SIF for Double- and single-sided composite repair in mode i and mixed mode

Journal of Reinforced Plastics and Composites

Volumn 29, Issue 10, 2010, Pages 1463-1475

  Bachir Bouiadjra, B ^a   Fekirini, H ^a   Belhouari, M ^a   Serier, B ^a   Benguediab, M ^a   Ouinas, D ^b  

^a UNIVERSITY OF SIDI BEL ABBES   (Algeria)

^b UNIVERSITY OF MOSTAGANEM   (Algeria)

Author keywords

Composite patch; Double patch; Finite element method; Mixed mode; Mode I; SIF; Single patch

Indexed keywords

ADHESIVE FAILURE; ADHESIVE PROPERTIES; AIRCRAFT STRUCTURE; BENEFICIAL EFFECTS; COMPOSITE PATCH; COMPOSITE PATCHES; COMPOSITE REPAIR; FINITE ELEMENT; MIXED MODE; SINGLE PATCH;

AIRCRAFT MANUFACTURE; AIRFRAMES; CRACK TIPS; REPAIR; STRESS INTENSITY FACTORS;

FINITE ELEMENT METHOD;

EID: 77953017197     PISSN: 07316844     EISSN: 15307964     Source Type: Journal    
DOI: 10.1177/0731684409102836     Document Type: Article

References (12)

1. Baker, A.A. (1999). Bonded Composite Repair for Fatigue-cracked Primary Aircraft Structure, Compos. Struct., 74: 431-443.
2. Callinan, R.J., Sanderson, S. and Keeley, D. (1997). Finite Element Analysis of an F-111 Lower Wing Skin Fatigue Crack Repair, DSTO, Melbourne. DSTO-TN-0067.
3. Schubbe, J.J. and Mall, S. (1999). Modeling of Cracked Thick Metallic Structure with Bonded Composite Patch Repair Using Three-layer Technique, Compos. Struct., 45: 185-193.
4. Ting, T., Jones, R., Chiu, W.K., Marshall, I.H. and Greer, J.M. (1999). Composite Repair to Rib Stiffned Panels, Compos. Struct., 47: 737-743.
5. Turaga, V.R.S. and Ripudaman, S. (1999). Modelling of Patch Repair to a Thin Cracked Sheet, Eng. Fract. Mech., 62: 267-289.
6. Jones, R. and Chiu, W.K. (1999). Composite Repairs to Crack in Metallic Components, Compos. Struct., 44: 17-29.
7. Bachir, B.B., Belhouari M. and Serier, B. (2002). Computation of the Stress Intensity Factors for Repaired Cracks with Bonded Composite Patch in Mode I and Mixed Mode, Compo. Struct., 56: 401-406.
8. Chen, W.H. and Yang, S.H. (1995). Estimation of Stress Intensity Factors in Partially Patched Cracked Composite Laminates by Multiplayer Hybrid-stress Finite Element Method., Finite Elem. Anal. Des., 21: 21-44.
9. Megueni, A., Bachir, B.B. and Boutabout, B. (2003). Computation of the Stress Intensity Factor for Patched Crackwith Bonded Composite Repair in Pure Mode II, Comp. Struct., 59: 415-418.
10. Achour, T., Bachir, B.B. and Serier, B. (2003). Numerical Analysis of the Performances of the Bonded Composite Patch for Reducing Stress Concentration and Repairing Cracks at Notch, Comp. Mat. Sci., 28: 41-48.
11. Klug, J.C., Maley, S. and Sun, C.T. (1999). Characterization of Fatigue Behaviour of Bonded Composite Repairs., J. Aircraft, 36 (6). 1016-1022.
12. Swenson, D. and James, M. (1998). FRANC2D/L: Version 1.4 Users Guide available online on the web site: www.cfg.cornell.edu.