[1] Mouritz A P. Review of z-pinned composite laminates [J]. Composites Part A: Applied Science and Manufacturing, 2007, 38(12): 2383-2397.
[2] Mouritz A P, Bannister M K, Falzon P J, et al. Review of applications for advanced three-dimensional fibre textile composites[J]. Composites Part A: Applied Science and Manufacturing, 1999, 30(12): 1445-1461.
[3] Tomashevskii V T, Shalygin V N, Romanov D A, et al. Transversal reinforcement of composite materials using ultrasonic vibrations[J]. Mechanics of Composite Materials, 1988, 23(6): 769-772.
[4] Sun X N, Zheng C L. Advances on modeling through-the-thickness reinforcement of laminated composite by z-pinning[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(6): 1194-1202 (in Chinese). 孙先念, 郑长良. 层合复合材料z-pinning增强技术的力学进展[J]. 航空学报, 2006, 27(6): 1194-1202.
[5] Freitas G, Magee C, Dardzinski P, et al. Fiber insertion process for improved damage tolerance in aircraft laminates[J]. Journal of Advanced Materials, 1994, 25(4): 36-43.
[6] Zheng X T, Li Z J, Yang F. Experimental investigation on the fracture toughness of Z-pins reinforced composite laminates[J]. Acta Materiae Compositae Sinica, 2010, 27(4): 180-188 (in Chinese). 郑锡涛, 李泽江, 杨帆. Z-pin增强复合材料层合板断裂韧性试验研究[J]. 复合材料学报, 2010, 27(4): 180-188.
[7] Sun X N, Liu S T. Effect of Z-pins distribution on mode I delamination toughness of Z-pinned laminated double cantilever beam specimens[J]. Acta Materiae Compositae Sinica, 2007, 24(3): 160-166 (in Chinese). 孙先念, 刘书田. Z-pins几何分布对其增强复合材料双悬臂梁Ⅰ型层间韧性的影响[J]. 复合材料学报, 2007, 24(3): 160-166.
[8] Cartié D D R, Troulis M, Partridge I K. Delamination of Z-pinned carbon fibre reinforced laminates[J]. Composites Science and Technology, 2006, 66(6): 855-861.
[9] Dai S C, Yan W, Liu H Y, et al. Experimental study on z-pin bridging law by pullout test[J]. Composites Science and Technology, 2004, 64(16): 2451-2457.
[10] Li Y, Xiao J, Tan Y G, et al. Study on compressive properties of X-cor sandwich structures[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(3): 557-561 (in Chinese). 李勇, 肖军, 谭永刚, 等. X-cor夹层结构压缩性能研究[J]. 航空学报, 2009, 30(3): 557-561.
[11] Hao J J, Zhang Z G, Zhang L, et al. Effects of Z-pin inserting parameters on X-Cor sandwich mechanical property[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(3): 763-768 (in Chinese). 郝继军, 张佐光, 张蕾, 等. Z-pin植入参数对X-Cor夹层复合材料力学性能的影响[J]. 航空学报, 2008, 29(3): 763-768.
[12] Huang T, Jiao G Q, Du L. Experimental study on X-cor reinforced foam core sandwich[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(6): 1542-1549 (in Chinese). 黄涛, 矫桂琼, 杜龙. X-cor增强泡沫夹层结构力学性能试验[J]. 航空学报, 2008, 29(6): 1542-1549.
[13] Koh T M, Isa M D, Chang P, et al. Improving the structural properties and damage tolerance of bonded composite joints using z-pins[J]. Journal of Composite Materials, 2012, 46(26): 3255-3265.
[14] Chang P, Mouritz A P, Cox B N. Elevated temperature properties of pinned composite lap joints[J]. Journal of Composite Materials, 2008, 42(8): 741-769.
[15] Nanayakkara A M, Feih S, Mouritz A P. Improving the fracture resistance of sandwich composite T-joints by z-pinning[J]. Composite Structures, 2013, 96(1): 207-215.
[16] Li C H, Yan Y. Modeling and analysis of z-pin reinforcing in through-thickness direction of composite T-joint[J]. Acta Materiae Compositae Sinica, 2010, 27(6): 152-157 (in Chinese). 李成虎, 燕瑛. Z-pin增强复合材料T型接头层间性能的建模与分析[J]. 复合材料学报, 2010, 27(6): 152-157.
[17] Dong X Y, Li Y, Zhang X Y, et al. Performance of polymer composite single lap joints reinforced by Z-pin[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(5): 1302-1310 (in Chinese). 董晓阳, 李勇, 张向阳, 等. Z-pin增强树脂基复合材料单搭接连接性能[J]. 航空学报, 2014, 35(5): 1302-1310.
[18] Wang X X, Chen L. Experimental study on pullout strength of Z-pins[J]. Journal of Materials Engineering, 2011, 11(1): 1-4 (in Chinese). 王晓旭, 陈利. Z-pin的拔出强度试验研究[J]. 材料工程, 2011, 11(1): 1-4.
[19] Vazquez J T, Castanié B, Barrau J J, et al. Multi-level analysis of low-cost Z-pinned composite joints: Part 1: Single Z-pin behavior[J]. Composites Part A: Applied Science and Manufacturing, 2011, 42(12): 2070-2081.
[20] Shang W. Research on the influence of Z-pin's curing degree on the properties of composites [D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012 (in Chinese). 尚伟. Z-pin固化度对复合材料力学性能影响的研究[D]. 南京:南京航空航天大学, 2012.
[21] Yue C Y, Looi H C. Factors which influence the reliability of the assessment of interfacial bonding in fibrous composites using the pull-out test[J]. International Journal of Adhesion and Adhesives, 2001, 21(4): 309-323.
[22] Chang P, Mouritz A P, Cox B N. Properties and failure mechanisms of z-pinned laminates in monotonic and cyclic tension[J]. Composites Part A: Applied Science and Manufacturing, 2006, 37(10): 1501-1513.
[23] Chang P, Mouritz A P, Cox B N. Flexural properties of z-pinned laminates[J]. Composites Part A: Applied Science and Manufacturing, 2007, 38(2): 244-251.
[24] Mouritz A P. Delamination properties of z-pinned composites in hot-wet environment[J]. Composites Part A: Applied Science and Manufacturing, 2013, 52(1): 134-142.
[25] Song M C, Sankar B V, Subhash G, et al. Analysis of mode I delamination Z-pinned composites using a non-dimensional analytical model[J]. Composites Part B: Engineering, 2012, 43(4): 1776-1784.
[26] Park Y B, Lee B H, Kweon J H, et al. The strength of composite bonded T-joints transversely reinforced by carbon pins[J]. Composite Structures, 2012, 94(2): 625-634.
[27] Sweeting R D, Thomson R S. The effect of thermal mismatch on Z-pinned laminated composite structures[J]. Composite Structures, 2004, 66(1-4): 189-195.
[28] Li C H, Yan Y, Wang P, et al. Study on compressive properties of Z-pinned laminates in RTD and hygrothermal environment[J]. Chinese Journal of Aeronautics, 2012, 25(1): 64-70.