Rotor Performance Analysis and Modeling of Multirotor Using Wind-Tunnel Test

科研成果: 书/报告/会议事项章节会议稿件同行评审

6 引用 (Scopus)

摘要

In this study, the performance characteristics of a rotor used for multirotor are investigated through wind-tunnel tests. The rotor is tested at several flow speeds and angles to approximate the actual flying condition. A high resolution six-axis force/moment sensor is utilized to record the forces and moments in three directions. Wind tunnel results show the changes in the rotor performance with the variation in flying speed, flying angle, and rotor revolution. The results also demonstrate that the aerodynamic characteristics of the rotor quite differ from those in the hovering state when the vehicle is flying forward. Finally, aerodynamic models of the rotor in forward state are provided.

源语言英语
主期刊名2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
出版商Institute of Electrical and Electronics Engineers Inc.
1644-1649
页数6
ISBN(电子版)9781728142777
DOI
出版状态已出版 - 9月 2020
活动2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020 - Athens, 希腊
期限: 1 9月 20204 9月 2020

出版系列

姓名2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020

会议

会议2020 International Conference on Unmanned Aircraft Systems, ICUAS 2020
国家/地区希腊
Athens
时期1/09/204/09/20

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