Fatigue Life Recovery in Corroded Aluminium Alloys Using Bonded Composite Reinforcements
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Abstract
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Research context
OpenAlex topics: Fatigue and fracture mechanics · Advanced Welding Techniques Analysis · Concrete Corrosion and Durability
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References (8)
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1. Cole G., Clark G. and Sharp K., ‘The implications of corrosion with respect to aircraft structural integrity,’ DSTO Research Report, DSTO-RR-0102, 1997.
2. Baker A.A., Rose L.F.J, and Jones R. (eds.), Advances in the Bonded Composite Repair of Aircraft Structure, Elsevier 2002, Chapter 1.10.1016/B978-008042699-0/50003-6 ↗
3. Cole G., Clark G. and Sharp K., ‘The implications of corrosion with respect to aircraft structural integrity’, DSTO Research Report, DSTO-RR-0102, 1997. Chapters 11 to 13.
4. Baker A.A., Rose L.F.J, and Jones R. (eds.), Advances in the Bonded Composite Repair of Aircraft Structure, Elsevier 2002. Chapter 13.
5. Burchill, M. and Heller, M., J Strain Analysis 39, 2003, 99–115.10.1177/030932470403900108 ↗
6. Sharp, P.K., Mills, T., Clark, G. and Russo, S., ‘Recent advances in modelling exfoliation corrosion,’ Australian Fracture Group Conference Sydney 2000.
7. Baker A.A., Rose L.F.J, and Jones R. (eds.), Advances in the Bonded Composite Repair of Aircraft Structure, Elsevier 2002. Chapter 3.
8. Crawford, B.R., Loader, C., Ward, A.R., Urbani, C., Bache, M.R., Spence, S.H., Hay, D.G., Evans, W.J., Clark, G. and Stonham, A.J., ‘The EIFS Distribution for Anodized and Pre-Corroded 7010-T7651 Under Constant Amplitude Loading’, Fatigue and Fracture of Engineering Materials and Structures 28(9), (2005), 795–808.10.1111/j.1460-2695.2005.00912.x ↗