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Nitromethane ignition behind reflected shock waves: Experimental and numerical study

机译:反射冲击波背后的硝基甲烷点火:实验和数值研究

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Ignition delay times for nitromethane have been measured behind reflected shock waves over wide ranges of temperature (875-1595 K); pressure (2.0-35 atm); equivalence ratio (0.5, 1.0, and 2.0); and dilution (99, 98, 95, and 90% Ar by volume) using a L9 Taguchi array. Emission from excited-state hydroxyl radials (OH*) was the primary diagnostic for determining the ignition delay times from the experiments. Results showed that nitromethane's ignition delay time is very sensitive to most of the experimental parameters that were varied. In addition, the OH* profile for nitromethane presents an interesting double feature, with the relative intensity between the two peaks varying greatly depending on the experimental conditions. A detailed chemical kinetics mechanism was assembled from previous work by the authors and from sub-mechanisms from the literature. The latest theoretical work on nitro methane decomposition was used, and the final mechanism satisfactorily reproduces the ignition delay time data from the present study, as well as nitromethane and CH4/NOx ignition delay time data available from the literature. (C) 2016 Elsevier Ltd. All rights reserved.
机译:硝基甲烷的点火延迟时间是在很宽的温度范围(875-1595 K)内,在反射的冲击波后面进行测量的。压力(2.0-35 atm);当量比(0.5、1.0和2.0);使用L9 Taguchi阵列稀释(按体积计算的99、98、95和90%Ar)。激发态羟基辐射(OH *)的发射是确定实验中点火延迟时间的主要诊断方法。结果表明,硝基甲烷的点火延迟时间对变化的大多数实验参数非常敏感。此外,硝基甲烷的OH *曲线具有有趣的双重特征,两个峰之间的相对强度根据实验条件而变化很大。详细的化学动力学机理是由作者先前的工作以及文献中的子机理组装而成的。使用了有关硝基甲烷分解的最新理论工作,并且最终机理令人满意地再现了本研究的点火延迟时间数据,以及可从文献中获得的硝基甲烷和CH4 / NOx点火延迟时间数据。 (C)2016 Elsevier Ltd.保留所有权利。

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