Mechanistic Model to Predict Statistical Scatter in Fatigue Response of Titanium Aluminide
Author:
Affiliation:
1. Sr. Devel. Engr., VEXTEC Corp., 116 Wilson Pike, Brentwood, TN 37027.
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282001%2914%3A4%28120%29
Reference17 articles.
1. Balsone S. J. Worth B. D. Larsen J. M. and Jones J. W. ( 1995). “Fractographic study of fatigue crack growth process in fully lamellar γ-TiAl alloy.” Scripta Metallurgica et Materialia 32(10) 1653–1658.
2. Hall E. O. ( 1951). Proc. Phys. Soc. 64B 747.
3. Kad B. K. Ming D. and Asaro R. J. ( 1995). “Numerical simulations of stress-strain behavior in two-phase α 2 + γ lamellar TiAl alloys.” Mat. Sci. Engrg. A192/193 97–103.
4. Kruzic J. J. Campbell J. P. and Ritchie R. O. ( 1999). “On the fatigue behavior of γ-based titanium aluminides: Role of small cracks.” Acta mater 47(3) 801–816.
5. Larsen J. M. et al. ( 1999a). . “The role of near-threshold small-crack behavior in life prediction of titanium alloys for use in advanced turbine engines.” Small fatigue cracks: Mechanics and mechanisms K. S. Ravichandran R. O. Ritchie and Y. Murakami eds. Elsevier Science Oxford U.K.
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