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共轴式双旋翼诱导速度的PIV水洞试验研究
引用本文:胡增龙,邓彦敏.共轴式双旋翼诱导速度的PIV水洞试验研究[J].飞机设计,2008,28(1):10-15.
作者姓名:胡增龙  邓彦敏
作者单位:北京航空航天大学,航空科学与工程学院,北京,100083
摘    要:采用PIV(粒子图像测速)技术,对共轴式双旋翼在悬停和以不同速度前飞时的流场进行水洞试验,测量得到旋翼流场的速度和涡量分布,主要研究了共轴式双旋翼流场的垂向诱导速度沿径向的分布规律。为了比较,对单旋翼也进行了测量。试验结果对共轴式直升机的气动计算和合理设计具有重要意义。

关 键 词:共轴式直升机  旋翼流场  诱导速度  水洞  PIV
文章编号:1673-4599(2008)01-0010-06
收稿时间:2007-08-06
修稿时间:2008-01-10

Experimental Investigation of Coaxial-Rotor Induced Velocity in Water Tunnel Using PIV
HU Zeng-long,DENG Yan-min.Experimental Investigation of Coaxial-Rotor Induced Velocity in Water Tunnel Using PIV[J].Aircraft Design,2008,28(1):10-15.
Authors:HU Zeng-long  DENG Yan-min
Institution:HU Zeng-long, DENG Yan-min (School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China)
Abstract:Particle Image Velocimetry technique is applied to the experiment of coaxial-rotor in hover and in level flight in water tunnel.Velocity vectors and vortex contours of the rotor flow fields are measured.The radial distribution of vertical induced velocity of coaxial-rotor flow fields is mainly investigated.For comparison,single-rotor is also measured.The experimental results have important meaning to the aerodynamic calculation and reasonable design of coaxial-rotor helicopter.
Keywords:coaxial helicopter  rotor flow fields  induced velocity  water tunnel  PIV
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