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Surface Engineering Volume 29, 2013 - Issue 8
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Original Article

Distribution of residual stress fields in TC6 blade by LSP

Y W Fang Air Force Engineering UniversityXi’an710077, ChinaCorrespondence[email protected]
,
S H Zhao Air Force Engineering UniversityXi’an710077, China
,
Y Wang Air Force Engineering UniversityXi’an710077, China
,
J Sun Air Force Engineering UniversityXi’an710077, China
&
P Y LiXi’an University of Technology, Xi’an710048, China
Pages 608-615 | Received 15 Mar 2013, Accepted 24 Jun 2013, Published online: 03 Dec 2013

Citations (5)

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Read on this site (1)

J. Arakawa, M. Kakuta, Y. Hayashi, R. Tanegashima, H. Akebono, M. Kato & A. Sugeta. (2014) Fatigue strength of USP treated ASTM CA6NM for hydraulic turbine runner. Surface Engineering 30:9, pages 662-669.
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Articles from other publishers (4)

Yingwu Fang. (2021) Strengthening Effects of the Laser Light Impact on a TC17 Blade in View of Simulations and Experiments. Journal of Russian Laser Research 42:3, pages 328-339.
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M Ayeb, M Frija & R Fathallah. (2019) Influence of multiple laser impacts on thin leading edges of turbine blade. Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 234:1, pages 130-143.
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G Ranjith Kumar, G Rajyalakshmi & S Swaroop. (2019) A critical appraisal of laser peening and its impact on hydrogen embrittlement of titanium alloys. Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture 233:13, pages 2371-2398.
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Pengyang Li, Shikun Huang, Haifeng Xu, Yuxi Li, Xiaoli Hou, Quandai Wang, Weiping Fu & Yingwu Fang. (2015) Numerical simulation and experiments of titanium alloy engine blades based on laser shock processing. Aerospace Science and Technology 40, pages 164-170.
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