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基于激光多普勒原理的极低风速测量实验

徐大川 龙彦志 李玉栋

徐大川, 龙彦志, 李玉栋. 基于激光多普勒原理的极低风速测量实验[J]. 航空动力学报, 2020, 35(6): 1228-1237. doi: 10.13224/j.cnki.jasp.2020.06.013
引用本文: 徐大川, 龙彦志, 李玉栋. 基于激光多普勒原理的极低风速测量实验[J]. 航空动力学报, 2020, 35(6): 1228-1237. doi: 10.13224/j.cnki.jasp.2020.06.013
XU Dachuan, LONG Yanzhi, LI Yudong. Experiment of extremely low wind velocity measurement based on laser Doppler[J]. Journal of Aerospace Power, 2020, 35(6): 1228-1237. doi: 10.13224/j.cnki.jasp.2020.06.013
Citation: XU Dachuan, LONG Yanzhi, LI Yudong. Experiment of extremely low wind velocity measurement based on laser Doppler[J]. Journal of Aerospace Power, 2020, 35(6): 1228-1237. doi: 10.13224/j.cnki.jasp.2020.06.013

基于激光多普勒原理的极低风速测量实验

doi: 10.13224/j.cnki.jasp.2020.06.013

Experiment of extremely low wind velocity measurement based on laser Doppler

  • 摘要: 介绍了利用激光多普勒效应进行风速测量的原理及定点遥测原理,分析了探测气溶胶颗粒大小的要求,并以此搭建了一套极低风速测量系统。同时分析了系统的测速精度,以及安装角度对测量结果的影响。最后分别开展了转台实验、直线导轨实验和风洞实验,实验结果表明,该极低风速测量系统的测量误差基本可以控制在001 m/s以内,当风洞工作介质为未经处理的环境空气时,系统可以获得稳定可靠的信号,测量结果与高性能仪器十分接近。

     

