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兵工学报 ›› 2018, Vol. 39 ›› Issue (6): 1225-1232.doi: 10.3969/j.issn.1000-1093.2018.06.024

• 论文 • 上一篇    下一篇

小型共轴旋翼自然来流下的抗风扰气动特性分析

雷瑶, 纪玉霞   

  1. (福州大学 机械工程及自动化学院, 福建 福州 350116)
  • 收稿日期:2017-08-18 修回日期:2017-08-18 上线日期:2018-07-29
  • 作者简介:纪玉霞(1991—),女,硕士研究生。E-mail:fzu_yuxiaji@163.com
  • 基金资助:
    国家自然科学基金项目(51505087)

Aerodynamic Characteristics of Small Coaxial Rotor Considering the Wind Gust

LEI Yao, JI Yu-xia   

  1. (School of Mechanical Engineering and Automation, Fuzhou University, Fuzhou 350116, Fujian, China)
  • Received:2017-08-18 Revised:2017-08-18 Online:2018-07-29

摘要: 针对自然环境中的二级风(1.6~3.3 m/s)和三级风(3.4~5.4 m/s),对悬停状态的共轴双旋翼进行水平和竖直来流的抗风扰气动性能测试。在建立自然来流影响下的桨叶速度分布模型基础上,采用低速风洞模拟自然环境对共轴双旋翼进行了来流吹风试验。采用滑移网格方法计算旋翼流场,捕捉自然来流环境中流场内部的气动干扰现象,主要包括桨尖压强分布、流线分布和桨尖速度矢量。研究结果表明:所建立的模拟方法能够准确反映自然来流对共轴双旋翼流场气动特性影响;相比无来流状态,受竖直来流影响的共轴旋翼性能下降,而水平来流环境中的共轴旋翼具有较好的抗风扰性能,旋翼性能随着水平来流速度的增大而大幅度提高。

关键词: 共轴旋翼, 自然来流, 气动干扰, 风洞试验, 滑移网格

Abstract: The wind resistance of coaxial rotors in hover is tested considering the horizontal and vertical light breezes with the wind velocity varied from 1.6 to 3.3 m/s and the gentle breeze with the wind velocity varied from 3.4 to 5.4 m/s in the natural environment. A velocity distribution model of blade in the natural incoming flow is established, and a low-speed wind tunnel is also introduced to simulate the natural disturbance on the coaxial rotors. The sliding mesh method is adopted to calculate the flow field and capture the aerodynamic interference in the natural incoming flow, mainly including the distribution of tip pressure, the streamline distribution of flow field and the velocity vector of blade tip. Results show that the proposed simulation method can accurately reflect the influence of natural incoming flow on the aerodynamic characteristics of coaxial rotors. Compared to the case with no wind gust, the performance of coaxial rotors is declined due to vertical incoming flow. It is noted that the coaxial rotors can effectively resist the wind disturbance in the horizontal incoming flow, and eventually the rotor performance is greatly improved with the increase in wind velocity.Key

Key words: coaxialrotor, naturalwindgust, aerodynamicinterference, windtunneltest, slidingmesh

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