Abstract
Single lap bolted joints subjected to tensile load are essential joining methods in engineering design. Lateral displacement of the grip in single lap bolted joint experiment was examined and analyzed. This was different from early investigations that considered the joint fully gripped with no lateral degree of freedom. The lateral stiffness of the grip was tested to obtain the test machine properties. Tensile experiments on single lap composite-to-aluminum bolted joints were conducted, and the lateral displacement of the grip measured. Other measurements included tensile displacement, out-of-plane displacement, and surface strains. By allowing for lateral displacement, the novel finite element model predicted good results. The influence of lateral displacement of the grip was analyzed using the novel and traditional models. The novel model predicted 13 % smaller joint stiffness than traditional model. The parameters related to secondary bending were found different and the failure load of the joint was delayed because of lateral displacement of the grip.
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References
Cloud GL (2013) 2012 William M. Murray lecture: some curious unresolved problems, speculations, and advances in mechanical fastening. Exp Mech 53:1073–1104
Kapidžić Z, Nilsson L, Ansell H (2014) Finite element modeling of mechanically fastened composite-aluminum joints in aircraft structures. Compos Struct 109:198–210
Thoppul SD, Finegan J, Gibson RF (2009) Mechanics of mechanically fastened joints in polymer–matrix composite structures–a review. Compos Sci Technol 69(3):301–329
Okutan Baba B (2006) Behavior of Pin-loaded laminated composites. Exp Mech 46:589–600
McCarthy MA, Lawlor VP, Stanley WF, McCarthy CT (2002) Bolt-hole clearance effects and strength criteria in single bolt, single lap, composite joints. Compos Sci Technol 62(10–11):1415–1431
Khashaba UA, Sallam HEM, Al-Shorbagy AE (2006) Effect of washer size and tightening torque on the performance of bolted joints in composite structures. Compos Struct 73(3):310–317
Ireman T (1998) Three-dimensional stress analysis of bolted single-lap composite joints. Compos Struct 43(3):195–216
McCarthy MA, McCarthy CT, Lawlor VP et al (2005) Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints: part I—model development and validation. Compos Struct 71(2):140–158
Horn WJ, Schmitt RR (1994) Influence of clamp-up force on the strength of bolted composite joints. AIAA J 32(3):665–667
Xiao Y, Ishikawa T (2005) Bearing strength and failure behavior of bolted composite joints (part I: Experimental investigation). Compos Sci Technol 65(7):1022–1031
Yan Y, Wen WD, Chang FK et al (1999) Experimental study on clamping effects on the tensile strength of composite plates with a bolt-filled hole. Compos A: Appl Sci Manuf 30(10):1215–1229
Xiao Y, Ishikawa T (2005) Bearing strength and failure behavior of bolted composite joints (part II: modeling and simulation). Compos Sci Technol 65(7–8):1032–43
Dano ML, Gendron G, Picard A (2000) Stress and failure of mechanically fastened joints in composite laminates. Compos Struct 50(3):287–96
Olmedo Á, Santiuste C (2010) On the prediction of bolted single-lap composite joints. Compos Struct 94(6):2110–2117
Tserpes KI, Papanikos P, Kermanidis T (2001) A three-dimensional progressive damage model for bolted joints in composite laminates subjected to tensile loading. Fatigue Fract Eng Mater Struct 24(10):663–675
Hühne C, Zerbst A-K, Kuhlmann G, Steenbock C, Rolfes R (2010) Progressive damage analysis of composite bolted joints with liquid shim layers using constant and continuous degradation models. Compos Struct 92(2):189–200
Kim J, Yoon JC, Kang BS (2007) Finite element analysis and modeling of structure with bolted joints. Appl Math Model 31(5):895–911
Olmedo A, Santiuste C, Barbero E (2014) An analytical model for the secondary bending prediction in single-lap composite bolted-joints. Compos Struct 111:354–361
Atas A, Mohamed GF, Soutis C (2012) Effect of clamping force on the delamination onset and growth in bolted composite laminates. Compos Struct 94:548–552
Tong L (2000) Bearing failure of composite bolted joints with non-uniform bolt-to-washer clearance. Compos A: Appl Sci Manuf 31(6):609–615
Abaqus Analysis User’s Manual, Simulia; 2011. <www.simulia.com>
Schön J (2004) Coefficient of friction for aluminum in contact with a carbon fiber epoxy composite. Tribol Int 37(5):395–404
Cheng X, Li Z (2005) Damage progressive model of compression of composite laminates after low velocity impact. Adv Appl Math Mech 26(5):618–626
Chang FK, Lessard LB (1991) Damage tolerance of laminated composites containing an open hole and subject to compressive loadings: part I – Analysis. J Compos Mater 25(1):2–43
Reddy YS, Reddy JN (1993) Three-dimensional finite element progressive failure analysis of composite laminates under axial extension. J Compos Technol Res 15(2):73–87
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Wang, S.W., Cheng, X.Q., Guo, X. et al. Influence of Lateral Displacement of the Grip on Single lap Composite-to-Aluminum Bolted Joints. Exp Mech 56, 407–417 (2016). https://doi.org/10.1007/s11340-015-0110-5
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DOI: https://doi.org/10.1007/s11340-015-0110-5