TY - GEN
T1 - Experimental and numerical study of flapping wing rotary MAV
AU - Wei, Xu
AU - Li, Daochun
AU - Jiaqi, Jiang
AU - Puxue, Tan
AU - Jinwu, Xiang
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/7/2
Y1 - 2017/7/2
N2 - In this paper, investigation was made into the design, experimental study and numerical analysis of a novel design for flapping wing rotary micro aerial vehicles (FWR-MAV). This novel design is applied on the RotorBee project which is the world's first FWR-MAV to achieve vertical take-off and landing untethered. Attention was firstly focused on the overall design and experiment of RotorBee prototype. In the experiment, the aerodynamic force produced by the flapping wing rotor including the aerodynamic has been measured through the test system. Then a numerical model containing the complete two wing with bionic shape, simplified from RotorBee, is used to analysis the motion and aerodynamic properties. The geometry and motion parameters of the model are measured from practical aircraft. The comparison shows a very good agreement between the experimental and numerical results. Improvement of the design can be made by using this numerical method.
AB - In this paper, investigation was made into the design, experimental study and numerical analysis of a novel design for flapping wing rotary micro aerial vehicles (FWR-MAV). This novel design is applied on the RotorBee project which is the world's first FWR-MAV to achieve vertical take-off and landing untethered. Attention was firstly focused on the overall design and experiment of RotorBee prototype. In the experiment, the aerodynamic force produced by the flapping wing rotor including the aerodynamic has been measured through the test system. Then a numerical model containing the complete two wing with bionic shape, simplified from RotorBee, is used to analysis the motion and aerodynamic properties. The geometry and motion parameters of the model are measured from practical aircraft. The comparison shows a very good agreement between the experimental and numerical results. Improvement of the design can be made by using this numerical method.
KW - MAV
KW - flapping wing rotary
KW - numerical method
UR - https://www.scopus.com/pages/publications/85050864566
U2 - 10.1109/ICUS.2017.8278311
DO - 10.1109/ICUS.2017.8278311
M3 - 会议稿件
AN - SCOPUS:85050864566
T3 - Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
SP - 23
EP - 28
BT - Proceedings of 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
A2 - Xu, Xin
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2017 IEEE International Conference on Unmanned Systems, ICUS 2017
Y2 - 27 October 2017 through 29 October 2017
ER -