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Interferometric investigation of methanol droplet combustion in varying oxygen environments under normal gravity

机译:重力作用下不同氧气环境下甲醇液滴燃烧的干涉测量研究

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Non-intrusive diagnostics of droplet combustion using laser-based interferometric technique have been presented. The experiments have been conducted with methanol droplet as the model combusting material under normal gravity with oxygen-nitrogen mixtures at ambient pressure and temperature. The mixtures contained five different oxygen concentrations of 9, 13, 17, 21 and 25%. Projection data of the temperature field around the combusting droplet have been recorded using a Mach-Zehnder interferometer and the interferograms have been analyzed to retrieve the whole field flame temperature distribution around the combusting droplet. The limiting oxygen index (LOI) has been deduced based on real time interferometric images by varying the oxygen concentration levels. Results of the study showed an increase in the flame temperatures with increasing oxygen concentrations and an oxygen concentration level of 13% has been identified as the LOI for methanol droplet. The whole field temperature distribution has been used to calculate the radial temperature gradients between the flame and the droplet surface. These temperature gradients were seen to be a direct function of oxygen concentration. Based on the radial temperature gradients, instantaneous mass burning rates and burning rate constants were computed and a reasonably close agreement between the interferometric predictions and those based on the videographic method was observed. To the best of the knowledge of the authors, the present work is the first successful application of Mach Zehnder interferometry for investigating droplet combustion phenomena. In contrast to the conventional videography approach, the interferometric technique not merely acts as a visualization tool, but also provides quantitative information in the form of whole field temperature distribution, which plays an important role in the determination of mass burning rates and burning rate constants.
机译:已经提出了使用基于激光的干涉技术对液滴燃烧进行非侵入式诊断。实验是在常压和常温常压下,以氧气-氮气混合物在正常重力下,以甲醇滴为模型燃烧材料进行的。混合物包含9、13、17、21和25%的五种不同的氧气浓度。使用Mach-Zehnder干涉仪记录了燃烧液滴周围温度场的投影数据,并对干涉图进行了分析,以获取燃烧液滴周围的整个场火焰温度分布。极限氧指数(LOI)已根据实时干涉图像通过更改氧浓度水平得出。研究结果表明,火焰温度随氧气浓度的增加而升高,氧气浓度水平为13%已被确定为甲醇滴的LOI。整个场温度分布已用于计算火焰和液滴表面之间的径向温度梯度。这些温度梯度被认为是氧浓度的直接函数。根据径向温度梯度,计算瞬时质量燃烧速率和燃烧速率常数,并观察到干涉测量预测与基于摄像方法的预测之间的合理接近一致性。据作者所知,目前的工作是马赫曾德尔干涉测量法在液滴燃烧现象研究中的首次成功应用。与传统的摄影方法相比,干涉技术不仅充当可视化工具,而且还以全场温度分布的形式提供定量信息,这在确定质量燃烧速率和燃烧速率常数方面起着重要作用。

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