Application of ultrasonic fatigue technology in very-high-cycle fatigue testing of aviation gas turbine engine blade materials: A review
Crossref DOI link: https://doi.org/10.1007/s11431-023-2556-1
Published Online: 2024-04-26
Published Print: 2024-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zhao, JiuCheng
Wan, Jie
Zhang, ShiZhong
Yan, ChuLiang
Zhao, HongWei
Text and Data Mining valid from 2024-04-26
Version of Record valid from 2024-04-26
Article History
Received: 6 June 2023
Accepted: 20 November 2023
First Online: 26 April 2024