Analysis on tensile properties and influence factors of composite hybrid joints

[1] Kelly G.Load transfer in hybrid (bonded/bolted) composite single-lap joints [J].Composite Structures,2005,69(1):35-43 [2] Gomez S,Onoro J,Pecharroman J.A simple mechanical model of a structural hybrid adhesive/riveted single lap joint [J].International Journal of Adhesion & Adhesives,2007,27(4):263-267 [3] Barut A,Madenci E.Analysis of bolted-bonded composite single-lap joints under combined in-plane and transverse loading [J].Composite Structures,2009,88(4):579-594 [4] Sadowski T,Knec M,Golewski P.Experimental investigations and numerical modeling of steel adhesive joints reinforced by rivets [J].International Journal of Adhesion & Adhesives,2010,30(5):338-346 [5] Ding K,Dhanasekar M.Flexural behavior of bonded-bolted butt joints due to bolt looseness [J].Advances in Engineering Software,2007,38(8-9):598-606 [6] Ryosuke M,Motoko S,Akira T.Improving performance of GFRP/aluminum single lap joints using bolted/co-cured hybrid method [J].Composites:Part A,2008,39(2):154-163 [7] Fu M F,Mallick P K.Fatigue of hybrid (adhesive/bolted) joints in SRIM composites [J].International Journal of Adhesion & Adhesives,2001,21(2):145-159 [8] Hoang-Ngoc C T,Paroissien E.Simulation of single-lap bonded and hybrid (bolted/bonded) joints with flexible adhesive [J].International Journal of Adhesion & Adhesives,2010,30(3):117-129 [9] Kweon J H,Jung J W,Kim T H,et al.Failure of carbon composite-to-aluminum joints with combined mechanical fastening and adhesive bonding [J].Composite Structures,2006,75(1/2/3/4):192-198 [10] 程小全,汪源龙,张纪奎,等.平面编织复合材料胶螺混合连接接头拉伸性能分析[J].固体力学学报,2011,32(4):346-352 Cheng Xiaoquan,Wang Yuanlong,Zhang Jikui,et al.Tensile performance analysisi of combined adhesive and bolted joints for plain woven composites [J].Chinese Journal of Solid Mechanics,2011,32(4):346-352(in Chinese) [11] 陈浩然,息志臣.复合材料机械连接件非线性接触应力分析[J].航空学报,1990,11(7):410-414 Chen Haoran,Xi Zhichen. Nonlinear contact stress analysis of composite bolted joints [J].Acta Aeronautica et Astronautica Sinica,1990,11(7):410-414(in Chinese) [12] 陈浩然,息志臣.具有销钉承载孔的复合材料层合板的接触应力分析 [J].航空学报,1990,11(8):379-382 Chen Haoran,Xi Zhichen.Contact stress analysis of composite laminate with pin-loaded holes [J].Acta Aeronautica et Astronautica Sinica,1990,11(8):379-382(in Chinese) [13] Tserpes K I,Papanikos P,Labeas G,et al.Fatigue damage accumulation and residual strength assessment of CFRP laminates [J].Composite Structures,2004,63(2):219-230 [14] Papanikos P,Tserpes K I,Labeas G,et al.Progressive damage modeling of bonded composite repairs [J].Theoretical and Applied Fracture Mechanics,2005,43(2):189-198 [15] Yi X,Takashi I.Bearing strength and failure behavior of bolted composite joints (part II:modeling and simulation) [J].Composites Science and Technology,2005,65(7/8):1032-1043 [16] Kallmeyer A R,Stephens R I.Finite element model for predicting time-dependent deformations and damage accumulation in laminated composite bolted joints [J].Journal of Composite Materials,1999,33(9):794-826 [17] Reifsnider K,Case S.The mechanics of composite strength evolution [J].Composite Science and Technology,2000,60(12/13):2539-2546 [18] Kim Y M,Hong C S.Progressive failure model for the analysis of laminated composites based on finite element approach [J].Journal of Reinforced Plastics and Composites,1992,11(10):1078-1092 [19] Chang F K,Springer G S.Strengths of fiber reinforced composite bends [J].Journal of Composite Materials,1986,20(1):30-45 [20] Tserpes K I,Labeas G.Strength prediction of bolted joints in graphite/epoxy composite laminates [J].Composite Part B:Engineering,2002,33(7):521-529 [21] Tserpes K I,Papanikos P,Kermanidis T.A three-dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading [J].Fatigue and Fracture of Engineering Materials and Structures,2002,24(10):673-686 [22] Riccio A,Scaramuzzino F.Embedded delamination growth in composite panels under compressive load [J].Composites:Part B,2001,32(3):209-218