High Frequency Fatigue Crack Propagation in the Nickel-Base Superalloy KM4 at High Temperatures-Reference-Cited by-同舟云学术

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High Frequency Fatigue Crack Propagation in the Nickel-Base Superalloy KM4 at High Temperatures

Published:2013-10-04 Issue: Volume: Page:8-15
ISSN:
Container-title:Fatigue and Fracture Behavior of High Temperature Materials
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Author:

Shyam A.,Padula S.A.,Milligan W.W.

Publisher

John Wiley & Sons, Inc.

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1002/9781118787823.ch2/fullpdf

Reference18 articles.

1. High cycle fatigue in aircraft gas turbines- an industry perspective;Cowles;International Journal of Fracture,1996

2. High frequency fatigue crack propagation behavior of a nickel-base turbine disk alloy;Padula II;International Journal of Fatigue,1999

3. Thresholds for high-cycle fatigue in a turbine engine Ti-6Al-4V alloy;Ritchie;International Journal of Fatigue,1999

4. D.D. Krueger et al, US Patent 5143563, September 1, 1992

5. S. Sinharoy “Deformation behavior of two nickel-base turbine disk alloys at 650°C,” Metall. Mater. Transactions A, in review

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