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干涉瑞利散射测速技术在跨超声速风洞的湍流度测试应用研究

杨富荣 陈力 闫博 苏铁 鲍伟义 陈爽

杨富荣, 陈力, 闫博, 等. 干涉瑞利散射测速技术在跨超声速风洞的湍流度测试应用研究[J]. 实验流体力学, 2018, 32(3): 82-86. doi: 10.11729/syltlx20170103
引用本文: 杨富荣, 陈力, 闫博, 等. 干涉瑞利散射测速技术在跨超声速风洞的湍流度测试应用研究[J]. 实验流体力学, 2018, 32(3): 82-86. doi: 10.11729/syltlx20170103
Yang Furong, Chen Li, Yan Bo, et al. Measurement of turbulence velocity fluctuations in transonic wind tunnel using Interferometric Rayleigh Scattering diagnostic technique[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(3): 82-86. doi: 10.11729/syltlx20170103
Citation: Yang Furong, Chen Li, Yan Bo, et al. Measurement of turbulence velocity fluctuations in transonic wind tunnel using Interferometric Rayleigh Scattering diagnostic technique[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(3): 82-86. doi: 10.11729/syltlx20170103

干涉瑞利散射测速技术在跨超声速风洞的湍流度测试应用研究

doi: 10.11729/syltlx20170103
基金项目: 

国家自然科学基金 11272337

详细信息
    作者简介:

    杨富荣(1962-), 男, 江西莲花人, 高级工程师。研究方向:光谱诊断, 流动显示。通信地址:四川省绵阳市二环路南段6号14信箱(621000)。E-mail:chenli_03@163.com

    通讯作者:

    陈力, E-mail:Huangmao_03@163.com

  • 中图分类号: V7

Measurement of turbulence velocity fluctuations in transonic wind tunnel using Interferometric Rayleigh Scattering diagnostic technique

  • 摘要: 为了测量高速流场的湍流度,研究了基于法布里-珀罗(Fabry-Pérot)干涉仪的干涉瑞利散射测速技术。设计了干涉瑞利散射速度测量装置,主要由大功率窄线宽连续激光器、法布里-珀罗干涉仪和高帧频EMCCD相机组成,激光器提供连续光源照射流场形成气体分子瑞利散射,并通过法布里-珀罗干涉仪和EMCCD,实现了对流场气体分子瑞利散射光谱精细分辨,获得了高时间分辨速度测量结果。经过理论分析,该装置的速度分辨率为1.23m/s;通过与热线风速仪湍流度测量实验的结果进行对比,验证了干涉瑞利散射测速技术具备流场湍流度非接触测量能力;利用干涉瑞利散射测速装置,在0.3m×0.3m跨超声速风洞上,开展了Ma3.0条件下流场湍流度测量实验,获得了超声速流场的平均速度和湍流度测量结果,装置时间采样率达到4kHz。
  • 图  1  干涉瑞利散射测速装置示意图

    Figure  1.  Sketch of the time-resolved IRS speedometer

    图  2  (a) 同一时刻不同级次(只标记出kk-1)的参考激光(用黑色虚线标记)及瑞利散射信号(用黑色点线标记)形成的干涉圆环;(b)不同波长激光Fabry-Pérot干涉圆环一维强度分布计算结果,插图为局部放大结果

    Figure  2.  (a) Interference rings consist of the reference laser (black dotted lines) and the Rayleigh light (black solid lines) scattered simultaneously at different levels (k, k-1), (b) Computational 1D intensity distributions of Fabry-Pérot interference rings at different laser wavelengths. The inset shows a partially enlarged view

    图  3  热线风速仪速度脉动(a)及功率谱(b)测量结果

    Figure  3.  The measured velocity pulsation (a) and the power spectrum (b) by the hot wire anemometry

    图  4  干涉瑞利散射测速装置速度脉动(a)及功率谱(b)测量结果

    Figure  4.  The measured velocity pulsation (a) and the power spectrum (b) by the IRS speedometer

    图  5  干涉瑞利散射测速装置在0.3m×0.3m跨超声速风洞上的实验布局

    Figure  5.  The measuring layout in 0.3m×0.3m transonic wind tunnel using the time-resolved IRS speedometer

    图  6  速度脉动(a)及功率谱(b)测量结果

    Figure  6.  Velocity pulsation (a) and the power spectrum (b)

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出版历程
  • 收稿日期:  2017-08-14
  • 修回日期:  2017-10-30
  • 刊出日期:  2018-06-25

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