Influence of debonding on the efficiency of crack patching

A simplified analysis of crack patching is presented in which the restraining effect of the external bonded reinforcement on the crack opening is simulated by distributed springs acting between the crack faces. It is suggested that elastic-perfectly plastic springs provide an adequate idealization for the case where debonding can occur. The analysis is thereby reduced to the solution of a one-dimensional integral equation involving only two material parameters: a spring constant k and a limit stress σL, both of which can be determined from the behaviour of a suitable overlap joint. The efficiency of the reinforcement is shown to be determined by the normalized crack length ka and the normalized stress σ/σL, so that a comprehensive characterization can be obtained from relatively little computation or experimental study.

[1]  L. R. F. Rose,et al.  Theoretical analysis of crack patching , 1988 .

[2]  F. Erdogan,et al.  A sandwich plate with a part-through and a debonding crack. , 1972 .

[3]  Rhys Jones,et al.  Finite Element Analysis of Patched Cracks , 1979 .

[4]  Leon M Keer,et al.  FRACTURE ANALYSIS OF ADHESIVELY BONDED SHEETS. , 1976 .

[5]  Rhys Jones,et al.  Neutral axis offset effects due to crack patching , 1983 .

[6]  L. Rose A cracked plate repaired by bonded reinforcements , 1982 .

[7]  R. Marissen,et al.  Flight simulation behaviour of aramid reinforced aluminium laminates (ARALL) , 1984 .

[8]  Rhys Jones,et al.  Analysis of composite laminates and fibre composite repair schemes , 1981 .

[9]  Richard A. Mitchell,et al.  Analysis of Composite-Reinforced Cutouts and Cracks , 1974 .

[10]  R. J. Callinan,et al.  Crack Patching: Analysis and Design , 1982 .

[11]  Rhys Jones,et al.  A crack opening displacement approach to crack patching , 1980 .

[12]  M. Ratwani,et al.  Nonlinear adhesive behavior effects in cracked metal-to-composite bonded structures☆ , 1981 .

[13]  R. J. Callinan,et al.  Analysis of bonded repairs to damaged fibre composite structures , 1983 .

[14]  M. M. Ratwani,et al.  A Parametric Study of Fatigue Crack Growth Behavior in Adhesively Bonded Metallic Structures , 1978 .

[15]  M. Ratwani Analysis of Cracked, Adhesively Bonded Laminated Structures , 1979 .

[16]  A. Baker Repair of cracked or defective metallic aircraft components with advanced fibre composites—an overview of Australian work , 1984 .

[17]  R. J. Callinan,et al.  A design study in crack patching , 1981 .

[18]  Ramesh Chandra,et al.  Photoelastic determination of stress intensity factors in patched cracked plates , 1983 .

[19]  A. Baker A summary of work on applications of advanced fibre composites at the Aeronautical Research Laboratories, Australia , 1978 .

[20]  L. Rose An application of the inclusion analogy for bonded reinforcements , 1981 .

[21]  M. Ratwani,et al.  Influence of nonlinear adhesive behavior on analysis of cracked adhesively bonded structures , 1980 .

[22]  T. S. Ramamurthy,et al.  Analytical estimation of stress intensity factors in patched cracked plates , 1985 .

[23]  L. Rose Crack reinforcement by distributed springs , 1987 .