College of Aerospace Engineering, Chongqing University, Chongqing 400044, P. R. China;Key Laboratory of Fundamental Science for National Defence of Aeronautical Digital Manufacturing Process, Shenyang Aerospace University, Shenyang 110136, P. R. China 在期刊界中查找 在百度中查找 在本站中查找
Accurate simulation of the delamination growth behavior in composite multidirectional laminates is important for the designs of composite structures. According to the failure mechanism of multidirectional laminates, a novel three-linear cohesive zone model has been established in our previous work, in order to include the influence of fiber bridging on the delamination growth behavior in simulation. Based on that, numerical researches on the critical parameters in the novel three-linear cohesive zone model are performed in this study using two-dimensional finite element method. A value scheme of the critical parameters suitable for the simulation on the delamination growth in composite multidirectional laminates is obtained. The simulated results using the value scheme have good agreements with the experimental results, validating its effectiveness in the novel three-linear cohesive zone model.
[1] Zhao L B, Gong Y, Qin T L, et al. Failure prediction of out-of-plane woven composite joints using cohesive element[J]. Composite Structures, 2013, 106:407-416.
[2] Shokrieh M M, Zeinedini A, Ghoreishi S M. On the mixed mode I/II delamination R-curve of E-glass/epoxy laminated composites[J]. Composite Structures, 2017, 171:19-31.
[3] Shahkhosravi N A, Yousefi J, Najafabadi M A, et al. Fatigue life reduction of GFRP composites due to delamination associated with the introduction of functional discontinuities[J]. Composites Part B:Engineering, 2019, 163:536-547.
[4] Falcó O, Ávila R L, Tijs B, et al. Modelling and simulation methodology for unidirectional composite laminates in a Virtual Test Lab framework[J]. Composite Structures, 2018, 190:137-159.
[5] Liu L L, Zhao Z H, Chen W, et al. An experimental investigation on high velocity impact behavior of hygrothermal aged CFRP composites[J]. Composite Structures, 2018, 204:645-657.
[6] Gong Y, Zhao L B, Zhang J Y, et al. A novel model for determining the fatigue delamination resistance in composite laminates from a viewpoint of energy[J]. Composites Science and Technology, 2018, 167:489-496.
[7] Zhao L B, Wang Y N, Zhang J Y, et al. XFEM-based model for simulating zigzag delamination growth in laminated composites under mode I loading[J]. Composite Structures, 2017, 160:1155-1162.
[8] Zhao L B, Gong Y, Zhang J Y, et al. A novel interpretation of fatigue delamination growth behavior in CFRP multidirectional laminates[J]. Composites Science and Technology, 2016; 133:79-88.
[9] Peng L, Zhang J Y, Zhao L B, et al. Mode I delamination growth of multidirectional composite laminates under fatigue loading[J]. Journal of Composite Materials, 2011, 45(10):1077-1090.
[10] Bin Mohamed Rehan M S, Rousseau J, Fontaine S, et al. Experimental study of the influence of ply orientation on DCB mode-I delamination behavior by using multidirectional fully isotropic carbon/epoxy laminates[J]. Composite Structures, 2017, 161:1-7.
[11] Adluru H K, Hoos K H, Larve E V, et al. Delamination initiation and migration modeling in clamped tapered laminated beam specimens under static loading[J]. Composites Part A:Applied Science and Manufacturing, 2019, 118:202-212.
[12] Zhao L B, Gong Y, Zhang J Y, et al. Simulation of delamination growth in multidirectional laminates under mode I and mixed mode I/II loadings using cohesive elements[J]. Composite Structures, 2014, 116:509-522.
[13] Gong Y, Zhao L B, Zhang J Y, et al. Delamination propagation criterion including the effect of fiber bridging for mixed-mode I/II delamination in CFRP multidirectional laminates[J]. Composites Science and Technology, 2017, 151:302-309.
[14] Gong Y, Zhang B, Hallett S R. Delamination migration in multidirectional composite laminates under mode I quasi-static and fatigue loading[J]. Composite Structures, 2018, 189:160-176.
[15] Gong Y, Zhang B, Mukhopadhyay S, et al. Experimental study on delamination migration in multidirectional laminates under mode II static and fatigue loading, with comparison to mode I[J]. Composite Structures, 2018, 201:683-698.
[16] Gong Y, Zhao L B, Zhang J Y, et al. An improved power law criterion for the delamination propagation with the effect of large-scale fiber bridging in composite multidirectional laminates[J]. Composite Structures, 2018, 184:961-968.
[17] Zhao L B, Wang Y N, Zhang J Y, et al. An interface-dependent model of plateau fracture toughness in multidirectional CFRP laminates under mode I loading[J]. Composites Part B:Engineering, 2017, 131:196-208.
[18] Gong Y, Zhang B, Zhao L B, et al. R-curve behaviour of the mixed-mode I/II delamination in carbon/epoxy laminates with unidirectional and multidirectional interfaces[J]. Composite Structures, 2019, 223:110949.
[19] Turon A, Dávila C G, Camanho P P, et al. An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models[J]. Engineering Fracture Mechanics, 2007, 74(10):1665-1682.
[20] Alfano G, Crisfield M A. Finite element interface models for the delamination analysis of laminated composites:mechanical and computational issues[J]. International Journal for Numerical Methods in Engineering, 2001, 50(7):1701-1736.
[21] Ye Q, Chen P H. Prediction of the cohesive strength for numerically simulating composite delamination via CZM-based FEM[J]. Composites Part B:Engineering, 2011, 42(5):1076-1083.