Fatigue Crack Detection in Coldworked Aluminum Alloys Using Acoustic Emission Technique


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Key Engineering Materials (Volumes 270-273)

Edited by:

Seung-Seok Lee, Dong-Jin Yoon, Joon-Hyun Lee and Sekyung Lee




D. S. Lee et al., "Fatigue Crack Detection in Coldworked Aluminum Alloys Using Acoustic Emission Technique ", Key Engineering Materials, Vols. 270-273, pp. 537-542, 2004

Online since:

August 2004




[1] M. O. Lai, J. T. Oh and Y. C Nee : Fatigue Properties of hole with residual stresses, Engineering Fracture Mechanics, Vol. 45(5), (1993), pp.551-557.

DOI: https://doi.org/10.1016/0013-7944(93)90262-q

[2] M. Heller, R. Jones and J. F. Williams : Analysis of cold-expansion for cracked and uncracked fastener holes, Engineering Fracture Mechanics, Vol. 39(2), (1991), pp.195-212.

DOI: https://doi.org/10.1016/0013-7944(91)90035-y

[3] S.L. McBride, P. Bowman, and K.I. McRae : The Acoustic Emission Source Mechanism for Fatigue Crack Propagation in 7075 Aluminum, Journal of Acoustic Emission, Vol. 7(4), (1988), pp.225-229.

DOI: https://doi.org/10.1016/0963-8695(92)90745-3

[4] A. Berkovits, and D. Fang : Study of Fatigue Characteristics by Acoustic Emission, Engineering Fracture Mechanics, Vol. 51(3), (1995), pp.401-416.

DOI: https://doi.org/10.1016/0013-7944(94)00274-l

[5] Lindley, T. C., Palmer, I. G. and Richards, C. E., : Acoustic Emission Monitoring of Fatigue Crack Growth, Materials Science and Engineering, Vol. 32, (1978), pp.1-15.

DOI: https://doi.org/10.1016/0025-5416(78)90206-9

[6] P. M. Toor : Cracks Emanating from Precracked Cold-Worked Holes, Engineering Fracture Mechanics, Vol. 8, (1978), pp.391-395.

DOI: https://doi.org/10.1016/0013-7944(76)90019-9

[7] F, Alten. J,R. Grandt, and J. Terry : The Effect of Edge Distance on Coldworking Fastener Holes, The Fourth Joint DoD/FAA/NASA Conference on Aging Aircraft, (2000), pp.1-20.

[8] Leon, A., : Benefits of Split Mandrel Coldworking, Int. J. Fatigue, Vol. 20(1), (1998), pp.1-8.

[9] R. E. Link, and R. J. Sanford : Residual Strains Surrounding Split Sleeve Cold Expanded Holes in 7075-T7451 Aluminum, Journal of Aircraft, Vol. 27(7), (1990), pp.599-604.

DOI: https://doi.org/10.2514/3.25328