@inproceedings{21ccf158e0af4db8b435cf61227d4ddc,
title = "CFD analysis of ducted-fan UAV based on Magnus effect",
abstract = "Uninhabited Aerial Vehicle(UAV) has been developed quickly for decades and a new kind of VTOL(Vertical Take-Off and Landing)UAV which is called Ducted-Fan Uninhabited Aerial Vehicle attracts more and more attention. This paper presents a new structure of the ducted-fan UAV. In this vehicle, the actuator system consists of four rotary cylinders which are symmetrically installed at bottom of inside duct. The force used for attitude stabilization is generated by the interaction between the surface of cylinder and the downwash, which is known as Magnus effect. In this paper, the aerodynamic characteristics of propeller-wing interaction for the ducted fan UAV were simulated numerically based on the Computational Fluid Dynamics (CFD) by means of sliding mesh technology.",
keywords = "CFD, Ducted-fan UAV, Magnus effect",
author = "Jie Zhao and Qingming Hou and Hongzhe Jin and Yanhe Zhu and Ge Li",
year = "2012",
doi = "10.1109/ICMA.2012.6284396",
language = "英语",
isbn = "9781467312776",
series = "2012 IEEE International Conference on Mechatronics and Automation, ICMA 2012",
pages = "1722--1726",
booktitle = "2012 IEEE International Conference on Mechatronics and Automation, ICMA 2012",
note = "2012 9th IEEE International Conference on Mechatronics and Automation, ICMA 2012 ; Conference date: 05-08-2012 Through 08-08-2012",
}