Funding for this research was provided by:
This work was supported by the Strategic Priority Research Program of the Chinese Academy of Sciences (Grant No. XDC04000000)
the National Natural Science Foundation of China (Grant No. 62073312)
the Key Research and Development Program of LiaoNing (Grant No. 2020JH2/10100023)
China Aero-engine Independent Innovation Special Fund Project (Grant No. ZZCX-2018-035)
Article History
Accepted: 24 November 2021
First Online: 10 January 2022
Declarations
:
: The authors declare that they have no conflict of interest.