[1] CHAKHERLOU T N, RAZAVI M J, AGHDAM A B, et al. An experimental investigation of the bolt clamping force and friction effect on the fatigue behavior of aluminum alloy 2024-T3 double shear lap joint[J]. Materials & Design, 2011, 32(8):4641-4649. [2] WU T, ZHANG K F, CHENG H, et al. Analytical modeling for stress distribution around interference fit holes on pinned composite plates under tensile load[J]. Composites Part B:Engineering, 2016,100(1):176-185. [3] MOHAMMADPOUR A, CHAKHERLOU T N. Numerical and experimental study of an interference fitted joint using a large deformation Chaboche type combined isotropic-Kinematic hardening law and mortar contact method[J]. International Journal of Mechanical Sciences, 2016, 106:297-318. [4] MIRZAJANZADEH M, CHAKHERLOU T N, VOGWELL J. The effect of interference-fit on fretting fatigue crack initiation and ΔK of a single pinned plate in 7075 Al-alloy[J]. Engineering Fracture Mechanics, 2011, 78(6):1233-1246. [5] CHAKHERLOU T N, TAGHIZADEH H, AGHDAM A B. Experimental and numerical comparison of cold expansion and interference fit methods in improving fatigue life of holed plate in double shear lap joints[J]. Aerospace Science and Technology, 2013, 29(1):351-362. [6] LIU J, WU H, YANG J, et al. Effect of edge distance ratio on residual stresses induced by cold expansion and fatigue life of TC4 plates[J]. Engineering Fracture Mechanics, 2013,109(3):130-137. [7] 左杨杰, 曹增强, 杨柳,等. 基于对称加载的均匀干涉配合铆接方法[J]. 航空学报, 2016, 37(3):1049-1059. ZUO Y J, CAO Z Q, YANG L, et al. Interference-fit evenness riveting method based on symmetrical loading[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3):1049-1059(in Chinese). [8] 姜杰凤, 董辉跃, 柯映林. 高锁螺栓干涉连接中极限干涉量[J]. 机械工程学报, 2013, 49(3):145-152. JIANG J F, DONG H Y, KE Y L. Maximum interference fit size of hi-lock bolted joints[J]. Chinese Journal of Mechanical Engineering, 2013, 49(3):145-152(in Chinese). [9] CHAKHERLOU T N, ABAZADEH B. Investigating clamping force variations in Al2024-T3 interference fitted bolted joints under static and cyclic loading[J]. Materials & Design, 2012, 37:128-136. [10] ABAZADEH B, CHAKHERLOU T N, ALDERLIESTEN R C. Effect of interference fitting and/or bolt clamping on the fatigue behavior of Al alloy 2024-T3 double shear lap joints in different cyclic load ranges[J]. International Journal of Mechanical Sciences, 2013, 72(7):2-12. [11] TIMOSHENKO S P. Strength of materials part Ⅱ:Advanced theory and problems[M].3rd ed. 1956:205-213. [12] HSU Y C, FORMAN R G. Elastic-plastic analysis of an infinite sheet having a circular hole under pressure[J]. Journal of Applied Mechanics, 1975, 42(2):347-352. [13] GUO W L. Elastic-plastic analysis of a finite sheet with a cold-worked hole[J]. Engineering fracture mechanics, 1993, 46(3):465-472. [14] 郭兰中, 朱琪, 邢文珍. 过盈压入强化预应力及其变化规律的研究[J]. 应用力学学报, 2002, 19(1):27-31. GUO L Z, ZHU Q, XING W Z. Prestressing of force-fit and its characters under load[J]. Chinese Journal of Applied Mechanics, 2002, 19(1):27-31(in Chinese). [15] KIM S Y, HE B, SHIM C S, et al. An experimental and numerical study on the interference-fit pin installation process for cross-ply glass fiber reinforced plastics (GFRP)[J]. Composites Part B:Engineering, 2013, 54:153-162. [16] LANCIOTTI A, POLESE C. The effect of interference-Fit fasteners on the fatigue life of central hole specimens[J]. Fatigue & Fracture of Engineering Materials & Structures, 2005, 28(7):587-597. [17] HAO D, WANG D. Finite-element modeling of the failure of interference-fit planet carrier and shaft assembly[J]. Engineering Failure Analysis, 2013, 33(7):184-196. [18] 张岐良, 曹增强, 甘学东, 等. 拉伸板中心孔干涉配合对载荷幅值的影响[J]. 航空学报, 2014, 35(6):1643-1650. ZHANG Q L, CAO Z Q, GAN X D, et al. Effect of interference-fit on load amplitude of a single central holed tensile plate[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6):1643-1650(in Chinese). [19] ZHANG Q L, CAO Z Q, WEI FY, et al. Mechanical analysis of a pin interference-fitted sheet under tensile loading[J]. Journal of Aerospace Engineering, 2016, 29(4):04015085. [20] 中国航空科学技术研究院. 飞机结构抗疲劳断裂强化设计手册[M]. 北京:航空工业出版社, 1993. Chinese Academy of Aviation Science and Technology. Handbook of aircraft structure anti-fatigue and anti-fracture strengthen technology[M]. Beijing:Aviation Industry Press, 1993(in Chinese). [21] BROWN M A, EVANS J L. Fatigue life variability due to variations in interference fit of steel bushings in 7075-T651 aluminum lugs[J]. International Journal of Fatigue, 2012, 44(9):177-187. [22] CHAKHERLOU T N, MIRZAJANZADEH M, VOGWELL J. Experimental and numerical investigations into the effect of an interference fit on the fatigue life of double shear lap joints[J]. Engineering Failure Analysis, 2009, 16(7):2066-2080. [23] CROCCOLO D, DE A M, CESCHINI L, et al. Interference fit effect on improving fatigue life of a holed single plate[J]. Fatigue & Fracture of Engineering Materials & Structures, 2013, 36(7):689-698. [24] 郝小忠, 王珉, 陈文亮. 自动钻铆最佳干涉量试验研究[J]. 航空制造技术, 2012(12):77-79. HAO X Z, WANG M, CHEN W L. Experimental research of best interference fit level on automatic drilling and riveting[J]. Aeronautical Manufacturing Technology, 2012(12):77-79(in Chinese). |