[1] 李吻, 李勇, 还大军. 增强复合材料帽型加筋壁板接头拉伸性能. 航空学报, 2016, 37(6): 2003-2012.
[2] 叶金蕊, 张博明. 复合材料蒙皮加筋壁板结构成本-质量优化设计.复合材料学报, 2009, 26(2): 187-194.
[3] 段友社, 周晓芹, 侯军生, 等. 大飞机复合材料机翼研制技术现状. 航空制造技术, 2012(18): 34-37.
[4] 鞠苏, 曾竟成, 江大志, 等. 碳纤维增强复合材料接头研究进展. 高科技纤维与应用, 2006, 31(3): 29-35.
[5] 许巍, 陈力, 张钱城, 等. 粘结界面力学行为及其表征. 中国科学: 技术科学, 2012, 42(12): 1361-1376.
[6] Kim J K, Mackay D B, Mai Y W. Drop-weight impact damage tolerance of CFRP with rubbermodified epoxy matrix. Composites, 1993, 24(6): 485-494.
[7] Jang K, Cho W J, Ha C S. Influence of processing method on the fracture toughness of thermoplastic-modified carbon-fiber-reinforced epoxy composites. Composites Science & Technology, 1999, 59(7): 995-1001.
[8] Sjögren B A, Berglund L A. Toughening Mechanisms in rubber-modified glass fiber/unsaturated polyester composites. Polymer Composites, 1999, 20(20): 705-712.
[9] 潘杰, 文立伟, 肖军. 复合材料预制体单面双针缝合装备技术研究. 玻璃钢/复合材料, 2017(2): 76-81.
[10] 王芳芳, 张方超, 吴晓青. 缝合工艺对复合材料面内力学性能影响实验研究. 玻璃钢/复合材料, 2017(7): 35-39.
[11] 孔斌, 陈普会, 李梦佳, 等. Z-pin/缝合对复合材料T型接头剪切承载能力的影响. 复合材料学报, 2018, 35(4): 834-842.
[12] 李梦佳, 陈普会, 孔斌, 等. 缝合参数对复合材料 T型接头拉脱承载能力的影响. 复合材料学报, 2016, 33(3): 681-688.
[13] Emile G, Aaron L, Richard B, et al. Evaluation of toughening concepts at structural features in CFRP-Part Ⅰ: Stiffener pull-off. Composites Part Applied Science and Manufacturing, 2006, 37(10): 1521-1535.
[14] Kim C H, Jo D H, Choi J H. Failure strength of composite T-joints prepared using a new 1-thread stitching process. Composite Structures, 2017(178): 225-231.
[15] Kumari S, Sinha P K. Effects of transverse stitching and hygrothermal environment on composite wing T-joints. Reinf. Plast. Compos., 2003, 22: 1705-28.
[16] Glaessgen E H. Delamination and stitched failure in stitched composite joints: AIAA-1999-1247. Reston: AIAA, 1999.
[17] 谭彦. Z-pin增强复合材料T型加筋结构增强机理研究. 南京: 南京航空航天大学, 2017.
[18] 燕瑛, 韩凤宇, 杨东升, 等. 缝合复合材料弹性性能的三维有限元细观分析与试验验证. 航空学报, 2004, 25(3): 267-269.
[19] 邵会学. 复合材料T型接头损伤监测方法研究. 南京: 南京航空航天大学, 2015.
[20] Bigaud J, Aboura Z, Martins A T, et al. Analysis of the mechanical behavior of composite T-joint reinforced by one side stitching. Composite Structures, 2018(184): 249-255.
[21] Cox B N. Snubbing Effects in the pullout of a fibrous rod from a laminate. Mechanics of Advanced Materials & Structures, 2005, 12(2): 85-98.
[22] Koh T M. Improving the mechanical properies of aerospace carbon fibre-epoxy joints by Z-pinning. Melbourne: RMIT University, 2012.
[23] Koh T M, Isa M D, Feih S, et al. Experimental assessment of the damage tolerance of Z-pinned T-stiffened composite panels. Composites Part B Engineering, 2013, 44(1): 620-627.
[24] Cartié D D R, Cox B N, Fleck N A. Mechanisms of crack bridging by composite andmetallic rods. Composites Part A Applied Sience & Manufacturing, 2004, 35(11): 1325-1336 |