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Lean fuel detection with nanosecond-gated laser-induced breakdown spectroscopy

机译:用纳秒门控激光诱导击穿光谱检测瘦燃料检测

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Nanosecond-gated laser-induced breakdown spectroscopy (n-LIBS) has been used to quantify fuel mole fraction (X-C2H4) in the cavity flameholder of a model high-speed combustor. The measurement locations selected, in the vicinity of the cavity shear layer, have low fuel concentrations. Previous n-LIBS measurements showed unexpectedly high values at these locations with expected low average fuel mole fraction (X-C2H4) and intermittent fuel presence; thus, an effort was undertaken to understand potential sources of error with n-LIBS at low X-C2H4. An improved direct spectrum matching (DSM) calibration matrix was thus constructed, focusing on low X-C2H4 for both reacting and non-reacting conditions. Comparisons were made between n-LIBS measurements using two different laser systems for plasma generation, and the insensitivity of the signal to the specific laser was demonstrated for the first time. Uncertainty of the n-LIBS measurement technique at two different gas densities was analyzed through the processing of spectra acquired at known values of X-C2H4. Measurements in the windtunnel, around the shear layer of the cavity flameholder, were conducted with a Mach-2 or Mach-3 freestream, and comparisons were made between n-LIBS results-using two DSM calibration matrices with different increments in X-C2H4-and numerical results employing dynamic hybrid Reynolds-averaged Navier-Stokes and large-eddy simulation (DHRL). The high-resolution DSM matrix produced slightly lower X-C2H4 than those from the coarse matrix, and comparisons with the simulation showed good agreement overall. For Mach-3 conditions, comparisons were made for both a non-reacting and a reacting cavity flameholder. Here, results showed a systematic difference between measured and simulated values of the mean X-C2H4 within the shear layer but good (even excellent) agreement within the upper portion of the recirculation zone. For reacting condition, four reduced chemical kinetic models were implemented with the DHRL technique and compared to n-LIBS results. Overall, the four kinetic models produced a substantial range of results (e.g., temperatures and reaction progress), showing the importance of a validated diagnostic technique like n-LIBS for model testing. (C) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:纳秒门激光诱导的击穿光谱(N-LIB)已被用于量化模型高速燃烧器的腔体积器中的燃料摩尔分数(X-C2H4)。在腔剪切层附近选择的测量位置具有低燃料浓度。以前的N-libs测量在这些位置显示出意外的高值,其具有预期的低平均燃料摩尔分数(X-C2H4)和间歇燃料存在;因此,在低X-C2H4处,努力了解潜在的误差源误差。因此构造了改进的直接光谱匹配(DSM)校准基质,聚焦在低X-C2H4上,用于反应和非反应条件。使用两种不同的激光系统进行等离子体生成的N-LIB测量在N-LIB测量之间进行比较,并且首次证明了信号与特定激光器的不敏感性。通过在已知的X-C2H4的已知值下获得的光谱处理分析了两种不同气体密度的N-LIBS测量技术的不确定度。围绕腔体持有者的剪切层的挡风机的测量用Mach-2或Mach-3 FreeStream进行,并且在N-LIBS结果之间进行比较 - 使用X-C2H4中具有不同增量的两个DSM校准矩阵 - 使用动态混合雷诺平均Navier-Stokes和大涡模拟(DHRL)的数值结果。高分辨率DSM矩阵比来自粗矩阵的X-C2H4略低,并且与模拟的比较显示了良好的一致。对于Mach-3条件,对非反应和反应腔剥夺者进行比较。这里,结果显示了剪切层内的平均X-C2H4的测量值和模拟值之间的系统差异,但在再循环区域的上部内的良好(甚至优异)一致性。对于反应条件,用DHRL技术实施了四种减少的化学动力学模型,并与N-LIBS结果相比。总体而言,四个动力学模型产生了大量的结果(例如,温度和反应进展),显示了验证诊断技术的重要性,如N-libs进行模型测试。 (c)2020燃烧研究所。由elsevier Inc.出版的所有权利保留。

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