journal article·2016-09

A novel interpretation of fatigue delamination growth behavior in CFRP multidirectional laminates

Libin Zhao, Yu Gong, Jianyu Zhang, Yana Wang, Zizi Lu, Lei Peng, Ning Hu

Publisher page

Abstract

Abstract Two Paris-type models are proposed to characterize the fatigue delamination growth (FDG) behavior in CFRP laminates. The crack-driving forces denoted by two definitions of the strain energy release rate (SERR) range against the fatigue delamination resistance of composite materials are introduced to control the FDG. The first definition is the square of the difference between the square root of maximum SERR and that of minimum SERR. The second one is the arithmetic difference between the maximum and minimum SERR. A series of fatigue delamination tests of CFRP multidirectional laminates under various stress ratios and mode-mixity ratios were carried out. Among different Paris relations, the FDG rate corrected by the first model exhibits a linear relationship with R -ratio dependency, and the second model further removes the R -ratio dependence, under different mode-mixity ratios, on a log-log scale. The experimental results indicate that the presented models can provide more generic descriptions and a proper interpretation of the FDG behavior in CFRP multidirectional laminates.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Behavior of Reinforced Concrete · Fatigue and fracture mechanics

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

References (45)

Show source-provided references
1. Growth of internal delaminations under cyclic compression in composite plates10.1016/0022-5096(95)00012-8 ↗
2. In-situ SEM study of transverse cracking and delamination in laminated composite materials10.1016/j.compscitech.2014.10.012 ↗
3. The relationship between mixed-mode II/III delamination and delamination migration in composite laminates10.1016/j.compscitech.2014.10.001 ↗
4. 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 ↗
5. Finite element simulation of delamination growth in composite materials using LS-DYNA10.1016/j.compscitech.2009.01.036 ↗
6. Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates10.1016/j.ijfatigue.2003.10.016 ↗
7. Crack closure and fibre bridging during delamination growth in carbon fibre/epoxy laminates under mode I fatigue loading10.1016/j.compositesa.2014.08.028 ↗
8. Mixed-mode delamination growth in carbon-fibre composite laminates under cyclic loading10.1016/j.ijsolstr.2004.02.040 ↗
9. Delamination growth in composites under cyclic loads10.1177/002199839402800803 ↗
10. Mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites under fatigue loading10.1016/S0266-3538(97)00021-3 ↗
11. Simulation of fatigue delamination growth in composites with different mode mixtures10.1177/0021998307075439 ↗
12. Misinterpreting the results: how similitude can improve our understanding of fatigue delamination growth10.1016/j.compscitech.2010.11.010 ↗
13. Effect of stress ratio on near-threshold propagation of delimination fatigue cracks in unidirectional CFRP10.1016/0266-3538(87)90076-5 ↗
14. Application of the energy release rate approach for delamination growth in Glare10.1016/j.engfracmech.2005.10.006 ↗
15. Application of the Hartman-Schijve equation to represent Mode I and Mode II fatigue delamination growth in composites10.1016/j.compstruct.2011.11.030 ↗
16. Bridging effect on mode I fatigue delamination behavior in composite laminates10.1016/j.compositesa.2014.04.007 ↗
17. Delamination crack growth in composite laminates
18. A new semi-empirical model for stress ratio effect on mode II fatigue delamination growth10.1016/j.compositesa.2011.02.013 ↗
19. Mixed-mode delamination growth in carbon-fibre composite laminates under cyclic loading10.1016/j.ijsolstr.2004.02.040 ↗
20. Characterization of mode I and mixed-mode delamination growth in T300/5208 graphite/epoxy
21. Predicting interlaminar fatigue crack growth rates in compressively loaded laminates
22. A non-linear damage evolution model for mode II fatigue delamination onset and growth10.1016/j.ijfatigue.2012.03.016 ↗
23. Crack growth resistance curves in strain-softening materials10.1016/0022-5096(86)90039-6 ↗
24. A total fatigue life model for mode I delaminated composite laminates10.1016/j.ijfatigue.2005.04.006 ↗
25. A comparison of total fatigue life models for composite laminates10.1111/j.1460-2695.2006.00958.x ↗
26. Evaluation of delamination growth characterization methods under mode I fatigue loading
27. Discussion on the use of the strain energy release rate for fatigue delamination characterization10.1016/j.compositesa.2014.06.018 ↗
28. Mode I delamination growth of multidirectional composite laminates under fatigue loading10.1177/0021998310385029 ↗
29. Fatigue delamination growth rates and thresholds of composite laminates under mixed mode loading10.1016/j.ijfatigue.2012.01.008 ↗
30. Mixed mode delamination growth of multidirectional composite laminates under fatigue loading10.1016/j.engfracmech.2012.09.033 ↗
31. Methods for the prediction of fatigue delamination growth in composites and adhesive bonds-A critical review10.1016/j.engfracmech.2013.10.003 ↗
32. Loading variable effects on mode-I fatigue of wood-FRP composite bonded interface10.1016/S0266-3538(03)00231-8 ↗
33. Fatigue threshold and crack growth rate of adhesively bonded joints as a function of load/displacement ratio10.1016/j.compositesa.2013.11.001 ↗
34. Study of load ratio for mode-I fatigue fracture of wood-FRP-bonded interfaces10.1177/0021998304042083 ↗
35. Delamination growth behavior of a fabric reinforced laminated composite under mode I fatigue10.1115/1.2812390 ↗
36. Two-parameter model for delamination growth under mode I fatigue loading (Part A: experimental study)10.1016/j.compositesa.2014.06.007 ↗
37. Standard test method for mixed mode I-mode II interlaminar fracture toughness of unidirectional fiber reinforced polymer matrix composites
38. Mixed-mode bending method for delamination testing10.2514/3.25204 ↗
39. Reeder · 1991
40. New load introduction concept for improved and simplified delamination beam testing10.1111/j.1747-1567.1998.tb00582.x ↗
41. Bridging tractions in mode I delamination: measurements and simulations10.1016/j.compscitech.2007.08.024 ↗
42. Stress ratio effect on cyclic debonding in adhesively bonded composite joints10.1016/0263-8223(87)90014-6 ↗
43. The mixed-mode delamination of fibre composite materials10.1016/0266-3538(93)90031-B ↗
44. End corrections for orthotropic DCB specimens10.1016/0266-3538(89)90058-4 ↗
45. Corrections needed in double-cantilever beam tests for assessing the interlaminar failure of fibre-composites10.1007/BF00730701 ↗