Author:
Wang Weiqi,Cui Zhuangzhuang,Chen Xi,Zhao Qijun
Funder
National Natural Science Foundation of China
Reference37 articles.
1. A computational fluid dynamic acoustic investigation of a tiltwing eVTOL concept aircraft;Higgins;Aerospace Science Technolgy,2021
2. Reduction of helicopter blade-vortex interaction noise by active rotor control technology;Yu;Prog Aerosp Sci,1997
3. Numerical characterization of helicopter noise hemispheres;Gennaretti;Aerosp Sci Technol,2016
4. High-fidelity aerodynamic and acoustic design and analysis of a heavy-lift eVTOL;Zhang;Aerosp Sci Technol,2023
5. On the aerodynamic performance of redundant propellers for multi-rotor eVTOL in cruise;Zhang;Aerosp Sci Technol,2023