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Authors
Zhang, Xiaochen
Li, Hanwen
Meng, Weiying
Liu, Yaofeng
Zhou, Peng
He, Cai
Zhao, Qingbo
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Funding
Funding for this research was provided by:
National Natural Science Foundation of China (Grant No. 52005352，62173238)
Key Laboratory of Vibration and Control of Aero-Propulsion System, Ministry of Education, Northeastern University (VCAME202007)
Open Fund of Key Laboratory of Fundamental Science for National Defense of Aeronautical Digital Manufacturing Process of Shenyang Aerospace University (SHSYS202107)
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Article History
Received: 11 April 2022
Accepted: 24 August 2022
First Online: 13 September 2022
Declarations
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: The authors declare that they have no conflicts of interest. This manuscript has not been published or presented elsewhere in part or in entirety and is not under consideration by another journal. We have read and understood your journal’s policies, and we believe that neither the manuscript nor the study violates any of these. There are no conflicts of interest to declare. The data of article permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
