Effects of blade aspect ratio and taper ratio on hovering performance of cycloidal rotor with large blade pitching amplitude

Autor: HU, Yu, FU, Xuyang, ZHANG, Hailang, WANG, Gengqi, FARHAT, Hussain
Zdroj: In Chinese Journal of Aeronautics May 2019 32(5):1121-1135
Databáze: ScienceDirect