Relationship between Microstructure and Fatigue Properties of Forged Ti–5Al–2Sn–2Zr–4Mo–4Cr for Aircraft Applications-Reference-Cited by-同舟云学术

Relationship between Microstructure and Fatigue Properties of Forged Ti–5Al–2Sn–2Zr–4Mo–4Cr for Aircraft Applications

Published:2020-10-01 Issue:10 Volume:61 Page:2017-2024
ISSN:1345-9678
Container-title:MATERIALS TRANSACTIONS
language:en
Short-container-title:Mater. Trans.

Author:

Tanaka Saki¹,Akahori Toshikazu²,Niinomi Mitsuo²³⁴⁵⁶,Nakai Masaaki⁷

Affiliation:

1. Graduate School of Science and Technology, Meijo University

2. Faculty of Science and Technology, Meijo University

3. Institute for Materials Research, Tohoku University

4. Department of Materials and Manufacturing Science, Graduate School of Engineering, Osaka University

5. Institute of Materials and Systems for Sustainability, Nagoya University

6. Faculty of Chemistry, Materials and Bioengineering, Kansai University

7. Faculty of Science and Technology, Kinki University

Publisher

Japan Institute of Metals

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Link

https://www.jstage.jst.go.jp/article/matertrans/61/10/61_MT-M2020184/_pdf

Reference11 articles.

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2. 2) S. Nishikiori: J. JILM 55 (2005) 557–560.

3. 3) R. Boyer, G. Welsch and E.W. Collings: Materials Properties Handbook Titanium Alloys, (The Materials Information Society, America, 1994) pp. 453–463.

4. 4) M.J. Donachie, Jr.: Titanium A Technical Guide Second Edition, (The Materials Information Society, America, 2000) pp. 195–198.

5. 5) M. Niinomi, T. Akahori, M. Nakai, Y. Koizumi, A. Chiba, T. Nakano, T. Kakeshita, Y. Yamabe-Mitarai, S. Kuroda, N. Motohashi, Y. Itsumi and T. Choda: Mater. Trans. 60 (2019) 1740–1748.

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