Effects of blade aspect ratio and taper ratio on hovering performance of cycloidal rotor with large blade pitching amplitude
Hu, Yu, Fu, Xuyang, Zhang, Hailang, Wang, Gengqi, Farhat, HussainLanguage:
english
Journal:
Chinese Journal of Aeronautics
DOI:
10.1016/j.cja.2019.01.015
Date:
February, 2019
File:
PDF, 2.28 MB
english, 2019