Abstract
Several recent papers have demonstrated that dwell periods at peak stress can significantly reduce the number of cycles to failure in LCF tests on titanium alloys and can cause enhanced growth rates in fatigue crack propagation tests. In all cases cleavage or quasi-cleavage facet formation has been intimately linked with the dwell sensitive fatigue response. The present paper demonstrates that facets can also form during creep deformation at ambient temperatures and it proposes that the LCF dwell effect and facet formation under cyclic conditions is dependent on time dependent plastic strain accumulation. If hydrogen contributes to the failure process it is suggested this must be through an interaction with dislocations. The significance of the model for dwell sensitive fatigue crack propagation is discussed.
Similar content being viewed by others
References
D. W. Hoeppner:A Fractographic Analysis of Flaw Growth in a High Strength Titanium Alloy, Report, University of Missouri Columbia, 1975.
C. A. Stubbington and S. Pearson: RAE Technical Report 76040, RAE, Farnborough, Hants, UK, 1976.
C. A. Stubbington, S. Pearson, and T. S. Baker: RAE Technical Report 76147, RAE, Farnborough, Hants, UK, 1976.
P. J. Postans and R. H. Jeal:Dependence of Crack Growth Performance Upon Structure in β-Processed Titanium Alloys, Paper 9, Conference on Forging and Properties of Aerospace Materials, The Metals Society, Leeds, UK, January 1977.
D. Eylon and J. A. Hall:Met. Trans. A, 1977, vol. 8A, p. 981.
S. Pearson: RAE Technical Report 66204, RAE, Farnborough, Hants, UK, 1966.
B. Gross and J. E. Srawley:Stress Intensity Factors for Single Edge Notch Specimens in Bending or Combined Bending and Tension by Boundary Collocation of a Stress Function, NASA TN D-2603, 1965.
D. N. Williams:Met. Trans., 1974, vol. 5, p. 2351.
H. Margolin:Met. Trans. A, 1976, vol. 7A, p. 1233.
W. J. Evans:The Effect of Microstructure on Fatigue Crack Propagation in α+β Titanium Alloys, no. 20, p. 153, Practical Implications of Fracture Mechanisms, Series, 2, Institution of Metals, 1973.
W. J. Evans and A. W. Beale:Fatigue Crack Propagation in Wrought Titanium Alloys, Paper 8, Conference on Forging and Properties of Aerospace Materials, The Metals Society, Leeds, UK, January 1977.
W. J. Evans: Unpublished research, NGTE, Pyestock, Hanfs UK, 1974.
P. J. Bania and D. Eylon:Met. Trans. A., 1978, vol. 9A, p. 847.
N. E. Paton and R. A. Spurling:Met. Trans. A., 1976, vol. 7A, p. 1769.
I. W. Hall:Met. Trans. A, 1978, vol. 9A, p. 815.
I. W. Hall and C. HammondMater. Sci. Eng., 1978, vol. 32, p. 241.
D. McLean:Mechanical Properties of Metals, John Wiley and Sons Inc., 1962.
J. F. Knott:Fundamentals of Fracture Mechanics, Butterworth, London, 1973.
D. N. Williams:Mater. Sci. Eng., 1975, vol. 18, p. 149.
D. A. Meyn:Met. Trans., 1974, vol. 5, p. 2405.
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Evans, W.J., Gostelow, C.R. The effect of hold time on the fatigue properties of a β-processed titanium alloy. Metall Trans A 10, 1837–1846 (1979). https://doi.org/10.1007/BF02811727
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF02811727