[1] Ilcewicz L B, Smith P J, Horton R E. Advanced composite fuselage technology. N95-29034, 1995. [2] Ilcewicz L B, Smith P J, Hanson C T, et al. Advanced composite fuselage program overview. NASA CR-4734, 1997. [3] Gray P J, McCarthy C T. A global bolted joint model for finite element analysis of load distributions in multi-bolt composite joints. Composites: Part B, 2010, 41(4): 317-325. [4] Dano M L, Gendron G, Picard A. Stress and failure analysis of mechanically fastened joints in composite laminates. Composite Structures, 2000, 50(3): 287-296. [5] Jiang Y P, Yue Z F. Numerical failure simulation of bolt-loaded composite laminate. Acta Material Composite Sinica, 2005, 22(4): 177-182. (in Chinese) 姜云鹏, 岳珠峰. 复合材料层合板螺栓连接失效的数值模拟. 复合材料学报, 2005, 22(4): 177-182. [6] Zhao M Y, Yan G L, Gu Y L, et al. Design of computation methods of the load distribution in composite fastener group joints. Aeronautical Computing Technique, 2006, 36(3): 97-100. (in Chinese) 赵美英, 阎国良, 顾亦磊, 等. 复合材料层板钉群连接载荷分配计算方法研究. 航空计算技术, 2006, 36(3): 97-100. [7] Wang F, Zhao M Y, Wan X P. Analysis method on first crippling strength for multiple-bolted composite joints. Aeronautical Computing Technique, 2006, 36(2): 120-123. (in Chinese) 王芳, 赵美英, 万小朋. 多钉连接初始破坏强度的工程方法研究. 航空计算技术, 2006, 36(2): 120-123. [8] Sun G M, Ding H L, Duan S H. Method of joint calculation for composite plate by super-element. Acta Material Composite Sinica, 1998, 15(1): 116-120. (in Chinese) 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. 复合材料学报, 1998, 15(1): 116-120. [9] ABAQUS/standard user’s manual: Version 6.10. Rhode Island, USA: Hibbit, Karlsson and Sorensen Inc., 2010. [10] Sun Y P. Research on the joint technologies of composite/metal mixed structures. Nanjing: College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, 2011. (in Chinese) 孙彦鹏. 复合材料/金属混合夹层结构干涉连接技术研究. 南京: 南京航空航天大学航空宇航学院, 2011. [11] Niu C Y. Airframe structural design. Beijing: Aviation Industry Press, 2008: 83-84. (in Chinese) 牛春匀. 实用飞机结构工程设计. 北京: 航空工业出版社, 2008: 83-84. [12] Institute of Aeronautics China. Handbook of composite structure design. Beijing: Aviation Industry Press, 2001: 149-150. (in Chinese) 中国航空研究院. 复合材料结构设计手册. 北京: 航空工业出版社, 2001: 149-150. [13] Zhao M Y. Failure analysis of composite mechanically fastened joints and study of effect on failure strength. Xi’an: School of Aeronautics, Northwestern Polytechnical University, 2006. (in Chinese) 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: 西北工业大学航空学院, 2006. [14] Chen X M. Application of contact technology based on user defined cohesive element in the strength analysis of composite fastened joint. Xi’an: Aircraft Strength Research Institute of China, 2011. (in Chinese) 陈向明. 自定义粘接元接触技术及其在复合材料连接强度分析中的应用. 西安: 中国飞机强度研究所, 2011. [15] Hashin Z. Failure criteria for unidirectional fiber composites. Journal of Applied Mechanics, 1980, 47(2): 329-335. [16] Maimi P, Camanho P P, Mayugo J A, et al. A continuum damage model for composite laminatesⅠ: constitutive model. Mechanics of Materials, 2007, 39(10): 897-908. [17] Lapczyk I, Hurtado J A. Progressive damage modeling in fiber-reinforced materials. Composites Part A: Applied Science and Manufacturing, 2007, 38(11): 2333-2341. |