Abstract
Under fatigue conditions fibre reinforced aluminium–lithium laminates do not respond in the same manner as monolithic aluminium alloys. The variation of fatigue crack growth rates with initial loading condition has been examined for both carbon and glass fibre reinforced laminates, and compared with the behaviour of unreinforced 8090 aluminium–lithium alloy for a range of conditions (different initial nominal stress intensity factor range, load range and reversed loading). During fatigue, cracks grow in the metal layers of these laminates whilst the fibres in the crack wake remain intact, bridging the crack faces. The fibre bridging mechanism, inherent in this laminate system, reduces the fatigue crack growth rate. The magnitude of the bridging effect appears to be inversely related to the applied load range. This relationship can account for the behaviour observed in the performed experiments.
Similar content being viewed by others
References
L. B. VOGELESANG, R. MARISSEN and J. SCHIJVE, in Proceedings of 11th International Committee on Aeronautical Fatigue (ICAF) Symposium, Noorduijkerhoot, The Netherlands, 20-22 May 1981, 3.4/1.
R. O. RITCHIE, WEIKANG YU and R. J. BUCCI, Technical Report UCB/87/AL1049, ALCOA Laboratories, Dec 1987.
R. MARISSEN, Ph.D. thesis, Delft University of Technology, The Netherlands (1988).
S. B. DAVENPORT, Ph.D. thesis, University of Southampton, UK (1995).
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Davenport, S.B., Gregson, P.J., Moreton, R. et al. Response of fibre reinforced aluminium–lithium laminates to different fatigue conditions. Journal of Materials Science 32, 6555–6560 (1997). https://doi.org/10.1023/A:1018619512832
Published:
Issue Date:
DOI: https://doi.org/10.1023/A:1018619512832