delamination migration in composite laminates10.1016/j.compositesb.2019.02.045 ↗
30. Numerical investigation to prevent crack jumping in Double Cantilever Beam tests of multidirectional composite laminates10.1016/j.compscitech.2011.07.002 ↗
31. Characterization of crack propagation in mode I delamination of multidirectional CFRP laminates10.1016/j.compscitech.2012.04.011 ↗
32. Additive binding layers to suppress free edge delamination in composite laminates under tension10.1016/j.compositesa.2022.106902 ↗
33. Delamination of multidirectional composite laminates at 0°/θ° ply interfaces10.1016/j.engfracmech.2006.05.013 ↗
34. A modified DCB specimen for mode I testing of multidirectional laminates10.1177/002199839202601101 ↗
35. Influence of curing processes on the development of fiber bridging during delamination in composite laminates10.1016/j.compositesa.2021.106564 ↗
36. How the spatial correlation in adhesion properties influences the performance of secondary bonding of laminated composites
37. How variability in interfacial properties results in tougher bonded composite joints by triggering bridging
38. Laser-based interfacial patterning enables toughening of CFRP/epoxy joints through bridging of adhesive ligaments10.1016/j.compositesa.2020.106094 ↗
39. On controlling interfacial heterogeneity to trigger bridging in secondary bonded composite joints: an efficient strategy to introduce crack-arrest features10.1016/j.compscitech.2019.107964 ↗
40. Point-wise evaluation of the growth driving direction for arbitrarily shaped delamination fronts using cohesive elements10.1016/j.euromechsol.2018.05.006 ↗