Bearing failure analysis of mechanically fastened joints in composite laminates

An experimental investigation was performed to study the effects of stacking sequence and clamping force on delamination bearing strengths of mechanically fastened joints in carbon/epoxy composite laminates using acoustic emission (AE) technique. The experimental work of the study was presented in [H.J. Park, Effects of stacking sequence and clamping force on the bearing strengths of mechanically fastened joints in composite laminates, Compos. Struct., submitted], and this paper summarizes the analytical work. The major focus of the analytical work was to develop an effective methodology for assessing the delamination bearing strength of joints in finite composite laminates in conjunction with an accurate three-dimensional contact stress analysis via an efficient quasi-three-dimensional finite element procedure based on layerwise theory. The contact phenomena and stress distribution in the vicinity of joints in composite laminates are investigated in detail. The delamination bearing failure strengths of mechanically fastened joints in composite laminates are predicted using modified Ye-delamination failure criterion based on layerwise finite element contact stress analysis. The effects of stacking sequence and clamping pressure are considered. The accuracy and applicability of the proposed methodology are confirmed by comparisons to the referenced experimental data and previous investigations.

[1]  Fu-Kuo Chang,et al.  The Effect of Pin Load Distribution on the Strength of Pin Loaded Holes in Laminated Composites , 1986 .

[2]  Pd Mangalgiri Pin-Loaded Holes in Large Orthotropic Plates , 1984 .

[3]  F. L. Matthews Joining fibre-reinforced plastics , 1987 .

[4]  I. H. Marshall,et al.  Observations on bolted connections in composite structures , 1989 .

[5]  Je Hoon Oh,et al.  Optimum bolted joints for hybrid composite materials , 1997 .

[6]  Robert E. Rowlands,et al.  Finite element analysis of multiple-bolted joints in orthotropic plates , 1993 .

[7]  Jaroslav Mackerle,et al.  Contact-Impact Problems: A Review With Bibliography , 1994 .

[8]  Michael R Wisnom,et al.  A novel finite element investigation of the effects of washer friction in composite plates with bolt-filled holes , 1994 .

[9]  L. Ingvar Eriksson,et al.  Contact stresses in bolted joints of composite laminates , 1986 .

[10]  B. L. Agarwal Static Strength Prediction of Bolted Joint in Composite Material , 1980 .

[11]  Richard A. Scott,et al.  Strength of Mechanically Fastened Composite Joints , 1982 .

[12]  Wen-Hwa Chen,et al.  Three-dimensional contact stress analysis of a composite laminate with bolted joint , 1995 .

[13]  W. J. Quinn,et al.  The Effect of Stacking Sequence on the Pin-Bearing Strength in Glass Fibre Reinforced Plastic , 1977 .

[14]  D. W. Wilson,et al.  Analysis of the Net Tension Failure Mode in Composite Bolted Joints , 1982 .

[15]  Z. Zhong Finite Element Procedures for Contact-Impact Problems , 1993 .

[16]  Hiroyuki Hamada,et al.  Strength Prediction of Mechanically Fastened Quasi-Isotropic Carbon/Epoxy Joints , 1996 .

[17]  Ran Y. Kim,et al.  Experimental and Analytical Studies On the Onset of Delamination in Laminated Composites , 1984 .

[18]  Hiroyuki Hamada,et al.  Effects of Stacking Sequences on Mechanically Fastened Joint Strength in Quasi-Isotropic Carbon-Epoxy Laminates , 1995 .

[19]  Heung-Joon Park,et al.  Effects of stacking sequence and clamping force on the bearing strengths of mechanically fastened joints in composite laminates , 2001 .

[20]  M.Y. Tsai,et al.  Stress and Failure Analysis of a Pin-Loaded Composite Plate: An Experimental Study , 1990 .

[21]  F. L. Matthews,et al.  A Finite Element Analysis of Single and Two-Hole Bolted Joints in Fibre Reinforced Plastic , 1981 .

[22]  John H. Crews,et al.  Stress analysis method for a clearance-fit bolt under bearing loads , 1986 .

[23]  John C. Brewer,et al.  Quadratic Stress Criterion for Initiation of Delamination , 1988 .

[24]  J. N. Reddy,et al.  Modelling of thick composites using a layerwise laminate theory , 1993 .

[25]  Richard A. Scott,et al.  Failure of Composite Laminates Containing Pin Loaded Holes—Method of Solution , 1984 .

[26]  Fu-Kuo Chang,et al.  Bearing Failure of Bolted Composite Joints. Part I: Experimental Characterization , 1996 .

[27]  Robert E. Rowlands,et al.  Single- and multiple-bolted joints in orthotropic materials , 1982 .

[28]  Ramamurthy Prabhakaran Photoelastic investigation of bolted joints in composites , 1982 .

[29]  Fu-Kuo Chang,et al.  Bearing Failure of Bolted Composite Joints. Part II: Model and Verification , 1996 .

[30]  Byung Man Kwak,et al.  Contact analysis of mechanically fastened joints in composite laminates by linear complementarity problem formulation , 1997 .

[31]  Army Materials,et al.  Fibrous composites in structural design , 1980 .

[32]  N. J. Pagano,et al.  The Influence of Stacking Sequence on Laminate Strength , 1971 .

[33]  Wen-Hwa Chen,et al.  Numerical and Experimental Failure Analysis of Composite Laminates with Bolted Joints under Bending Loads , 1995 .

[34]  Chien-Chang Lin,et al.  Stress and strength analysis of composite joints using direct boundary element method , 1993 .