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Fully explicit implementation of direct numerical simulation for a transient near-field methane/air diffusion jet flame

机译:完全明确实现瞬态近场甲烷/空气扩散射流火焰的直接数值模拟

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Direct numerical simulation (DNS) is a kind of ultimate numerical simulation tool for studying fundamental turbulent flows, mixing, chemical reactions and interactions among them. In the present work, a fully explicit method of implementing DNS is presented for investigating transient multi-component methane/air jet flame in the near field. The detailed methodology, enclosing non-dimensional governing equations, inlet velocity disturbance, chemical scheme and fluid property, was discussed. An explicit eighth-order finite-difference scheme was used combined with an explicit tenth-order filter. Conservative variables are temporally advanced in two segmented stages that handle Euler terms and viscous terms respectively. A modified non-reflecting boundary condition was used, which has better performance about the characteristic waves on boundary planes. The developed code was firstly tested with an air jet and evaluated in terms of accuracy and parallel efficiency. Then a methane/air combusting jet was simulated to study the characteristics of the chemical heat-release in turbulence.
机译:直接数值模拟(DNS)是一种用于研究基本湍流,混合,化学反应以及它们之间相互作用的终极数值模拟工具。在当前的工作中,提出了一种完全明确的实施DNS的方法,用于研究近场中的瞬态多组分甲烷/空气喷射火焰。讨论了详细的方法,包括无量纲控制方程,入口速度扰动,化学方案和流体性质。显式八阶有限差分方案与显式十阶滤波器组合使用。保守变量在两个分别处理欧拉项和粘性项的分段阶段中在时间上前进。使用了改进的非反射边界条件,它对边界平面上的特征波具有更好的性能。最初使用喷气机对开发的代码进行测试,并在准确性和并行效率方面进行了评估。然后模拟了甲烷/空气燃烧喷嘴,以研究湍流中化学放热的特征。

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