[1] THOPPUL S D, FINEGAN J, GIBSON R F. Mechanics of mechanically fastened joints in polymer–matrix composite structures—a review. Compos Sci Technol, 2009, 69(3): 301-329.
[2] KIM S Y, HE B, SHIM C S. An experimental and numerical study on the interference-fit pin installation process for cross-ply glass fiber reinforced plastics (GFRP). Composites Part B: Engineering, 2013, 54: 153-162.
[3] 蔡闻峰, 薛小平. 先进复合材料结构飞机机械连接技术现状及发展方向. 航空精密制造技术, 2010, 46(2):24-26.
[4] 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. Compos Sci Technol, 2002, 62(10-11):1415–1431.
[5] American Society for Testing and Materials. ASTM D 5961/D 5961M-13 Standard test method for bearing response of polymer matrix composite laminates. America: American Society for Testing and Materials, 2013.
[6] 石亦平,周玉蓉.ABAQUS 有限元分析实例详解.北京:机械工业出版社,2006.
[7] STOCCHI C, ROBINSON P, PINHO ST. A detailed finite element investigation of composite bolted joints with countersunk fasteners. Compos Part A-Appl S, 2013, 52:143-150.
[8] MCCARTHY C T, MCCARTHY M A, STANLEY W F, et al. Experiences with modeling friction in composite bolted joints. J Compos Mater,2005, 39(21):1881-1908.
[9] NIU M CY. 实用飞机复合材料结构设计与制造.程小全, 张纪奎,译.北京: 航空工业出版社, 2010.