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Use of PLIF and PIV Techniques to Analyze the Flow Mixing in Dilution Zone of an Aeronautic Combustor

机译:使用PLIF和PIV技术分析航空燃烧器稀释区的流动混合

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摘要

This paper presents a study using PIV and PLIF techniques to investigate the mixing of eight jets flowing transversally into a pipe flow. These methods permit to identify the unsteady and steady features of the flow. The different vortical structures are revealed and quantitative information is obtained to characterize the mass transfer between the different flows. The analysis of the instantaneous velocity field indicates that the two counter rotative structures typical of this flow configuration, are stable close to the jet exit and become unsteady further downstream. The PLIF techniques applied on acetone permits to analyze the mixing of the different jet. Mean trajectories are determined with respect to the R ratio and the spreading of the jets is analyzed. Comparison between the velocity and the concentration results reveals the coupling between the aerodynamic and the mixture fields. Further treatments can be done in order to identify the influence of the Schmidt number on the mass and momentum diffusion. All these results were used to validate LES calculations (Priere, 2005).
机译:本文介绍了一项使用PIV和PLIF技术进行的研究,以研究横向流动成管道流的8个射流的混合。这些方法可以识别流的不稳定和稳定特征。揭示了不同的涡旋结构,并获得了定量信息以表征不同流之间的传质。对瞬时速度场的分析表明,这种流动形态的两个典型的反向旋转结构在射流出口附近稳定,在下游更不稳定。应用于丙酮的PLIF技术可以分析不同射流的混合情况。确定相对于R比的平均轨迹,并分析射流的扩散。速度和浓度结果之间的比较揭示了空气动力场和混合气场之间的耦合。为了确定施密特数对质量和动量扩散的影响,可以做进一步的处理。所有这些结果均用于验证LES计算(Priere,2005年)。

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