[[1] J. Zehnder, Aluminium: Technology, application, and environment, a profile of a modern metal, (ed) Dietrich G Altenpohl (Pennsylvania: TMS Warrendale) (1997) p. 319]Search in Google Scholar
[[2] B. B. Verma, J. D. Atkinson and M. Kumar, Bull. Mater. Sci., 24 (2001), 23110.1007/BF02710107]Search in Google Scholar
[[3] Hendricks, W.R., Structural Integrity of Aging Airplanes, (Atluri, S.N., Sampath, S.G., Tong, P., editors), Springer-Verlag Berlin, Heidelberg, (1991) p. 153]Search in Google Scholar
[[4] Inman, M.E., Kelly, R.G., Willard, S.A., Piascik, R.S., Proc. of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures, Atlanta, Georgia, (Bigelow, C., editor), National Technical Information Service, Springfield, Virginia 22161, USA, (1996) pp. 129-146]Search in Google Scholar
[[5] Bray, G.H., Bucci, R.J., Colvin E.L., and Kulak, M., ASTM STP 1298, (Van Der Sluys, W.A., Piascik, R.S., and Zawierucha, R., editors), American Society for Testing and Materials, (1997) pp. 89-103]Search in Google Scholar
[[6] Zamber, J.E. and Hillberry, B.M. (1999). Probabilistic approach to predicting fatigue lives of corroded 2024-T3. AIAA Journal, 37, 1311-131710.2514/2.602]Search in Google Scholar
[[7] Chubb, J.P., Morad, T.A., Hockenhull, B.S., Bristow, J.W., The effect of exfoliation corrosion on the fatigue behaviour of structural aluminium alloys, In Structural Integrity of Aging Airplanes, (Atluri, S.N., Sampath, S.G., Tong, P., editors), Springer-Verlag Berlin, Heidelberg, pp. 87-97 (1991)10.1007/978-3-642-84364-8_6]Search in Google Scholar
[[8] A Monasalve, M Paez, M Toledano, A Artigas, Y Sepulveda and Y N Valencia Fatigue Fract Engng Mater Struct. Vol. 30, pp. 748–758 (2007)10.1111/j.1460-2695.2007.01134.x]Search in Google Scholar
[[9] C. C. Osgood, Fatigue Design, 2nd ed. Pergamon Press, New York, 1982, p 439.10.1016/B978-0-08-026167-6.50006-0]Search in Google Scholar