Estimation of the fatigue crack initiation site and life of Ti-6Al-4V alloy for two types of circle and slender crystal grains-Reference-Cited by-同舟云学术

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Estimation of the fatigue crack initiation site and life of Ti-6Al-4V alloy for two types of circle and slender crystal grains

Published:2024-04 Issue: Volume:181 Page:108097
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Arakawa Jinta,Kawahara Yuya,Kimura Yukihiko^ORCID,Hashimoto Shotaro^ORCID,Akebono Hiroyuki,Sugeta Atsushi^ORCID

Publisher

Elsevier BV

Reference21 articles.

1. Additively manufactured Ti-6Al-4V replacement parts for military aircraft;Jones;Int J Fatigue,2019

2. M. Nagentrau, A. L. Mohd Tobi, S. Jamian, Y. Otsuka, R. Hussin. Delamination-fretting wear failure evaluation at HAp-Ti-6Al–4V interface of uncemented artificial hip implant. J. Mech. Behav. Biomed. 2021 October;(122):104657.

3. A critical review on additive manufacturing of Ti-6Al-4V alloy: microstructure and mechanical properties;Nguyen;J Mater Res Tech,2022

4. Microstructure and tensile properties of additive manufactured Ti-6Al-4V with refined prior-β grain structure obtained by rapid heat treatment;Zou;Mater Sci Eng A,2021

5. Tensile properties prediction by multiple linear regression analysis for selective laser melted and post heat-treated Ti-6Al-4V with microstructural quantification;Kusano;Mater Sci Eng A,2020

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. Investigation of micro-mechanisms for facet formation during dwell fatigue in Ti6321 alloy with equiaxed microstructure;International Journal of Fatigue;2025-01

2. Experimental and Analytical Study of Directional Isothermal Fatigue in Additively Manufactured Ti-TiB Metal Matrix Composites;Metals;2024-03-29

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