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Analysis of Flamelet Leading Point Dynamics in an Inhomogeneous Flow

机译:在非均匀流动中分析燧发燧发型

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Several studies have utilized "leading points" concepts to explain the augmentation of burning rates in turbulent flames by flow fluctuations. These ideas have been particularly utilized to explain the strong sensitivity of the burning rate to fuel composition. Leading point concepts suggest that the burning velocity is controlled by the velocity of the points on the flame that propagate farthest out into the reactants - thus, they de-emphasize the classical idea that burning velocity enhancement is due to increases in flame surface area. Rather, within this interpretation, flame area creation is the effect, not the cause, of augmented turbulent burning velocities. However, the theory behind the implementation of leading point concepts in turbulent combustion modeling needs further development and the definition of "leading point" has not been fully clarified. For a certain class of steady shear flows, it is straightforward to demonstrate the leading point concept in an intuitive manner, but the problem becomes more complex when the leading points themselves evolve in time. In this paper, we use the G-equation to describe the flame dynamics and, utilizing results for Hamilton-Jacobi equations from the Aubry-Mather theory, show how the large-time behavior of its solutions under certain conditions is controlled only by discrete points on the flame, whose space-time evolution in characteristic space forms a set of "optimal characteristics". However, it is possible to find other conditions where the large time behavior of the flame is not controlled by discrete points on the flame, but rather by its entire surface. Moreover, we also show that even in cases where the burning rate is controlled by discrete points, these points are not necessarily the most forward lying points in the flame front. Finally, we consider the case where the laminar flame speed is a weak function of flame curvature and derive exact results for the sensitivity of the front speed to the Markstein length, l, for l > 0. These solutions explicitly illustrate the reduction of front displacement speed for increasing l, a result previously suggested by measurements.
机译:一些研究采用“龙头点”的概念来解释流量波动在燃烧火焰动荡率的增强。这些想法已经特别用于解释燃烧速率到燃料组合物的强灵敏度。领导点的概念表明,燃烧速度是通过在火焰繁殖最远到物点的速度控制 - 因此,他们不再强调传统的想法,燃烧速度提高是由于火焰表面积增大。相反,这种解释中,火焰面积创作是效果,而不是原因,增强紊流燃烧速度。然而,领导点概念,湍流燃烧模型的实现背后的理论需要进一步发展的“龙头点”尚未完全阐明的定义。对于某一类稳态剪切流,它是简单的证明以直观的方式领先点的概念,但是当领先点本身在时间演变的问题变得更复杂。在本文中,我们使用G-方程来描述火焰动态,并利用从奥布里 - 马瑟理论汉密尔顿 - Jacobi方程的结果,显示了如何其解决方案在一定条件下的大时间行为由离散的点只有控制在火焰,其时空演化特征中形成空间的一组“最佳特性”。然而,有可能寻找到火焰的大时间行为不是由在火焰的离散点控制的其他条件,而是通过其整个表面。此外,我们还表明,即使在燃烧速率由离散点控制的情况下,这些点不一定在火焰的前最前沿躺在点。最后,我们考虑的情况下层流火焰速度是火焰曲率弱函数和导出精确的结果对于前部速度与马克斯坦长度,升的敏感性,对于l> 0。这些解决方案明确地示出了前部位移的减小速度增加升,结果先前由测量建议。

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