High cycle and very high cycle fatigue properties and microscopic crack growth modeling of Ti‐6.5Al‐3.5Mo‐1.5Zr‐0.3Si titanium alloy at elevated temperatures
Author:
Affiliation:
1. School of Mechanical Engineering Beijing Institute of Technology Beijing China
Funder
National Natural Science Foundation of China
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1111/ffe.13839
Reference73 articles.
1. Fatigue performance of laser shock peened Ti6Al4V and Al6061‐T6 alloys
2. Influence of processing parameters of selective laser melting on high‐cycle and very‐high‐cycle fatigue behaviour of Ti‐6Al‐4V
3. Influence of the volume content of α + β colonies on the very high cycle fatigue behavior of a titanium alloy
4. Effects of defects on fatigue behavior of TC17 titanium alloy for compressor blades: Crack initiation and modeling of fatigue strength
5. Anisotropic mechanical and fatigue behaviour of Inconel718 produced by SLM in LCF and high‐temperature conditions
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