Abstract
The fatigue crack growth behavior of aluminum alloy 5083-H131 has been systematically studied as a function of degree of sensitization for aging at 448 K (175 °C). Fatigue crack growth rates were measured at load ratios of 0.1 and 0.85, in vacuum, air, and a corrosive aqueous environment containing 1 pct NaCl with dilute inhibitor. Sensitization does not affect the fatigue crack growth behavior of Al 5083-H131 significantly in vacuum or air, at low- or high-load ratio. For high-load ratio, in the 1 pct NaCl+inhibitor solution, the threshold drops by nearly 50 pct during the first 200 hours of aging, then it degrades more slowly for longer aging times up to 2000 hours. The change in aging behavior at approximately 200 hours seems to be correlated with the transition from partial coverage of the grain boundaries by β Al3Mg2 phase, to continuous full β coverage. ASTM G-67 mass loss levels below approximately 30 mg/cm2 do not exhibit degraded corrosion-fatigue properties for R = 0.85, but degradation of the threshold is rapid for higher mass loss levels.
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E.L. Huskins, B. Cao, K.T. Ramesh: Mater. Sci. Eng. A, 2010, vol. 527, pp. 1292-98.
R.A. Sielski: Ships and Offshore Structures, 2008, vol. 3, pp. 57-65.
W.G. Babcock and E.J. Czyryca: AMPTIAC Quart., 2003, vol. 7, no. 3, pp. 31-36.
G.C. Blaze: Alcoa Green Letter: The 5000 Series Alloys Suitable for Welded Structural Applications, Aluminum Corporation of America, New Kensington, PA, 1972.
E.H. Dix, W.A. Anderson, and M.B. Shumaker: Corrosion, 1959, vol. 15, no. 2, pp. 19-26.
J.L. Searles, P.I. Gouma, and R.G. Buchheit: Metall. Mater. Trans. A, 2001, vol. 32A, pp. 2859-67.
R.H. Jones, D.R. Bauer, M.J. Danielson, and J.S. Vetrano: Metall. Mater. Trans. A, 2001, vol. 32A, pp. 1699-1711.
F.S. Bovard: Corrosion in Marine and Saltwater Environments II, Eds. D.A. Shifler, T. Tsuru, P.M. Natishan, and S. Ito, vols. 2004–2014, Electrochemical Society, Pennington, NJ, 2005, pp. 232–243.
C.R. Wong, G.P. Mercier, and J.J. Deloach: SeaFrame, 2007, vol. 3, no. 2, pp. 18-20.
N. Birbilis and R.G. Buchheit: J. Electrochem. Soc., 2005, vol. 152, pp. B140-51.
R.H. Jones: J. Met., 2003, vol. 55, no. 2, pp. 42–46.
M. Fellerkniepmeier, K. Detert, and L. Thomas: Z. Metallkunde, 1964, vol. 55, pp. 83-87.
P.N.T. Unwin and R.B. Nicholson: Acta Metall., 1969, vol. 17, pp. 1379-93.
L.I. Kaygorodova, B.N. Balandin, and N.N. Buynov: Phys. Met. Metall., 1985, vol. 59, pp. 126-30.
T. Sato and A. Kamio: Mater. Sci. Eng. A, 1991, vol. A146, pp. 161-80.
H. Inagaki: Z. Metallkunde, 2005, vol. 96, pp. 45-53.
A.J. Davenport, Y. Yuan, R. Ambat, B.J. Connolly, M. Strangwood, A. Afseth, and G. Scamans: Mater. Sci. Forum, 2006, vols. 519-521, pp. 641-46.
M.F. Komarova, N.N. Buinov, and L.I. Kaganovi: Phys. Met. Metall., 1973, vol. 36, pp. 358-64.
S. Osaki: Technology Reports of the Yamaguchi University, 1974, vol. 1, no. 3, pp. 347-48.
J.R. Pickens, J.R. Gordon, and J.A.S. Green: Metall. Trans. A, 1983, vol. 14A, pp. 925-30.
M. Popovic and E. Romhanji: J. Mater. Process. Technol., 2002, vols. 125–126, pp. 275–80.
R.H. Jones, J.S. Vetrano, and C.F. Windisch: Corrosion, 2004, vol. 60, pp. 1144-54.
I.N.A. Oguocha, O.J. Adigun, and S. Yannacopoulos: J. Mater. Sci., 2008, vol. 43, pp. 4208-14.
L. Tan and T.R. Allen: Corros. Sci., 2010, vol. 52, pp. 548-54.
J. Gao and D.J. Quesnel: Metall. Mater. Trans. A, 2011, vol. 42A, pp. 356-64.
C.B. Crane and R. Gangloff: DoD Corrosion Conf. Proc., NACE International, Houston, TX, Paper 20175, 2011, in press.
J.K. Brosi and J.J. Lewandowski: Scripta Mater., 2010, vol. 63, pp. 799-802.
C. Menzemer and T.S. Srivatsan: Mater. Sci. Eng. A, 1999, vol. A271, pp. 188-95.
K. Van Kranenburg, T. Riemslag, J. Zuidema, S. Benedictus-de Vries, and F. Veer: Mater. Sci., 2001, vol. 37, pp. 970-74.
F. Ford: Corrosion, 1979, vol. 35, pp. 281-87.
J.K. Donald: Fracture Mechanics Characterization of Aluminum Alloys for Marine Structural Applications, SSC-448, Ship Structure Committee, Washington, DC, 2007.
