A critical assessment of the mechanistic aspects in HAYNES 188 during low-cycle fatigue in the range 25 °C to 1000 °C-Reference-Cited by-同舟云学术

A critical assessment of the mechanistic aspects in HAYNES 188 during low-cycle fatigue in the range 25 °C to 1000 °C

Published:1997-02 Issue:2 Volume:28 Page:347-361
ISSN:1073-5623
Container-title:Metallurgical and Materials Transactions A
language:en
Short-container-title:Metall and Mat Trans A

Author:

Sankara Rao K. Bhanu,Castelli M. G.,Allen G. P.,Ellis John R.

Publisher

Springer Science and Business Media LLC

Subject

Metals and Alloys,Mechanics of Materials,Condensed Matter Physics

Link

http://link.springer.com/content/pdf/10.1007/s11661-997-0137-z.pdf

Reference52 articles.

1. Haynes Alloy 188, Report-Haynes International, Inc., Kokomo, In, 1991.

2. G.R. Halford, J.F. Saltsman, and S. Kalluri: High Temperature Fatigue Behavior of Haynes 188, Proc. Advanced Earth-to-Orbit Propulsion Technology Conf., MSFC, Huntsville, AL, May 10–13, 1988, NASA CP-3012, R.J. Richmond and S.T. Wu, eds., NASA, Washington, DC, 1988, pp. 497–507.

3. D.L. Klarstorm and G.Y. Lai: in Superalloys 1988, S. Reichman, D.N. Duhl, G. Maurer, S.D. Antolovich, and C. Lund, eds., TMS, Warrendale, PA, 1988, pp. 585–94.

4. G.R. Halford, M.J. Verrilli, S. Kalluri, F.J. Ritzert, R.E. Duckert, and F.A. Holland: ASTM STP 1122, Philadelphia, PA, 1992, pp. 120–42.

5. S. Kalluri and G.R. Halford: ASTM STP, ASTM, Philadelphia, PA, 1993, vol. 1186, pp. 120–42.

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