[1] ZHAO Y Q, JIANG F, HUANG Z M, et al. Micromechanical progressive damage analysis of inter-and intra-layer failures in fiber-reinforced composite laminates[J]. Journal of Composite Materials, 2020, 0021998319900300. [2] 梁珩, 王玉青, 童明波. C/C机织复合材料开孔板强度有限元模拟[J]. 航空工程进展, 2019, 10(1): 53-61. [3] BHATTACHARYYA R, BASU P K. Multiscale progressive damage analysis of CFRP composites using a mechanics based constitutive relation[J]. Composite Structures, 2020, 235: 111759. [4] 田志强, 李彦斌, 张培伟, 等. 复合材料层合板多尺度交互渐进损伤分析[J]. 工程力学, 2019, 36(12): 247-256. [5] CUI X, LUA J. Discrete crack informed continuum damage mechanics model in composite laminates[C]//AIAA Scitech 2020 Forum. 2020: 0252. [6] 许良, 何懿, 马少华, 等. 含孔复合材料层合板拉伸失效分析[J]. 科学技术与工程, 2018, 18(34): 242-247. [7] 李汝鹏, 陈磊, 刘学术, 等. 基于渐进损伤理论的复合材料开孔拉伸失效分析[J]. 航空材料学报, 2018, 38(5): 142-150. [8] ZHANG D, ZHENG X, WU T. Damage characteristics of open-hole laminated composites subjected to longitudinal loads[J]. Composite Structures, 2019, 230: 111474. [9] 拓宏亮, 马晓平, 卢智先. 含中心圆孔复合材料层合板失效分析及强度预测研究[J]. 航空工程进展, 2018, 9(2): 259-266. [10] BARTAN B, ACAR B, KAYRAN A. Three-dimensional delamination analysis in composite open hole tensile specimens with cohesive zone method[C]//57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. 2016: 0980. [11] LIU P F, GU Z P, PENG X Q, et al. Finite element analysis of the influence of cohesive law parameters on the multiple delamination behaviors of composites under compression[J]. Composite Structures, 2015, 131: 975-986. [12] 钱若力, 许诺, 王轩, 等. 考虑就位效应的大开口层合板拉伸失效预测[J]. 兵器材料科学与工程, 2020, 43(2): 103-108. [13] 刘向民, 姚卫星, 陈方. 复合材料层合板结构冲击损伤数值模拟的损伤力学模型[J]. 航空学报, 2016, 37(10): 3054-3063. [14] 杨凤祥, 陈静芬, 陈善富, 等. 基于剪切非线性三维损伤本构模型的复合材料层合板失效强度预测[J/OL]. 复合材料学报, 1-16[2020-05-19].https://doi.org/10.13801/j.cnki.fhclxb.20200110.002. [15] WANG G, JIA P, HUANG T. Numerical modeling of shear nonlinearity and failure analysis for composite laminates[J]. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2019, 233(18): 6616-6625. [16] RAIMONDO L, IANNUCCI L, ROBINSON P, et al. A progressive failure model for mesh-size-independent FE analysis of composite laminates subject to low-velocity impact damage[J]. Composites Science and Technology, 2012, 72(5): 624-632. [17] PUCK A, KOPP J, KNOPS M. Guidelines for the determination of the parameters in Puck′s action plane strength criterion[J]. Composites ence and Technology, 2002, 62(3): 371-378. [18] 李念. 复合材料加筋板边缘冲击损伤及冲击后压缩失效机理分析[D]. 南京: 南京航空航天大学, 2016. [19] DAVILA C G, CAMANHO P P, ROSE C A. Failure criteria for FRP laminates[J]. Journal of Composite materials, 2005, 39(4): 323-345. [20] CHANG F K, LESSARD L B. Damage tolerance of laminated composites containing an open hole and subjected to compressive loadings: Part I-Analysis[J]. Journal of composite materials, 1991, 25(1): 2-43. |