Funding for this research was provided by:
National Natural Science Foundation of China (12072305)
Aeronautical Science Foundation of China (20200057068001)
Open Fund from the National Key Laboratory of Science and Technology on Aerodynamic Design and Research of China (614220121030202)
Article History
Received: 28 March 2022
Revised: 30 December 2022
Accepted: 30 December 2022
First Online: 18 January 2025
Declarations
:
: On behalf of all authors, the corresponding author states that there is no conflict of interest.