Prediction of Fatigue Crack Growth of Aged Hardening Al-Alloys under Variable Amplitude Loading

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In this investigation, variable amplitude loading effect was studied on aged hardening Al-alloys in series 2000 and 7000. Generalised Willenborg model was used in order to show loading interaction effects (overload effects). Variable amplitude loading under different form of spectrum has affected highly the fatigue life and fatigue crack growth rates. Fatigue lives were increased and fatigue crack growth rates (FCGRs) were decreased in increasing of overload ratio in single overload case. In application of overload band, the fatigue lives and FCGRs were affected by band overload and R-ratio of them when level in FCGRs was increased.

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Advanced Materials Research (Volumes 891-892)

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1729-1735

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March 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] Jr J.C. Newman, J.J. Ruschau, The stress-level effect on fatigue crack growth under constant amplitude loading". Int. J. of Fatigue 29 (2000) 1608-1615.

DOI: 10.1016/j.ijfatigue.2006.11.003

Google Scholar

[2] J. R Mohanty, B. B Verma, P.K. Ray, Prediction of fatigue crack growth and residual life using an exponential model: Part I (CAL)". Int. J. of Fatigue 31 (2009) 418-424.

DOI: 10.1016/j.ijfatigue.2008.07.015

Google Scholar

[3] M. Benachour, A. Hadjoui, M. Benguediab, N. Benachour, Effect of the amplitude loading on FCG". Procedia Engineering 2 (2010) 121-127.

DOI: 10.1016/j.proeng.2010.03.013

Google Scholar

[4] A.T. Kermanidis, Sp.G. Pantelakisn, Prediction of crack growth following a single overload in Al-alloy with sheet and plate microstructure". Engng Fract. Mech. 78 (2011) 2325-2337.

DOI: 10.1016/j.engfracmech.2011.05.005

Google Scholar

[5] R. Kumar, S.B.L. Garg, Effect of single and intermediate tensile overload cycles on effective stress range ratio in 6063-T6 Al-alloys". Int. J. of Press. Vess. & Piping 36 (1989) 257-68.

DOI: 10.1016/0308-0161(89)90051-3

Google Scholar

[6] D.M. Corbley, P.F. Packman On the influence of single and multiple peak overloads on fatigue crack propagation in 7075 T6511 aluminum. Engng Fract. Mech., 5. (1973) 479-497.

DOI: 10.1016/0013-7944(73)90034-9

Google Scholar

[7] G.R. Chanani, B.J. Mays Observation of crack closure behaviour after single overload cycles in 7075-T6 single edge notched specimens. Engineering Fracture Mechanics, 9 (1977) 65-73.

DOI: 10.1016/0013-7944(77)90052-2

Google Scholar

[8] O.E. Wheeler Spectrum Loading and Crack Growth, Transaction of the ASME, Journal of Basic Engineering (1972) 181-186.

Google Scholar

[9] J. Willenborg, R. M. Engle, H. A. Wood, A crack growth retardation model using an effective stress concept" AFFDL-TM-FBRgl-7 (Air Force Dynamics Laboratory, Dayton, USA), (1979).

DOI: 10.21236/ada956517

Google Scholar

[10] K. Sadananda, AK. Vasudevan, Analysis of overloads effects and related phenomena. Int. J. of Fatigue 21 (1999) S233–246.

Google Scholar

[11] F. Taheri, D. Trask, N. Pegg, Experimental and analytical investigation of fatigue characteristics of 350WT steel under constant and variable amplitude loadings. Journal of Marine Structure 16 (2003) 69–91.

DOI: 10.1016/s0951-8339(02)00004-7

Google Scholar

[12] J.P. Gallagher, A Generalized Development of Yield-Zone Models, " AFFDL-TM-74-28, Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, (1974).

Google Scholar

[13] C.M. Ward-Close, A.F. Blom, R.O. Ritchie Mechanisms associated with transient fatigue crack growth under variable-amplitude loading: an experimental and numerical study. Engng Fract. Mech. 32 (1989) 613–38.

DOI: 10.1016/0013-7944(89)90195-1

Google Scholar

[14] R.H. Christensen, Metal fatigue. New York: McGraw-Hill, (1959).

Google Scholar

[15] J. F Knott, A.C. Pickard, Effects of overloads on fatigue-crack propagation: aluminium alloys. Metal Science 11 (1977) 399–404.

DOI: 10.1179/msc.1977.11.8-9.399

Google Scholar

[16] Ch. Bichler, R. Pippan, Effect of single overloads in ductile metals: a reconsideration. Engng Fract. Mech. 74 (2007) 1344–1359.

DOI: 10.1016/j.engfracmech.2006.06.011

Google Scholar

[17] L.P. Borrego, J.M. Ferreira, J.M. Pinho da Cruz, J.M. Costa Evaluation of overload effects on fatigue crack growth and closure". Engng Fract. Mech. 70 (2003) 1379-1397.

DOI: 10.1016/s0013-7944(02)00119-4

Google Scholar

[18] C. Bathias, M. Vancon, Mechanisms of overload effect on fatigue crack propagation in aluminium". Engng Fract. Mech. 10 (1978) 409-424.

DOI: 10.1016/0013-7944(78)90021-8

Google Scholar

[19] D.M. Corbley, P.F. Packman On the influence of single and multiple peak overloads on fatigue crack propagation in 7075 T6511 Al". Engng Fract. Mech. 5 (1973) 479-497.

DOI: 10.1016/0013-7944(73)90034-9

Google Scholar

[20] O. Vardar, Effect of single overload in FCP, Engng Fract. Mech. 30 (1988) 329-335.

Google Scholar

[21] A.T. Kermanidis, Sp.G. Pantelakisn, Prediction of crack growth following a single overload in Al-alloy with sheet and plate microstructure". Engng Fract. Mech. 78 (2011) 2325–2337.

DOI: 10.1016/j.engfracmech.2011.05.005

Google Scholar

[22] B.B. Verma, R.K. Pandey, The effects of loading variables on overload induced fatigue crack growth retardation parameters. Journal of Materials Science 34 (1999), 4867-4871.

Google Scholar

[23] R. Kumar, S. B. L. Garg, Effect of periodic bands of overloads on crack closure. Int. J. Pres. Ves. & Piping 38 (1989) 27-37.

DOI: 10.1016/0308-0161(89)90129-4

Google Scholar

[24] J.M. Potter The effect of interaction and sequence on the fatigue behavior of notched coupons. ASTM special Technical Publication 519 (1973) 109-132.

Google Scholar

[25] Rui Bao, Xiang Zhang, Fatigue crack growth behavior and life prediction for 2324-T39 and 7050-T7451 Al-alloys under truncated load spectra. Int. J. of Fatigue, 32(7) (2009) 1180-89.

DOI: 10.1016/j.ijfatigue.2009.12.010

Google Scholar

[26] J.C. Newman, predicting failure of specimens with either surface crack or comer crack at holes. TND-8244, NASA Langley Research Center, (1976).

Google Scholar

[27] J.A. Harter, AFGROW users guide and technical manual: AFGROW for Windows 2K/XP. Version 4. 0011. 14, Air Force Research Laboratory, (2006).

DOI: 10.21236/ada370431

Google Scholar