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Dynamic measurement of temperature, velocity, and density in hot jets using Rayleigh scattering

机译:使用瑞利散射动态测量热射流中的温度,速度和密度

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摘要

A molecular Rayleigh scattering technique is utilized to measure gas temperature, velocity, and density in unseeded gas flows at sampling rates up to 10 kHz, providing fluctuation information up to 5 kHz based on the Nyquist theorem. A high-power continuous-wave laser beam is focused at a point in an air flow field and Rayleigh scattered light is collected and fiber-optically transmitted to a Fabry–Perot interferometer for spectral analysis. Photomultiplier tubes operated in the photon counting mode allow high-frequency sampling of the total signal level and the circular interference pattern to provide dynamic density, temperature, and velocity measurements. Mean and root mean square velocity, temperature, and density, as well as power spectral density calculations, are presented for measurements in a hydrogen-combustor heated jet facility with a 50.8-mm diameter nozzle at NASA John H. Glenn Research Center at Lewis Field. The Rayleigh measurements are compared with particle image velocimetry data and computational fluid dynamics predictions. This technique is aimed at aeronautics research related to identifying noise sources in free jets, as well as applications in supersonic and hypersonic flows where measurement of flow properties, including mass flux, is required in the presence of shocks and ionization occurrence.
机译:分子瑞利散射技术用于以高达10 kHz的采样率测量非播种气流中的气体温度,速度和密度,基于奈奎斯特定理提供高达5 kHz的波动信息。高功率连续波激光束聚焦在气流场中的某个点,并收集瑞利散射光,然后将其光纤传输到法布里-珀罗干涉仪进行光谱分析。以光子计数模式工作的光电倍增管允许对总信号电平和圆形干涉图进行高频采样,以提供动态密度,温度和速度测量。提出了均方根和均方根速度,温度和密度,以及功率谱密度计算,用于在NASA约翰·格伦研究中心的刘易斯菲尔德(John H. Glenn)研究中心使用氢燃烧器加热的射流设备(直径为50.8毫米)进行测量。将瑞利测量值与粒子图像测速数据和计算流体动力学预测进行比较。这项技术旨在与自由喷气中的噪声源识别相关的航空研究,以及在存在冲击和电离现象的情况下需要测量流动特性(包括质量通量)的超音速和高超音速流中的应用。

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