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Authors
Li, Huitao
Wang, Zhineng https://orcid.org/0000-0001-9177-0243
Bin, Guangfu
Tian, Jing
Chen, Renzhen
Tran, Cong Trieu
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Funding
Funding for this research was provided by:
the Natural Science Foundation of Hunan Province, China (No. 2023JJ30258, No. 2023JJ50018)
the Key Lab of Advanced Measurement and Test Technology for Aviation Propulsion System, Liaoning Province (No. AMTAPS202301)
the Hunan Provincial Graduate Student Innovation Program (No. CX20240870)
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Article History
Received: 30 July 2024
Revised: 17 December 2024
Accepted: 19 December 2024
First Online: 3 January 2025
