Repair of cracked or defective metallic aircraft components with advanced fibre composites—an overview of Australian work
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Abstract
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Research context
OpenAlex topics: Structural Load-Bearing Analysis · Mechanical Behavior of Composites · Fatigue and fracture mechanics
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References (25)
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1. Work on advanced fibre composites at the Aeronautical Research Laboratories10.1016/0010-4361(78)90512-8 ↗
2. Evaluation of adhesives for fibre composite reinforcement of fatigue cracked aluminium alloys
3. Anodize optimization and adhesive evaluation for repair applications
4. Composite to metal bonding using thermosetting adhesives
5. Repair of fatigue cracked aircraft structures with advanced fibre composites: residual stress and thermal fatigue studies
6. Fibre composite reinforcement of cracked aircraft structures—thermal stress and thermal fatigue studies
7. Thermal considerations in the patching of metal sheets with composite overlays10.1080/03601218008907356 ↗
8. Finite element analysis of patched cracks10.1080/03601217908905315 ↗
9. A design study in crack patching10.1016/0015-0568(81)90035-X ↗
10. Analysis and repair of flaws in thick sections
11. Analysis of composite laminates and fibre composite repair schemes10.1016/0015-0568(81)90004-X ↗
12. A cracked plate repaired by bonded reinforcements10.1007/BF00019638 ↗
13. An application of the inclusion analogy for bonded reinforcements10.1016/0020-7683(81)90091-3 ↗
14. Experimental study of overlap joint parameters relevant to the K reduction due to crack patching
15. Fibre composite reinforcement of cracked aircraft structures
16. Application of BFRP crack patching to Mirage III aircraft
17. Williams, J. G., Roberts, J. D. and Hill, T. G., Repair of skin damage in aircraft under field conditions, ARL Technical Note, to be published.
18. Advanced composite cost comparison
19. Application of composites to the selective reinforcement of metallic aerospace structures
20. Torsional instabilities in composite and composite-reinforced aluminium-alloy thin walled cylinders
21. Boron-polyimide reinforced titanium fan discs
22. Neutral holes in plane sheet—reinforced holes which are elastically equivalent to the uncut sheet10.1093/qjmam/6.3.370 ↗
23. Three-dimensional stress analysis of cylindrically wound fibre reinforced annular discs surrounding a circular hole in a flat plate10.1016/0020-7403(76)90043-6 ↗
24. Analysis of composition reinforced cutouts and cracks
25. Mollifying stress fields by using filamentary composite materials