P.S. Pao, R. Goswami, R.A. Bayles, T.M. Longazel, and R.L. Holtz: Fatigue of Materials—Advances and Emergences of Understanding, Eds. T.S. Srivatsan and M.A. Imam, Wiley, Hoboken, NJ, 2010, pp. 85–92.
J.S. Montgomery and E.S. Chin: AMPTIAC Quart., 2004, vol. 8, no. 4, pp. 15-20.
R.L. Holtz, P.S. Pao, R.A. Bayles, T.M. Longazel, and R. Goswami: DoD Corrosion Conference Proceedings, NACE International, Houston, TX, Paper 20421, 2011, in press.
R. Goswami, G. Spanos, P.S. Pao, and R.L. Holtz: Metall. Mater. Trans. A, 2011, vol. 42A, pp. 348-55.
R. Goswami, G. Spanos, P.S. Pao, and R.L. Holtz: Mater. Sci. Eng. A, 2010, vol. 527, pp. 1089-95.
ASTM E647-05, Standard Test Method for Measurement of Fatigue Crack Growth Rates, 2005.
D.O. Sprowls, M.B. Shumaker, J.D. Walsh, and J.W. Coursen: “Evaluation of Stress Corrosion Cracking Susceptibility using Fracture Mechanics Techniques,” Final Report, Contract Number NAS 8-21487, May 1973, Alcoa Laboratories, Pittsburgh, PA.
M. Liu, P. Schmutz, S. Zanna, A. Seyeux, H. Ardelean, G. Song, A. Atrens, and P. Marcus: Corros. Sci., 2010, vol. 52, pp. 562-78.
Z. Xing, S. Yujui, and T. Mingjing: Int. J. Fatigue, 1991, vol. 13, pp. 69-72.
C.J. van der Wekken and M. Jassen: J. Electrochem. Soc., 1991, vol. 138, pp. 2891-96.
S. Suresh: Fatigue of Materials, 1st ed., Cambridge University Press, New York, NY, 1991, pp. 245-47.
Z.M. Gasem and R.P. Gangloff: Chemistry and Electrochemistry of Corrosion and Stress Corrosion Cracking: A Symposium Honoring the Contributions of R.W. Steahle, Ed. R.H. Jones, TMS, Warrendale, PA, 2001, pp. 501–21.
J.S. Warner, S. Kim, and R.P. Gangloff: Int. J. Fatigue, 2009, vol. 31, pp. 1952-65.
R.H. Jones, V.Y. Gertsman, J.S. Vetrano, and C.F. Windisch: Scripta Mater., 2004, vol. 50, pp.1355-59.
ASTM E 1681-03, “Standard Test Method for Determining Threshold Stress Intensity Factor for Environment-Assisted Cracking of Metallic Materials,” 2003.
F.S. Bovard: Alcoa Center, PA, Private communication, 2010.
S. Suresh: Fatigue of Materials, 1st ed., Cambridge University Press, New York, NY, 1991, pp. 380-82.
L. Hagn: Mater. Sci. Eng. A, 1988, vol. A103, pp.193-205.
R.P. Wei: Fatigue Fract. Eng. Mater. Struct., 2002, vol. 25, pp. 845-54.
I.P. Gnyp and V.I. Pokhmursky: Mater. Sci., 1994, vol. 30, pp. 621-35.
R.P. Wei and G.W. Simmons: Int. J. Fract., 1981, vol. 17, pp. 235-47.
K. Sadananda and A.K. Vasudevan: Int. J. Fatigue, 2004, vol. 26, pp. 39-47.
K. Sadananda, A.K. Vasudevan, and R.L. Holtz: Int. J. Fatigue, 2001, vol. 23, pp. S277-86.
K. Sadananda, A.K. Vasudevan, and I.W. Kang: Acta Mater., 2003, vol. 51, pp. 3399-3414.
K. Sadananda and A.K. Vasudevan: Int. J. Fatigue, 2005, vol. 27, pp. 1255-66.
K. Sadananda and A.K. Vasudevan: Fatigue Frac. Eng. Mater. Struct., 2003, vol. 26, pp. 835-45.
ASTM G-67-04, “Standard Test Method for Determining the Susceptibility to Intergranular Corrosion of 5XXX Series Aluminum Alloys by Mass Loss After Exposure to Nitric Acid (NAMLT Test),” 2004.
Acknowledgments
The authors are grateful to Dr. Francine Bovard of Alcoa for providing the material used in this study and basic stress corrosion cracking threshold characterization. Co-author R. Goswami is under contract with the Naval Research Laboratory. This work was funded in part by the Office of Naval Research, Dr. Lawrence Kabacoff, Program Officer.
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Manuscript submitted March 31, 2011.
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Holtz, R.L., Pao, P.S., Bayles, R.A. et al. Corrosion-Fatigue Behavior of Aluminum Alloy 5083-H131 Sensitized at 448 K (175 °C). Metall Mater Trans A 43, 2839–2849 (2012). https://doi.org/10.1007/s11661-011-0866-x
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DOI: https://doi.org/10.1007/s11661-011-0866-x