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Numerical study of laminar nonpremixed methane flames in coflow jets: Autoignited lifted flames with tribrachial edges and MILD combustion at elevated temperatures

机译:并流射流中层流非预混甲烷火焰的数值研究:具有三臂边缘的自动点燃的提升火焰和高温下的MILD燃烧

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Autoignition characteristics of laminar nonpremixed methane jet flames in high-temperature coflow air are studied numerically. Several flame configurations are investigated by varying the initial temperature and fuel mole fraction. At a relatively low initial temperature, a non-autoignited nozzle-attached flame is simulated at relatively low jet velocity. When the initial temperature is higher than that required for autoignition, two regimes are investigated: an autoignited lifted flame with tribrachial edge structure and an autoignited lifted flame with Mild combustion. The autoignited lifted flame with tribrachial edge exhibited three branches: lean and rich premixed flame wings and a trailing diffusion flame. Characteristics of kinetic structure for autoignited lifted flames are discussed based on the kinetic structures of homogeneous autoignition and flame propagation of stoichiometric mixture. Results showed that a transition from autoignition to flame propagation modes occurs for reasonably stoichiometric mixtures. The autoignited lifted flame with Mild combustion occurs when methane fuel is highly diluted with nitrogen. The kinetic structure analysis shows that the characteristics of Mild combustion can be treated as an autoignited lean premixed lifted flame. Transition behavior from Mild combustion to nozzle-attached flame was investigated by increasing the fuel mole fraction. As the maximum flame temperature increases with decreasing liftoff height, the kinetic structure showed a transition behavior from autoignition to flame propagation of a lean premixed flame. (C) 2016 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:数值研究了层状非预混甲烷射流火焰在高温同流空气中的自燃特性。通过改变初始温度和燃料摩尔分数来研究几种火焰构型。在较低的初始温度下,以较低的射流速度模拟了未自燃的喷嘴连接火焰。当初始温度高于自动点火所需的温度时,将研究两种情况:具有三臂边缘结构的自燃起火火焰和具有轻度燃烧的自燃起火火焰。具有三臂边缘的自燃起重火焰表现出三个分支:稀薄和浓密的预混合火焰翼和后随扩散火焰。基于化学计量混合物的均匀自燃和火焰传播的动力学结构,讨论了自燃举升火焰的动力学结构特征。结果表明,对于合理的化学计量混合物,会发生从自燃到火焰传播的转变。当甲烷燃料被氮气高度稀释时,会出现轻度燃烧的自燃起火火焰。动力学结构分析表明,轻度燃烧的特性可以看作是一种自动点燃的稀薄预混提升火焰。通过增加燃料摩尔分数,研究了从轻度燃烧到附有喷嘴的火焰的过渡行为。随着最高火焰温度随着离地高度的降低而增加,动力学结构显示出稀薄预混火焰从自燃过渡到火焰蔓延的行为。 (C)2016年燃烧研究所。由Elsevier Inc.出版。保留所有权利。

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