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Multiscalar line measurements in nonisobaric high-pressure underexpanded supersonic jets using rotational-vibrational raman spectroscopy

机译:使用旋转振动拉曼光谱法在非等压高压超膨胀超声速射流中进行多标量线测量

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摘要

This work describes the development of a Raman spectroscopy system formeasuring aerothermochemistry in high-speed jets and flames. A transmissive gratingspectrometer was newly developed for capturing pure rotational Raman and rotationalvibrationalRaman with a single CCD camera. Previous state-of-the-art experimentsapplied line imagining in known flowfields of constant pressure. The system describedherein is designed to provide local measurement of pressure, with full thermochemistry,along a line. In every point, temperature will be measured by examining the Boltzmanndecay of the rotational spectrum, while molar fraction will be measured from thevibrational Raman spectrum. The temperature and concentrations will then be combinedto obtain partial pressure measurements via the equation of state. This work examinesthe phenomenology of rotational and vibrational Raman scattering and proposesalgorithms that can be used for data extraction.
机译:这项工作描述了用于测量高速射流和火焰中的空气热化学的拉曼光谱系统的开发。新开发了一种透射式光栅光谱仪,用于通过单个CCD摄像机捕获纯旋转拉曼和旋转振动拉曼。先前的最新实验在恒定压力的已知流场中应用线成像。本文所述的系统设计用于沿管线提供具有完全热化学作用的局部压力测量。在每个点上,将通过检查旋转光谱的玻尔兹曼衰变来测量温度,而摩尔分数将从振动拉曼光谱中测量。然后将温度和浓度结合起来,通过状态方程获得分压测量值。这项工作研究了旋转和振动拉曼散射的现象学,并提出了可用于数据提取的算法。

著录项

  • 作者

    Cohen Benjamin Nathan;

  • 作者单位
  • 年度 2009
  • 总页数
  • 原文格式 PDF
  • 正文语种 en_US
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