Measurement of turbulence velocity fluctuations in transonic wind tunnel using Interferometric Rayleigh Scattering diagnostic technique
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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。Abstract: The interferometric Rayleigh scattering diagnostic technique for the time-resolved velocity measurement of the transonic wind tunnel is studied. The velocity-measurement apparatus, consisted of a CW laser, a high resolution Fabry-Pérot interferometer and a high-speed EMCCD camera, is designed. Rayleigh scattering light is produced as the flow irradiated by the laser. Then the light is collected and analyzed accurately by the Fabry-Pérot interferometer and the camera. Theoretically, this systematic velocity-measurement accuracy can reach 1.23m/s. Measurement accuracy is then evaluated by comparing with hot wire anemometry results. Moreover, the distributions of velocity and turbulence intensity in a supersonic flow at Mach number 3.0 are obtained quantitatively. The sampling rate in this measurement reached about 4 kHz.
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图 2 (a) 同一时刻不同级次(只标记出k,k-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
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