首页> 外文会议>Spring 2000 meeting of the Western States Section of the Combustion Institute (WSS/CI spring 2000) >Reduced Kinetic Mechanisms in Time Dependent Numerical Simulations of Nonpremixed Flames
【24h】

Reduced Kinetic Mechanisms in Time Dependent Numerical Simulations of Nonpremixed Flames

机译:非预混火焰的时变数值模拟中的简化动力学机理

获取原文
获取原文并翻译 | 示例

摘要

It is of great theoretical interest to investigate the interaction between rames and vortices asrna model problem to study turbulent combustion because a feld of turbulence can be considered asrnan ensemble of vortices of various length and time scales. Interaction between rames and vorticesrngoverns the rate of combustion and results in diu000berent types of instabilites. The goal of thisrnstudy is to understand the limits of applicability of progressively more accurate reduced kineticrnschemes for methane-air rames using time dependent numerical simulations in a two{dimensionalrnrow feld. Nonpremixed one{, three{ and four{step reduced kinetic methane{air rame structurernand rame response to interaction between a pair of counter rotating vortices with an initiallyrnlaminar unstrained rame is studied. Diu000berent combinations of sizes and strengths for the vortexrnpair are selected such that various regimes on a typical rame{vortex interaction map (Cuenot andrnPoinsot, [1]) are covered. From the numerical experiments, continuous burning regime for all threernreduced kinetic schemes are observed. Simulations in which local extinction of the rame by thernvortex pair has been observed for one- and three-step reduced kinetic mechanisms to date. Resultsrnhow that chemical kinetics plays a major role in the extinction dynamics of a methane-air ramernsimulated with a three-step reduced scheme. The precise mechanism by which it is quenched isrncurrently being investigated.
机译:研究湍流燃烧过程中的涡流和涡流asrna模型问题之间的相互作用具有重要的理论意义,因为湍流场可以被视为各种长度和时间尺度的涡流的涡流集合。闸板和涡流之间的相互作用控制燃烧速率,并导致不稳定类型的不稳定。这项研究的目的是利用二维时域中依赖于时间的数值模拟来了解逐步更精确的甲烷-气还原动力学方案的适用范围。研究了非预混合的一步,三步和四步还原的动力学甲烷空气模架结构和模架对一对反向旋转涡流与初始层流无应变模架之间相互作用的响应。选择涡旋对的大小和强度的不同组合,从而覆盖典型rame {涡旋相互作用图(Cuenot andrnPoinsot,[1])”上的各种形式。从数值实验中,观察到了所有三种降低的动力学方案的连续燃烧方案。迄今为止,对于其中一步和三步降低的动力学机制,已经观察到模拟模拟了通过涡旋对实现的局部消光。结果表明,化学动力学在三步还原方案模拟的甲烷-空气的消光动力学中起主要作用。目前正在研究淬火的精确机理。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号