Fracture mechanics analysis of cracked plate repaired by composite patch

Key Engineering Materials

Volumn 183, Issue , 2000, Pages

  Chung, K H ^a   Yang, W H ^a   Cho, M R ^b  

^a Sungkyunkwan University   (South Korea)

^b Induk University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; AIRCRAFT PARTS AND EQUIPMENT; ALUMINUM; BONDING; BORON; COMPOSITE MATERIALS; EPOXY RESINS; FINITE ELEMENT METHOD; FRACTURE MECHANICS; REPAIR; SERVICE LIFE; STRESS INTENSITY FACTORS;

ADHESIVE SHEAR STRESS; AIRCRAFT STRUCTURE; BOUNDARY LAYER EFFECT; COMPOSITE STRESS; DEBONDING;

PLATING;

EID: 0033722375     PISSN: 10139826     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

1. A.A. Baker and R. Jones, Dordrecht: Martinus Nijhoff, (1988), Bonded repair of aircraft structures.
2. R. Jones and R.J. Callinan, J. Struct. Mech., 7(1979) p.107-130, Finite element analysis of patched cracks.
3. R. Jones, R.J. Callinan and K.C. Aggarwal, Engng. Frac. Mech., 17(1983) p.37-46, Analysis of bonded repair to damaged fibre composite structures.
4. R.C. Chu and T.C. Ko, Theor. Appl. Frac. Mech., 17(1989) p.93-102, Isoparametric shear spring element applied to crack patching and instability.
5. J.J. Denney, M.S. Thesis. Air Force Inst. Of Tech. (1995), Fatigue response of cracked aluminum panel with partially bonded composite patch.
6. M. Isida, Int. J. Frac., 7(1971) p.301-316, Effect of width and length on stress intensity factors of internally cracked plates under various boundary conditions.
7. A.R. Ingraffa, Int. J. Numer. Meth. Engng., 7(1980) p.1427-1445, Stress intensity factor computation in three dimensions with quarter point element.
8. K.N. Shivakumar and I.S. Raju, Int. J. Frac., 45(1990) p.159-178, Treatment of singularities in three-dimensional cracked bodies.