Effect of Crystallographic Orientations on Stage I Fatigue Crack Propagation in a Ni-Base Single Crystal Superalloy
Author:
Affiliation:
1. Department of Mechanical Engineering, Tokyo Institute of Technology
2. Department of Mechanical & Control Engineering, Tokyo Institute of Technology
Publisher
Society of Materials Science, Japan
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science
Link
https://www.jstage.jst.go.jp/article/jsms/66/10/66_731/_pdf
Reference17 articles.
1. 1) R.C. Reed, “The Superalloys, Fundamentals and Applications”, Cambridge University Press, New York, (2006).
2. 2) H. Harada and M. Okazaki, “High temperature strength of Ni-based superalloys and coatings for advanced gas turbines”, Journal of the society materials science, Japan, Vol. 51, No. 7, pp. 836-842, (2002).
3. 3) H.L.Bernstein, T.S.Grant, R.C.McClung and J.M.Allen, “Prediction of thermal -mechanical fatigue life for gas turbine bladesin electric power generation.”, ASTM STP 1186, pp.212-238, (1993).
4. 4) R.B.Scarlin, “Fatigue Crack Propagation in a Directionally Solidified Nickel-base Alloy”, Metallurgical Transactions A, Vol.7A, pp.1535-1541, (1979).
5. 5) M. Okazaki, T.Tabata and S.Nohmi, “Intrinsic Stage I Crack Growth of Directionally-Solidified Ni-base Superalloys during Low-cycle Fatigue at Elevated Temperature”, Metallurgical Transactions A, Vol.21A, pp.2201-2209, (1990).
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