Probabilistic Life of DA718 for Aircraft Engine Disks-Reference-Cited by-同舟云学术

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Probabilistic Life of DA718 for Aircraft Engine Disks

Published:2005 Issue: Volume: Page:
ISSN:
Container-title:Superalloys 718, 625, 706 and Various Derivatives (2005)
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Author:

Deyber S.,Alexandre F.,Vaissaud J.,Pineau A.

Publisher

TMS

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. The Influence of Temperature and Stress Cycle Asymmetry at Fatigue Cracks Initiation and Propagation in Cylindrical Specimens of Ni-based Alloy EP741NP;Procedia Structural Integrity;2019

2. Production of Nitride-Free 718 by the VIM-VAR Processing Route;Proceedings of the 9th International Symposium on Superalloy 718 & Derivatives: Energy, Aerospace, and Industrial Applications;2018

3. Crack initiation sensitivity of wrought direct aged alloy 718 in the very high cycle fatigue regime: the role of non-metallic inclusions;Materials Science and Engineering: A;2016-12

4. Probabilistic approaches to fatigue with special emphasis on initiation from inclusions;International Journal of Fatigue;2016-12

5. Strain rate and oxidation effects on crack initiation at 600 and 650 °C in a nickel-based superalloy;Materials at High Temperatures;2016-04-13

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