Development of a generic repair joint for certification of bonded composite repairs

International Journal of Adhesion and Adhesives

Volumn 19, Issue 2, 1999, Pages 121-132

  Chalkley, Peter ^a   Baker, Alan ^a  

^a AERO AND MAR RESEARCH LABORATORY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVE JOINTS; AIRCRAFT; BONDING; DEFECTS; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; MECHANICAL TESTING; REPAIR;

ADHESIVELY BONDED JOINTS; BONDED COMPOSITE REPAIR; CERTIFICATION; DISBOND GROWTH;

COMPOSITE MATERIALS;

EID: 0033115999     PISSN: 01437496     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0143-7496(98)90028-8     Document Type: Article

References (13)

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2. Baker AA. On the Certification of Bonded Composite Repairs to Primary Aircraft Structure ICCM11, Gold Coast, Australia, 14-18 July 1997.
3. Baker AA. Crack patching: Experimental studies, practical applications. In: Baker AA, editor. Bonded Repair of Aircraft Structures, Chapter 6. Dordrecht: Martinus Nijhoff, 1988.
4. Hart-Smith LJ. Adhesive-bonded double-lap joints. NASA CR 112235, Douglas Aircraft Company, January 1973.
5. Rose LRF. An application of the inclusion analogy for bonded reinforcements. Int J Solids Struct, 1981;17:827-38.
6. Krenk S, Jonsson J, Hansen LP. Fatigue analysis and testing of adhesive joints. Eng Fracture Mech, 1996;53 (6):859-72.
7. Baker AA et al. Reinforcement of the F-111 wing pivot fitting with a boron/epoxy doubler system - material engineering aspects. Composites 1993:24(6).
8. Chalkley PD, Chiu WK. An improved method for testing the shear stress/strain behaviour of adhesives. Int J Adhesion Adhesives. 1993;13 (4).
9. Albat AM et al. Thermal residual strain measurement in a composite repair on a cracked aluminium structure. Presented at ICCM-11, Gold Coast, Australia, 14-18 July 1997.
10. Baker AA. Fatigue studies related to certification of composite crack patching for primary metallic aircraft structure. Presented at FAA-NASA Symp on Continued Airworthiness of Aircraft Structures, Atlanta, 28-30 August 1996.
11. Baker AA, Chester RJ, Davis MJ, Roberts JD, Retchford JA. Reinforcement of the F111 wing pivot fitting with a boron/epoxy doubler system - Materials engineering aspects. Composites 1993: 24(6).
12. Russell AJ. Fatigue crack growth in adhesively bonded graphite/epoxy joints under shear loading. ASME Symp on Advances in Adhesively Bonded Joints, Chicago, 28 November-2 December, 1988.
13. Chai H, Chiang MYM. Finite element analysis of interfacial crack propagation based on local shear, part ii-fracture. Int J Solids Struct, 1998;35 (9-10):815-29.