Chinese Journal of Aeronautics
 2019
DOI: 10.1016/j.cja.2019.01.015
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Effects of blade aspect ratio and taper ratio on hovering performance of cycloidal rotor with large blade pitching amplitude

Yu Hu
1
,
Xuyang Fu
2
,
Hailang Zhang
3
et al.
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Cited by 8 publications
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