Development and Material Properties of Titanium Alloys for Aeroengine and Airframe Applications
Author:
Affiliation:
1. High Temperature Material Design Group, Research Center for Structural Materials, National Institute for Materials Science
Publisher
Japan Institute of Metals
Subject
General Medicine
Link
https://www.jstage.jst.go.jp/article/materia/55/8/55_55.370/_pdf
Reference26 articles.
1. (3) F. H. Froes: Titanium-Physical Metallurgy, Processing, and Applications, ASM International, Novelty, OH, (2015).
2. (4) P. J. Bania: JOM, 46(1994), 16-19.
3. (5) H. W. Rosenberg: The Science, Technology and Application of Titanium, ed. by R.I. Jaffee, N.E. Promisel, Pergamon Press, Oxford, UK, (1970), 851-859.
4. (6) K.-H. Rendings: Airbus and Current Aircrafts Metal Technologies, http://www.polishengineers.org/data/history_activities/18.pdf
5. (7) R. R. Boyer: JOM, 44(1992), 23-25.
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1. Relationship between Microstructure and Fatigue Properties of Forged Ti–5Al–2Sn–2Zr–4Mo–4Cr for Aircraft Applications;MATERIALS TRANSACTIONS;2020-10-01
2. Relationship between Microstructure and Fatigue Properties of Forged Ti-5Al-2Sn-2Zr-4Mo-4Cr for Aircraft Applications;Journal of the Japan Institute of Metals and Materials;2020-06-01
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