[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: 10.1016/0013-7944(93)90262-q
Google Scholar
[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: 10.1016/0013-7944(91)90035-y
Google Scholar
[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: 10.1016/0963-8695(92)90745-3
Google Scholar
[4]
A. Berkovits, and D. Fang : Study of Fatigue Characteristics by Acoustic Emission, Engineering Fracture Mechanics, Vol. 51(3), (1995), pp.401-416.
DOI: 10.1016/0013-7944(94)00274-l
Google Scholar
[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: 10.1016/0025-5416(78)90206-9
Google Scholar
[6]
P. M. Toor : Cracks Emanating from Precracked Cold-Worked Holes, Engineering Fracture Mechanics, Vol. 8, (1978), pp.391-395.
DOI: 10.1016/0013-7944(76)90019-9
Google Scholar
[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.
Google Scholar
[8]
Leon, A., : Benefits of Split Mandrel Coldworking, Int. J. Fatigue, Vol. 20(1), (1998), pp.1-8.
DOI: 10.1016/s0142-1123(97)00059-5
Google Scholar
[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: 10.2514/3.25328
Google Scholar