Finite element-based three-dimensional stress analysis of composite bonded repairs to metallic aircraft structure

International Journal of Adhesion and Adhesives

Volumn 26, Issue 4, 2006, Pages 261-273

  Kaye, R ^a   Heller, M ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

Aluminium and alloys, composites; Finite element stress analysis; Repair; Stress concentration

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; COMPOSITE MATERIALS; FUSELAGES; REPAIR; STRESS CONCENTRATION; STRUCTURAL ANALYSIS;

ALUMINIUM AND ALLOYS, COMPOSITES; FINITE ELEMENT STRESS ANALYSIS; METALLIC AIRCRAFT STRUCTURE; THREE-DIMENSIONAL STRESS ANALYSIS;

STRESS ANALYSIS;

COMPOSITES; MAINTENANCE; STRESS ANALYSIS; STRESS CONCENTRATION; STRUCTURAL ANALYSIS;

EID: 30544436408     PISSN: 01437496     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijadhadh.2005.03.016     Document Type: Article

References (11)

1. Baker AA, Jones R, editors. Bonded repair of aircraft structures, Dordrecht: Martinus Nyhoff; 1988, ISBN 90-247-3606-4.
2. Hart-smith LJ. Adhesive bonded double lap joints, NASA CR-112235, 1973.
3. M. Heller, and R. Kaye Structural optimisation of bonded repairs, advances in the bonded composite repair of metallic airframe structures 2002 Exelvier Press New York 0-08-042699-9 (Chapter 8)
4. Shah LP, Heller M, Wang CH, Williams JF. Reduction of plate stress concentration factors due to bonded reinforcements, vol 2. International aerospace conference; 1997.
5. Callinan RJ, Sanderson S, Keeley D. 3D F. E. analysis of a bonded repair to an F111 wing, vol 2. First Australasian congress on applied mechanics; 1996. pp. 577-82.
6. A. Sheppard, D. Kelly, and L. Tong A Damage zone model for the failure analysis of adhesively bonded joints Int J Adhes Adhes 18 1998 385 400
7. R.H. Andruet, D.A. Dillard, and S.N. Holzer Two and three dimensional geometrical nonlinear finite elements for analysis of adhesive joints Int J Adhes Adhes 21 2001 17 34
8. M. Cheik, P. Coorevits, and A. Lorado Modelling the stress vector continuity at the interface of bonded joints Int J Adhes Adhes 21 2001 249 257
9. Kaye R, Heller M. Through-thickness shape optimisation of typical double lap-joints including effects of differential thermal contraction during curing. Int J Adhes Adhes 2004, accepted for publication.
10. J. Wang, A. Rider, M. Heller, and R. Kaye Theoretical and experimental research into optimal edge taper of bonded repair patches subject to fatigue loadings Int J Adhes Adhes 25 2005 410 426
11. C.H. Wang Fatigue crack growth analysis of repaired structures. Advances in the bonded composite repair of metallic airframe structures 2002 Exelvier Press New York 0-08-042699-9 (Chapter 12)