Effect of mean stress (stress ratio) and aging on fatigue-crack growth in a metastable beta titanium alloy, Ti-10V-2Fe-3Al

The effect of mean stress, or the stress ratio (R), on the fatigue-crack growth (FCG) behavior of α-aged and ω-aged microstructures of the beta titanium alloy Ti-10V-2Fe-3Al was investigated. While the mean stress had a negligible effect on the FCG behavior of the α-aged microstructure, a strong effect was observed in the ω-aged microstructure. In particular, the values of the threshold stress-intensity range (ΔKth) exhibited a strong dependence on R in the ω-aged microstructure, while this dependence was weak in the α-aged microstructure. These effects seem to arise primarily from fracture-surface roughness-induced crack closure. The crack closure levels for the α-aged microstructure were found to be very low compared to those for the ω-aged microstructure. Transmission electron microscopy and scanning electron microscopy studies of microstructures and fracture surfaces were performed to gain insight into the deformation characteristics and crack propagation mechanisms, respectively, in these microstructures. The microstructure-induced differences in FCG behavior are rationalized in terms of the effect of aging on slip and crack closure.

[1]  Y-W. Kim,et al.  Microstructure/property relationships in titanium aluminides and alloys , 1990 .

[2]  K. Ravichandran A theoretical model for roughness induced crack closure , 1990 .

[3]  Rodney R. Boyer,et al.  Issues in the development of beta titanium alloys , 1994 .

[4]  T. W. Duerig,et al.  Microstructural influences on fatigue crack propagation in Ti-10V-2Fe-3Al , 1985 .

[5]  W. Soboyejo,et al.  An investigation of the effects of stress ratio and crack closure on the micromechanisms of fatigue crack growth in Ti-6Al-4V , 1997 .

[6]  P. Irving,et al.  The effect of air and vacuum environments on fatigue crack growth rates in Ti-6Al-4V , 1974, Metallurgical and Materials Transactions B.

[7]  G. Yoder,et al.  Observations on microstructurally sensitive fatigue crack growth in a widmanstätten Ti-6Al-4V alloy , 1977 .

[8]  F. Erdogan Fracture Mechanics: 25th Volume , 1995 .

[9]  T. W. Duerig,et al.  Phase transformations and tensile properties of Ti-10V-2Fe-3AI , 1980 .

[10]  Rodney R. Boyer,et al.  Practical Considerations for Manufacturing High-Strength Ti-10V-2Fe-3A1 Alloy Forgings , 1979 .

[11]  Subra Suresh,et al.  Fatigue crack growth threshold concepts , 1984 .

[12]  K. Sadananda,et al.  Analysis of Fatigue Crack Closure and Thresholds , 1995 .

[13]  J. Williams,et al.  The ω-phase as an example of an unusual shear transformation , 1973 .

[14]  J. Williams,et al.  The omega phase transformation in titanium alloys as an example of displacement controlled reactions , 1971 .

[15]  P. Liaw Overview of Crack Closure at Near-Threshold Fatigue Crack Growth Levels , 1988 .

[16]  Rodney R. Boyer,et al.  Design Properties of a High-Strength Titanium Alloy, Ti-10V-2Fe-3Al , 1980 .

[17]  K. Minakawa,et al.  On crack closure in the near-threshold region , 1981 .

[18]  G. Leverant,et al.  Correlations between fracture surface appearance and fracture mechanics parameters for stage II fatigue crack propagation in TÏ-6AI-4V , 1974 .

[19]  T. W. Duerig,et al.  Microstructure, tensile deformation, and fracture in aged ti 10V-2Fe-3Al , 1983 .

[20]  J. Newman,et al.  Mechanics of Fatigue Crack Closure , 1988 .

[21]  Y. Ohmori,et al.  Effects of ω Phase Formation on Decomposition of α″⁄β Duplex Phase Structure in a Metastable β Ti Alloy , 1998 .

[22]  Subra Suresh,et al.  Crack deflection: Implications for the growth of long and short fatigue cracks , 1983 .

[23]  M. Niinomi,et al.  Toughness and Strength of Microstructurally Controlled Titanium Alloys , 1991 .

[24]  Rodney R. Boyer,et al.  Processing properties relationships of Ti-10V-2Fe-3Al , 1987 .

[25]  B. S. Hickman The formation of omega phase in titanium and zirconium alloys: A review , 1969 .