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Authors
Li, Zhanwei
Tian, Xinliang
Wen, Binrong
Ma, Hui
Ding, Weimin
Song, Hetao
Wang, Linqiao
Peng, Zhike
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Funding
Funding for this research was provided by:
National Key Laboratory of Science and Technology on Helicopter Transmission (HTL-A-21G08)
Key Laboratory of Vibration and Control of Aero-Propulsion System, Ministry of Education, Northeastern University (VCAME202201)
National Natural Science Foundation of China (52205108)
National Natural Science Foundation of China (12102251)
Natural Science Foundation of Jiangsu Province of China (BK20220897)
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Article History
Received: 27 March 2023
Revised: 10 May 2023
Accepted: 24 May 2023
First Online: 26 June 2023
Declarations
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: The author declared no potential conflicts of interest with respect to the research, authorship, and/or publication of this article. The author declares that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.
