Fatigue crack propagation behaviour of a nickel based superalloy at elevated temperatures-Reference-Cited by-同舟云学术

Fatigue crack propagation behaviour of a nickel based superalloy at elevated temperatures

Published:2014-07 Issue:sup4 Volume:18 Page:S4-1087-S4-1090
ISSN:1432-8917
Container-title:Materials Research Innovations
language:en
Short-container-title:Materials Research Innovations

Author:

Wang L.¹,Huang X.¹,Guo G.¹,Hu Y.²,Zhang L.¹

Affiliation:

1. AVIC Beijing Institute of Aeronautical Materials Beijing Key Laboratory of Aeronautical Materials Testing and EvaluationScience and Technology on Advanced High Temperature Structural Materials Laboratory, ZHONGHANG Testing Innovation Cooperation, Beijing 100095, China

2. MTS Systems CorporationEden Prairie, MN 55344, USA

Publisher

Informa UK Limited

Subject

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

Link

https://www.tandfonline.com/doi/pdf/10.1179/1432891714Z.000000000863

Reference13 articles.

1. Fatigue of Structures and Materials

2. Developing Damage Tolerance and Creep Resistance in a High Strength Nickel Alloy for Disc Applications

3. The effect of hold-time on fatigue crack growth behaviors of WASPALOY alloy at elevated temperature

4. Gas phase embrittlement and time dependent cracking of nickel based superalloys

Cited by 2 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. A novel laser-EMAT ultrasonic longitudinal wave resonance method for wall thickness measurement at high temperatures;Ultrasonics;2024-07

2. Testing and evaluation for fatigue crack propagation of Ti-6Al-4V/ELI and 7050-T7452 alloys at high temperatures;Chinese Journal of Aeronautics;2018-06