Abstract
Shot peening is a commonly used surface treatment process that imparts compressive residual stresses into the surface of metal components. Compressive residual stresses retard initiation and growth of fatigue cracks. During component loading history, shot-peened residual stresses may change due to thermal exposure, creep, and cyclic loading. In these instances, taking full credit for compressive residual stresses would result in a nonconservative life prediction. This article describes a methodical approach for characterizing and modeling residual stress relaxation under elevated temperature loading, near and above the monotonic yield strength of INI 00. The model incorporates the dominant creep deformation mechanism, coupling between the creep and plasticity models, and effects of prior plastic strain to simulate surface treatment deformation.
Similar content being viewed by others
References
P. Prevéy, D. Hornbach, and P. Mason, Proceedings of the 17th Heat Treating Society Conference and Exposition and the 1st International Induction Heat Treating Symposium, ed. D.L. Milam et.al. (Materials Park, OH: ASM International, 1998), pp. 3–12.
T.P. Gabbetal., TMS Lettere, 1(5) (2004), pp. 115–116.
W. Cao et al., Material Science and Technology, 10 (November 1994), pp. 947–954.
H. Holzapfel et al., Material Science and Engineering, A248 (1998), pp.9–18.
P. Prevéy, Proceedings of the 20th ASM Materials Solution Conference & Exposition (Materials Park, OM: ASM International, 2000), pp. 426–434.
D.J. Buchanan, R. John, and N.E. Ashbaugh, ASTM STP 1497 — Residual Stress Effects on Fatigue and Fracture Testing and Incorporation of Results into Design (West Conshohocken, PA: ASTM, 2007), pp. 47–57.
J.L. Chaboche and O. Jung, International Journal of Plasticity, 13(10) (1998), pp. 785–807.
G. Schoeck, Mechanical Behavbr of Materials at Elevated Temperatures, ed. J.E. Dorn (New York: McGraw-Hill Book Company, Inc., 1961), pp. 79–107.
A.S. Nowick and E.S. Machlin, National Advisory Committee for Aeronautics (NACA), Technical Note No. 1039 (Washington, D.C.: NACA, April 1946). [NACA was dissolved on October 1,1958 and its assets transferred to the newly created National Aeronautics and Space Administration (NASA).]
J. Weertman, J. Applied Physics, 26(10) (1955), pp. 1213–1217.
L.M. Kachanov, Izv. Akad. Nauk. SSR, Otd Tekh., Nauk No. 8 (1958), pp. 26–31.
Y.N. Rabotnov, Creep Problems in Structural Members (New York: American Elsevier Publishing Co., 1969), p. 137.
J.L. Chaboche, J. Applied Mechanics, 55 (March 1988), pp. 59–64.
J.L. Chaboche, J. Applied Mechanics, 55 (March 1988), pp. 65–72.
D.R. Sanders (Ph.D. thesis, Texas A&M University, 1986).
M. McLean and B.F. Dyson, J. Engineering Materials and Technology, 122 (July 2000), pp. 273–278.
B.F. Dyson, J. Pressure Vessel Technology, 122 (August 2000), pp. 281–296.
S.K. Sondhi, B.F. Dyson, and M. McLean, Acta Materialia, 52 (2004), pp. 1761–1772.
H. Basoalto et al., Superalloys 2004, ed. K.A. Green et al. (Warrendale, PA: TMS, 2004), pp. 897–906.
S.R. Bodner, J. Applied Mechanics, Transactions of the ASME (June 1975), pp. 385–389.
K. Walker, NASA Contractor Report, NASA-CR-165533 (Springfield, VA: National Technical Information Service, 1981).
V.G. Ramaswamy, NASA Contractor Report 3998 (Washington, D.C.: NASA Scientific and Technical Information Branch, 1986).
D.N. Robinson, ORNL TM-5969 (Oak Ridge, TN: U.S. Department of Energy Technical Information Center, 1978).
A.K. Miller, Trans. ASME Journal of Engineering Materials and Technology, 96 (1976), p. 97.
K. Li, N.E. Ashbaugh, and A.H. Rosenberger, Superalloys 2004, ed. K.A. Green et al. (Warrendale, PA: TMS 2004), pp. 251–258.
R.H. Dodds, Computers & Structures, 26(5) (1987), pp. 767–779.
D.J. Buchanan et al., Superalloys 2008, ed. R.C. Reed et al. (Warrendale, PA: TMS 2008), pp. 965–974.
D.J. Buchanan, R. John, and R.A. Brockman, J. Engineering Materials and Technology, 131(3) (2009), 031008.
D. Kirk, Proceedings of the Third International Conference on Shot Peening, ed. H. Wohlfahrt, R. Kopp, and O. Vöhringer (Mishawaka, IN: Int’l. Scientific Committee for Shot Peening, 1987), pp. 213–220.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
About this article
Cite this article
Buchanan, D.J., John, R., Brockman, R.A. et al. A coupled creep plasticity model for residual stress relaxation of a shot-peened nickel-based superalloy. JOM 62, 75–79 (2010). https://doi.org/10.1007/s11837-010-0016-8
Published:
Issue Date:
DOI: https://doi.org/10.1007/s11837-010-0016-8