0
Article

Relaxation of Peening Residual Stresses Due to Cyclic Thermo-Mechanical Overload

[+] Author and Article Information
S. A. Meguid, G. Shagal, J. C. Stranart

Department of Mechanical and Industrial Engineering, University of Toronto, 5 King’s College Road, Toronto, Ontario, M5S 3G8 Canada

Tel: (416) 978-5741

K. M. Liew, L. S. Ong

School of Mechanical and Production Engineering, Nanyang Technological University, 50 Nanyang Avenue, Singapore 639798

J. Eng. Mater. Technol 127(2), 170-178 (Apr 06, 2005) (9 pages) doi:10.1115/1.1867986 History: Received July 08, 2004; Revised January 08, 2005; Online April 06, 2005
Copyright © 2005 by ASME
Your Session has timed out. Please sign back in to continue.

References

Fuchs, H. O., 1962, Shot-peening effects and specifications, ASTM STP-196.
Meguid, S. A., 1986, editor, Impact Surface Treatment, Elsevier Applied Science Publishers, New York.
Shaw,  M. C., and De Salvo,  G., 1970, “On the plastic flow beneath a blunt axi-symmetric indentor,” ASME J. Eng. Ind., 92, pp. 480–494.
Meguid,  S. A., and Klair,  M. S., 1985, “An examination of the relevance of co-indentation studies to incomplete coverage in shot-peening using the finite-element method,” J. Mech. Work. Technol., 11, pp. 87–104.
Meguid,  S. A., and Klair,  M. S., 1985, “Elasto-plastic co-indentation analysis of a bounded solid using finite element method,” Int. J. Mech. Sci., 27, pp. 157–168.
Li,  A. K., Yao,  M., Wang,  D., and Wang,  R., 1991, “Mechanical approach to the residual stress field induced by shot-peening,” Mater. Sci. Eng., A, 147, pp. 167–173.
Johnson W., 1972, Impact Strength of Materials, Arnold, London.
Iida K., 1984, “Dent and affected layer produced by shot peening,” Second International Conference on Shot Peening, Chicago, USA, pp. 217–227.
Edberg J., Lindgren L., and Mori K., 1995, “Shot peening simulated by two different finite element formulations,” Simulation of Materials Processing: Theory, Methods and Applications, edited by Shen and Dawson, Balkema, Rotterdam, pp. 425–430.
Meguid,  S. A., Shagal,  G., Stranart,  J. C., and Daly,  J., 1999, “Three-dimensional dynamic finite element analysis of shot-peening induced residual stresses,” Finite Elem. Anal. Design, 31, pp. 179–191.
Meguid,  S. A., Shagal,  G., and Stranart,  J. C., 1999, “Finite element modelling of shot-peening residual stresses,” Mater. Processing Technol., 92-93, pp. 401–404.
Schiffner,  K., and Droste gen. Helling,  C., 1999, “Simulation of residual stresses by shot peening,” Comput. Struct., 72, pp. 329–340.
Meguid,  S. A., Shagal,  G., and Stranart,  J. C., 2002, “3D FE analysis of peening of strain-rate sensitive materials using multiple impingement model,” Int. J. Impact Eng., 27, pp. 119–134.
Mattson,  R. L., and Colemal,  W. S., 1954, “Effect of shot-peening variables and residual stresses on fatigue life of leaf spring specimens,” Trans. Soc. Automotive Eng., 62, pp. 546–556.
Morrow, J., and Sinclair, G. M., 1958, “Cycle-dependent stress relaxation,” Symposium on Basic Mechanisms of Fatigue, ASTM STP 237, American Society for Testing and Materials.
James, M. R., 1982, “The relaxation of residual stresses during fatigue. Residual stress and stress relaxation,” edited by Kula, E., Weiss, V., in Proceedings of the 28th Army Materials Research Conference, Plenum Press, New York, pp. 297–314.
Jhansale H. R., and Topper T. H., 1973, “Engineering analysis of the inelastic stress response of a structural metal under variable cyclic strains,” Cyclic Stress-strain Behavior-Analysis, Experimentation, and Failure Prediction, American Society for Testing and Materials, pp. 246–270.
Kodama, S., 1972, “The behavior of residual stress during fatigue stress cycles,” in Proceedings of the International Conference on Mechanical Behavior of Metals II, Society of Material Science, Kyoto, 2, pp. 111–118.
Iida,  K., Yamamoto,  S., and Takanashi,  M., 1997, “Residual stress relaxation by reversed loading,” Weld. World, 93(3), pp. 138–144.
Holzapfel,  H., Schulze,  V., Vöhringer,  O., and Macherauch,  E., 1998, “Residual stress relaxation in an AISI 4140 steel due to quasistatic and cyclic loading at higher temperatures,” Mater. Sci. Eng., A, 248, pp. 9–18.
Torres,  M. A. S., and Voorwald,  H. J. C., 2002, “An evaluation of shot peening, residual stress and stress relaxation on the fatigue life of AISI 4340 steel,” Int. J. Fatigue, 24, pp. 877–886.
Smith,  D. J., Farrahi,  G. H., Zhu,  W. X., and McMahon,  C. A., 2001, “Experimental measurement and finite element simulation of the interaction between residual stresses and mechanical loading,” Int. J. Fatigue, 23, pp. 293–302.
Zhuang,  W. Z., and Halford,  G. R., 2001, “Investigation of residual stress relaxation under cyclic load,” Int. J. Fatigue, 23, pp. S31–S37.
ANSYS, 2002, User’s manual, Ver. 6.1, ANSYS Inc.
Everett, R. Jr., Newman, J. Jr., and Phillips, E., 1999, “On the effects of a machining-like scratch on the fatigue life of 4340 steel,” in Proceedings of the 55th Ann. Forum of the Amer. Helicopter Society, Montreal, Quebec, 1, pp. 316–327.
Premack,  T., and Douglas,  A. S., 1995, “Three-dimensional analysis of the impact fracture of 4340 steel,” Int. J. Solids Struct., 32(17-18), pp. 2793–2812.
Batra,  R. C., Zhang,  X., and Wright,  T. W., 1995, “Critical strain ranking of 12 materials in deformations involving adiabatic shear bands,” Trans. ASME, J. Appl. Mech., 62, pp. 252–254.
Lee,  W. S., and Yeh,  G. W., 1997, “The plastic deformation behavior of AISI 4340 alloy steel subjected to high temperature and high strain rate loading conditions,” J. Mater. Process. Technol., 71, pp. 224–234.
Bodner,  S. R., and Symonds,  P. S., 1979, “Experiments on dynamic plastic loading of frames,” Int. J. Solids Struct., 15, pp. 1–13.
Chaboche,  J. L., and Jung,  O., 1998, “Application of a kinematic hardening viscoplasticity model with thresholds to the residual stress relaxation,” Int. J. Plast., 13(10), pp. 785–807.
Kobayashi,  M., and Nobutada,  O., 2002, “Implementation of cyclic plasticity models based on a general form of kinematic hardening,” Int. J. Numer. Methods Eng., 53, pp. 2217–2238.

