[1] Conti P. Influence of geometric parameters on the stress distribution around a pin-loaded hole in a composite laminate. Composite Science and Technology, 1986, 25(2): 1-19.[2] Naik R A, Crews J H. Stress analysis method for a clearance-fit bolt under bearing conditions. AIAA Journal, 1985, 24(3): 1348-1353.[3] Chen W H, Lee S, Yeh J T. Three-dimensional contact stress analysis of a composite laminate with bolted joint. Composite Structures, 1995, 30(3): 287-297.[4] Sun H T, Qing X, Chang F K. The response of composite joints with bolt-clamping loads, Part Ⅱ: model verification. Composite Material, 2002; 36(1): 69-91.[5] McCarthy M A, Lawlor V P, Stanley W F, et al. Bolt-hole clearance effects and strength criteria in single bolt, single lap, composite joints. Composite Science and Technology, 2002, 62(10-11): 1415-1431.[6] Xiao Y, Ishikawa T. Bearing strength and failure behavior of bolted composite joints, Part I: experimental investigation. Composites Science and Technology, 2005, 65(7-8): 1022-1031.[7] Liu P, Zhang K D. An experimental study on fatigue life of interference-fit composite joint. Acta Aeronautica et Astronautica Sinica, 1991, 12(12): 546-549. (in Chinese) 刘萍, 张开达. 干涉对复合材料叠层板螺栓连接疲劳强度的影响. 航空学报, 1991, 12(12): 546-549.[8] Zhang B P, Zhang K D. Fatigue of interference-fit mechanical joint in T300/QY8911 laminate. Acta Materiae Compositea Sinica, 1996, 13(1): 97-100. (in Chinese) 张博平, 张开达. T300/QY8911 π/4层压板机械连接干涉疲劳. 复合材料学报, 1996, 13(1): 97-100.[9] Chinese Aeronautical Establishment. Composite structures design manual. Beijing: Aviation Industry Press, 2001: 145-175. (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: 145-175.[10] Department of Defense. MIL-HDBK-17F Composite materials handbook: Volume 3, polymer matrix composite materials usage, design, and analysis. Philadelphia: Government Publication, 2002: 271-280.[11] Thoppul S D, Finegan J, Gibson R F. Mechanics of mechanically fastened joints in polymer-matrix composite structures—a review. Composites Science and Technology, 2009, 69(3-4): 301-329.[12] Hashin Z. Failure criteria for unidirectional fiber composites. Journal of Applied Mechanics, 1980, 47(2): 329-335.[13] Xiao Y, Ishikawa T. Bearing strength and failure behavior of bolted composite joints, Part Ⅱ: modeling and simulation. Composites Science and Technology, 2005, 65(7-8): 1032-1043.[14] Chang F K, Chang K Y. A progressive damage model for laminated composites containing stress concentrations. Journal of Composite Material, 1987, 21(9): 834-855.[15] Tan S C, Perez J. Progressive failure of laminated composites with a hole under compressive loading. Journal of Reinforced Plastic Composite, 1993, 18(10): 255-278.[16] Irisarri F X, Laurin F, Carrere N, et al. Progressive damage and failure of mechanically fastened joints in CFRP laminates, Part I: refined finite element modeling of single-fastener joints. Composite Structures, 2012, 94(8): 2269-2277.[17] ASTM D5961/D5961 M-05 Standard test method for bearing response of polymer matrix composite laminates. Philadelphia: American Society for Testing and Materials, 2005. |