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旋转状态下方形通道内部流场特性热线实验
引用本文:魏宽,陶智,邓宏武,李海旺.旋转状态下方形通道内部流场特性热线实验[J].航空动力学报,2016,31(11):2635-2640.
作者姓名:魏宽  陶智  邓宏武  李海旺
作者单位:1. 北京航空航天大学 能源与动力工程学院航空发动机气动热力国家级重点实验室, 北京 100191;
基金项目:国家自然科学基金(51541605)
摘    要:为了解决旋转条件下热线技术应用问题并且在此基础上精确测量旋转方形通道内部流场特性,搭建了用于旋转通道流场测试实验平台,采用了两种连线方式对热线进行了标定实验,获得了热线测量旋转通道内部平均速度的相对误差为±6%,对雷诺数和旋转数范围分别是5000~10000和0~0.222的旋转通道流场进行了测量,结果表明:旋转导致速度型整体向后缘面(Y/D=-0.5)偏转,X/D和旋转数越大,速度型偏转越明显;旋转数为0.222时,后缘面附近边界层速度型出现了一个拐点,可能与由哥氏力不稳定性引起的二次流有关. 

关 键 词:旋转通道    热线    接线方式    标定误差    平均速度
收稿时间:2015/10/9 0:00:00

Hot wire test on the flow fields in a rotating square channel
WEI Kuan,TAO Zhi,DENG Hong-wu and LI Hai-wang.Hot wire test on the flow fields in a rotating square channel[J].Journal of Aerospace Power,2016,31(11):2635-2640.
Authors:WEI Kuan  TAO Zhi  DENG Hong-wu and LI Hai-wang
Institution:1. National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics Astronautics, Beijing 100191, China;2. Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100191, China
Abstract:To apply the hot wire technique in rotation condition and accurately measure the flow fields in a rotating square channel, a rotating test rig was built.Two connection modes were applied in the hot wire calibration tests, and the relative error in measuring the averaged velocity was estimated to be ±6%. The measurements were conducted in a rotating channel with the Reynolds number and rotation number varying in the range of 5000-10000, and 0-0.222, respectively. The results show that there is a shift of the velocity profile to the trailing side(Y/D=-0.5), the drift of velocity profile increases with the bigger X/D and rotation number. When the rotation number is 0.222, there is a velocity profile inflection point near the trailing side that likely is related to the secondary flow induced by Coriolis force instability.
Keywords:rotating channel  hot wire  connection mode  calibration error  averaged velocity
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