Figures

Grahic Jump Location
FE model of multiple impingements of multiple shots with subsequent cyclic loading: (a) full model, and (b) discretized symmetry cell
Grahic Jump Location
Typical triangular cyclic loading with different R-ratios
Grahic Jump Location
Stress–strain relationship for AISI 4340 steel: (a) quasistatic uniaxial stress–strain curves for different temperatures, and (b) the normalized effective yield stress σyy0 accounted for strain-rate sensitivity
Grahic Jump Location
Comparison between experimental data 20 and FE prediction: (a) residual stress relaxation at the specimen top surface for different applied surface stress magnitudes, and (b) residual stress relaxation at the top and bottom surfaces for applied surface stress magnitude of 700 MPa
Grahic Jump Location
Residual stress contours in peened target for three consecutive stages: (a) after peening, (b) for the first loading cycle at the maximum normalized applied stress σmaxy=1.57, and (c) after first unloading
Grahic Jump Location
Residual stress relaxation time history during triangular cyclic loading
Grahic Jump Location
Residual stress relaxation for triangular applied cyclic stress: (a) versus number of cycles for a point 156 μm beneath the target surface, and (b) versus depth after 30 cycles
Grahic Jump Location
Effect of R-ratio σminmax of applied cyclic stress upon residual stress distribution after 30 cycles
Grahic Jump Location
Effect of peening velocity upon residual stress distribution for triangular applied cyclic stress: (a) after peening before applied cyclic loading, and (b) after 30 cycles
Grahic Jump Location
Effect of material hardening model upon residual stress relaxation for different R-ratios and for the maximum applied cyclic stress σmaxy=1.57
Grahic Jump Location
Residual stress relaxation for cyclic thermal and combined loadings: (a) versus number of cycles for a point 156 μm beneath the target surface, and (b) versus depth after 30 cycles
Grahic Jump Location
Effect of phase shift between mechanical and thermal loadings upon residual stress relaxation after 30 cycles

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In