  • [1] 中国气象局.地面气象观测规范[M].北京:气象出版社,2003.
    [2] 何云武.风向风速传感器的原理及其检测[J].四川气象,2004,24(1):40-42. HE Yunwu.Principle and detection of the wind sensor[J].Journal of Sichuan Meteorology,2004,24(1):40-42.(in Chinese)
    [3] 王晓蕾,郭俊,陈晓颖,等.两种测风仪的动态对比试验及分析[J].解放军理工大学学报(自然科学版),2014,15(3):283-289. WANG Xiaolei,GUO Jun,CHEN Xiaoying,et al.Introduction and analysis of dynamic comparison test between two wind sensors[J].Journal of PLA University of Science and Technology (Natural Science Edition),2014,15(3):283-289.(in Chinese)
    [4] ROBBINS B E.48-inch water tunnel turbulence level measurements with and without a honeycomb[R].State College,US:Pennsylvania State University,1977.
    [5] MAHER B A.A calibration of the preston tube in liquid flow systems[R].Wright-Patterson AFB,US:Air Force Institute of Technology,1980.
    [6] 戴昌晖.流体流动测量[M].北京:航空工业出版社,1992.
    [7] 刘佳佳.AIN基MEMS风速风向集成传感器的设计[D].哈尔滨:哈尔滨理工大学,2013. LIU Jiajia.Design of AIN-based MEMS wind speed and direction integrated sensor[D].Harbin:Harbin University of Science and Technology,2013.
    [8] 姚伟.微风速矢量测量系统[D].合肥:合肥工业大学,2012. YAO Wei.Measurement system of low wind speed and direction[D].Hefei:Hefei University of Technology,2012.(in Chinese)
    [9] 高东晖.CMOS集成二维风速传感器的研究[D].南京:东南大学,2005. GAO Donghui.Research on CMOS integrated two-dimensional thermal wind sensor[D].Nanjing:Southeast Uiversity,2005.(in Chinese)
    [10] 韦青燕,张天宏.高超声速热线/热膜风速仪研究综述及分析[J].测试技术学报,2012,26(2):142-149. WEI Qingyan,ZHANG Tianhong.Review and analysis of hot-wire/film anemometry for hypersonic airflow measurement[J].Journal of Test and Measurement Technology,2012,26(2):142-149.(in Chinese)
    [11] KUMAR S S,ALONE D B,THIMMAIAH S M,et al.Experimental investigation of unsteady flow in a transonic unistage axial compressor[C]∥Proceedings of the ASME Gas Turbine India Conference on America Society of Mechanical Engineers.New Delhi:ASME,2014:1-8.
    [12] DURI D,BAUDET C,MORO J P,et al.Hot-wire anemometry for superfluid turbulence coflows[J].Review of Scientific Instruments,2015,86(2):1-7.
    [13] AMINI N,SEKARAN A,SCHWAENEN M,et al.An experimental investigation of the free jet flow from a radially lobed nozzle using hotwire anemometry[J].International Journal of Mechanical Engineering Education,2012,40(4):261-275.
    [14] 江智耀,李海旺,由儒全.旋转光滑直通道湍流流动一维热线实验[J].航空动力学报,2019,34(3):556-566. JIANG Zhiyao,LI Haiwang,YOU Ruquan.Experiment on turbulent flow in rotating smooth channel with 1D hot wire[J].Journal of Aerospace Power,2019,34(3):556-566.(in Chinese)
    [15] 魏宽,陶智,邓宏武,等.旋转状态下方形通道内部流畅特性热线实验[J].航空动力学报,2016,31(11):2635-2640. WEI Kuan,TAO Zhi,DENG Hongwu,et al.Hot wire test on the flow fields in a rotating square channel[J].Journal of Aerospace Power,2016,31(11):2635-2640.(in Chinese)
    [16] 王洪伟,宋志强,王治.单斜热线探针测量压气机旋转失速流场[J].航空动力学报,2011,26(2):249-254. WANG Hongwei,SONG Zhiqiang,WANG Zhi.Measurement of rotating stall in an axial compressor using a single slanted hot-wire probe[J].Journal of Aerospace Power,2011,26(2):249-254.(in Chinese)
    [17] 杨杰.微机型超声瞬时风速风谱测量系统[J].合肥工业大学学报(自然科学版),1999,22(6):89-93. YANG Jie.Microprocessor based instantaneous wind speed and wind spectrum measuring system[J].Journal of Hefei University of Technology,1999,22(6):89-93.(in Chinese)
    [18] 程启明,程尹曼,汪明媚,等.风力发电中风速测量技术的发展[J].自动化仪表,2010,31(7):1-4. CHENG Qiming,CHENG Yinman,WANG Mingmei,et al.Development of wind speed measuring technologies in wind power generation[J].Process Automation Instrumentation,2010,31(7):1-4.(in Chinese)
    [19] 张艳艳,巩轲,何淑芳,等.激光多普勒测速技术进展[J].激光与红外,2010,40(11):1157-1162. ZHANG Yanyan,GONG Ke,HE Shufang,et al.Process in laser doppler velocity measurement techniques[J].Laser and Infrared,2010,40(11):1157-1162.(in Chinese)
    [20] 沈熊.激光多普勒测速技术及应用[M].北京:清华大学出版社,2004.
    [21] 杨海燕,刘启洲.叶片裂纹故障的多普勒在线监测技术仿真研究[J].航空动力学报,1999,14(1):69-73. YANG Haiyan,LIU Qizhou.Simulation of Doppler on-line monitoring technique for blade crack fault[J].Journal of Aerospace Power,1999,14(1):69-73.(in Chinese)
    [22] 赵军,刘宝杰,刘火星.机匣视窗折射对LDV聚焦的影响分析[J].航空动力学报,2007,22(7):1161-1166. ZHAO Jun,LIU Baojie,LIU Huoxing.Analysis of beam refraction effects in laser doppler velocimetry[J].Journal of Aerospace Power,2007,22(7):1161-1166.(in Chinese)
    [23] ERDIL A,KODAL A,AYDIN K.Decomposition of turbulent velocity fields in an SI engine[J].Flow,Turbulence and Combustion,2002,68:91-110.
    [24] ESIRGEMENZ E,LMEN S M.A spark-plug LDV probe for in-cylinder flow analysis of production IC engines[J].Measurement Science and Technology,2005,16(10):2038-2047.
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出版历程
  • 收稿日期:  2019-11-05
  • 刊出日期:  2020-06-28

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