Lawlor V P, McCarthy M A, Stanley W F. An experimental study of bolt-hole clearance effects in double-lap, multi-bolt composite joints [J]. Composite Structures, 2005, 71(2): 176-190.
[2]
谢鸣九. 复合材料多排螺接接头载荷分配的电测法 //李顺林. 全国第八届复合材料会议文集. 北京: 航空工业出版社, 1994: 641-645. Xie Mingjiu. Multi-row bolted composite joint load distribution electrical measuring method //Li Shunlin. Proceedings of the 8th National Conference on Composite Materials. Beijing: Aeronautical Industry Press, 1994: 641-645.
[3]
许陆文, 罗文琳, 陈 华. 复合材料等刚度多钉螺接载荷分配的实验研究 [J]. 南京航空学院学报, 1990, 22(3): 54-61. Xu Luwen, Luo Wenlin, Chen Hua. Experimental study on load sharing between multiple-bolted joints in composite laminates with equal stiffness [J]. Nanjing Aviation University Journal, 1990, 22(3): 54-61.
[4]
Stanley W F, McCarthy M A, Lawlor V P. Measurement of load distribute in multi-bolt, composite joints, in the presence of varying clearance [J]. Journal of Plastics, Rubber and Composites, 31(9): 412-418.
[5]
徐耀玲, 张振先. 多钉连接复合材料板钉传载荷的计算 [J]. 燕山大学学报, 2005, 29(2): 178-181. Xu Yaoling, Zhang Zhenxian. Pin-load computations for composite laminate joints with multi-fasteners [J]. Journal of Yanshan University, 2005, 29(2): 178-181.
[6]
蒋持平, 张 行. 多钉连接件传载荷计算的一个解析方法 [J]. 航空学报, 1994, 15(3): 310-317. Jiang Chiping, Zhang Xing. An analytical method of pin load computations for joints with multi-fasteners [J]. Acta Aeronautica et Astronautica Sinica, 1994, 15(3): 310-317.
[7]
杨 旭, 章怡宁, 许希武. 复合材料层板多钉机械连接强度计算方法 [J]. 飞机设计, 1999(3): 11-20. Yang Xu, Zhang Yining, Xu Xiwu. Strength analysis for multiple-row bolted joints in laminates [J]. Aircraft Design, 1999(3): 11-20.
[8]
Xiong Y, Bedair O K. Analytical and finite element modeling of riveted lap joints in aircraft structure [J]. AIAA Journal, 1999, 37(1): 93-99.
[9]
孙庚茂, 丁惠梁, 段世慧. 一种基于钉"超元"的复合材料机械连接钉载计算方法 [J]. 复合材料学报, 1998, 15(1): 116-120. Sun Gengmao, Ding Huiliang, Duan Shihui. Method of joint calculation for composite plate by super-element [J]. Acta Materiae Compositae Sinica, 1998, 15(1): 116-120.
[10]
Gray P J, McCarthy C T. A global bolted joint model for finite element analysis of load distributions in multi-bolt composite joints [J]. Composites Part B, 2010, 41(4): 317-325.
[11]
Madenci E, Shkarayev S, Sergeev B, et al. Analysis of composite laminates with multiple fasteners [J]. Solids and Structures, 1998, 15(35): 1793-1811.
[12]
McCarthy M A, McCarthy C T, Padhi G S. A simple method for determining the effects of bolt-hole clearance on load distribution in single-column multi-bolt composite joints [J]. Composite Structures, 2006, 73(1): 78-87.
[13]
中国航空研究院. 复合材料连接手册 [M]. 北京: 航空工业出版社, 1994. Chinese Aeronatatical Estabishment. Composite materials connection manual [M]. Beijing: Aviation Industry Press, 1994.
[14]
Starikov R, Sch?n J. Quasi-static behaviour of composite joints with protruding-head bolts [J]. Composite Structures, 2001, 51(4): 411-425.
[15]
Starikov R, Sch?n J. Quasi-static behaviour of composite joints with countersunk composite and metal fasteners [J]. Composite Part B, 2011, 32(5): 401-411.
[16]
Ekh J, Sch?n J. Load transfer in multirow, single shear, composite-to-aluminium lap joints [J]. Composites Science and Technology, 2006, 66(7/8): 875-885.
[17]
赵美英. 复合材料机械连接失效分析及强度影响因素研究 . 西安: 西北工业大学, 2006. Zhao Meiying. Failure analysis of composite mechanically fastened joints and study of effects on failure strength . Xi’an: Northwestern Polytechnical University, 2006.
[18]
张博平, 张开达. 层合板多钉机械连接载荷分配三维有限元分析 [J]. 机械科学与技术, 1998, 17(2): 235-236. Zhang Boping, Zhang Kaida. Three dimension finite element analysis for load distribution of multi fastener joints [J]. Mechanical Science and Technology, 1998, 17(2): 235-236.
[19]
刘兴科, 李亚智, 刘向东, 等. 金属和复合材料多钉连接钉载分配研究 [J]. 航空工程进展, 2011, 2(2): 193-197. Liu Xingke, Li Yazhi, Liu Xiangdong, et al. Study on load distribution of multiple-bolted metal to composite joints [J]. Advance in Aeronautical Science and Engineering, 2011, 2(2): 193-198.