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水空两栖太阳能四旋翼气动特性研究
引用本文:阮永井,王琦,邹森,陈金铭.水空两栖太阳能四旋翼气动特性研究[J].航空工程进展,2019,10(5):728-734.
作者姓名:阮永井  王琦  邹森  陈金铭
作者单位:南昌航空大学 通航学院,南昌,330063;南昌航空大学 飞行器工程学院,南昌,330063
基金项目:江西省研究生创新基金(YC2018-S374)
摘    要:太阳能四旋翼无人机结合了太阳能飞行器和四旋翼飞行器的优点,已受到广泛关注,但由于太阳能板的存在,旋翼的安装高度和轴距会对整机的气动效能产生影响。通过基于粒子法格子玻尔兹曼技术的XFlowCFD软件,对太阳能四旋翼无人机的整机流场进行非定常数值模拟,并分析该飞行器的气动特性。结果表明:旋翼高度对整机升力的影响较小,旋翼的安装轴距越大整机的升力越大,其主要原因是轴距较小时,旋翼产生的下洗流冲击在太阳能板上,对整机产生气动干扰。

关 键 词:太阳能四旋翼  XFlowCFD  下洗流  升力  气动布局优化
收稿时间:2019/6/21 0:00:00
修稿时间:2019/9/5 0:00:00

Research on Aerodynamic Characteristics of New Solar Four-rotor
Ruan Yongjing,Wang Qi,Zou Sen and Chen Jinming.Research on Aerodynamic Characteristics of New Solar Four-rotor[J].Advances in Aeronautical Science and Engineering,2019,10(5):728-734.
Authors:Ruan Yongjing  Wang Qi  Zou Sen and Chen Jinming
Institution:School of Navigation,Nanchang Hangkong University,School of Navigation,Nanchang Hangkong University,School of Aircraft Engineering,Nanchang Hangkong University,School of Aircraft Engineering,Nanchang Hangkong University
Abstract:Due to the existence of solar panels, the installation height and wheelbase of the rotor have an impact on the aerodynamic performance of the whole machine. The non-constant constant value simulation of the flow field of the whole machine is carried out by XFlow software based on the particle method lattice Boltzmann technique. The simulation results show that the height of the rotor has little effect on the lift of the whole machine. The larger the installation wheelbase of the rotor is, the larger the lift of the whole machine is. The main reason is that when the wheelbase is small, the lower wash flow generated by the rotor impacts on the board. The whole machine produces pneumatic interference. According to the simulation results and the whole machine, the analysis shows that the best installation method of the rotor is half-wheelbase R=859mm and height H=55mm, and provides some reference for the design of similar aircraft in the future.
Keywords:solar four-rotor  numerical simulation  Xflow CFD  lower wash flow  lift  aerodynamic layout optimization
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