首页> 外文会议>Proceedings of the Combustion Institute >TWO-DIMENSIONAL DIRECT NUMERICAL SIMULATION OF OPPOSED-JET HYDROGEN/AIR FLAMES: TRANSITION FROM A DIFFUSION TO AN EDGE FLAME
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TWO-DIMENSIONAL DIRECT NUMERICAL SIMULATION OF OPPOSED-JET HYDROGEN/AIR FLAMES: TRANSITION FROM A DIFFUSION TO AN EDGE FLAME

机译:对面喷射氢/火焰的二维直接数值模拟:从扩散到边缘火焰的过渡

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In an opposed-jet diffusion flame experiment, under certain conditions, after the extinction of the diffusion flame, an edge flame can be obtained. This ring-shaped edge flame was first reported in 1959 by Potter and Butler but received little attention. It was reported again recently in a numerical and an experimental work and is responsible for an interesting transition between two distinct burning flames (multiple solutions). Motivated by our previous numerical results, obtained with simplified kinetics and some recently reported experimental data, we performed direct numerical simulations of this transition to investigate the underlying physical mechanisms. The appearance of an edge flame after the extinction of the diffusion flame, the hysteresis reported in the experiments, and the existence of multiple vigorously burning flames at identical conditions are all captured by our simulations. Our numerical results show that, in the absence of an inert coflow curtain, when the diffusion flame disk is extinguished, an edge flame forms and propagates in the mixing layer. After the formation of this edge flame, even when the applied strain rate is reduced to the initial subcritical value, the diffusion flame disk does not reappear, because the local fluid velocity still exceeds the propagation speed of the edge flame. This hysteresis has significant implications in the common submodel that utilizes the strain rate as a parameter to determine local reignition in flamelet models; it indicates that a subcritical strain rate is not a sufficient condition for the reignition of a diffusion flame. Further investigation of this phenomenon is clearly needed to refine submodels of local extinction and reignition in the flamelet models for turbulent diffusion flames. The opposed-jet configuration provides a convenient platform to analyze edge flames which are stabilized aerodynami-cally in a two-dimensional geometry, thus making matching two-dimensional direct numerical simulations effective.
机译:在对置扩散火焰实验中,在一定条件下,扩散火焰消失后,可获得边缘火焰。这种环形的边缘火焰最早是1959年由Potter和Butler报道的,但很少受到关注。最近在数值和实验工作中又有报道,它负责两个不同的燃烧火焰(多种解决方案)之间的有趣过渡。受以前的数值结果(通过简化的动力学获得的结果)和一些最近报道的实验数据的激励,我们对这种转变进行了直接的数值模拟,以研究潜在的物理机理。扩散火焰消失后出现的边缘火焰,实验中报告的滞后现象以及在相同条件下存在多个剧烈燃烧的火焰均通过我们的模拟得以捕获。我们的数值结果表明,在没有惰性顺流帘的情况下,当扩散火焰盘熄灭时,边缘火焰在混合层中形成并传播。在形成该边缘火焰之后,即使当所施加的应变率减小到初始亚临界值时,由于局部流体速度仍然超过边缘火焰的传播速度,因此扩散火焰盘也不会重新出现。这种滞后现象对普通子模型具有重要意义,该子模型利用应变率作为参数来确定小火焰模型中的局部点火。这表明亚临界应变率不足以重新点燃扩散火焰。显然,需要进一步研究这种现象,以完善湍流扩散火焰的小火焰模型中局部熄灭和着火的子模型。对置射流配置提供了一个方便的平台来分析边缘火焰,这些边缘火焰在二维几何结构中被气固性地稳定在空气中,从而使匹配的二维直接数值模拟有效。

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