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Direct Numerical Simulation of the Transition from a Laminar Cool n-Heptane/Air Ignition Front to a Distributed Premixed Turbulent Cool Flame

机译:直接数值模拟从层状凉爽的正庚烷/空气点火前面的过渡到分布式预混湍流冷火焰

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The first direct numerical simulation of a 3D n-heptane/air premixed turbulent cool flame in turbulence intensity typical of the thin reaction zones regime is presented. Chemistry is described by a 129-species, 1234-reaction mechanism (reduced from CaltechMech). Under the current conditions (1 atm, 650 K, and equivalence ratio of 0.7) the initial laminar cool flame is strongly affected by auto-ignition, which is expected to occur under engine conditions, and has an ignition front (or wave) structure. As the turbulent flame develops, turbulent diffusion becomes sufficiently large to initiate self-propagation of the cool flame. The flame is observed to propagate upstream steadily until it reaches the inlet. The steady-state turbulent flame is found to be highly distorted and have a highly distributed reaction zone. As a result, the chemical source terms and heat release rate conditioned on temperature are strongly reduced (more than 50%) compared to the reference laminar cool flame. However, this strong turbulence does not affect the global chemical pathways, but only their magnitude and locations in temperature space.
机译:提出了薄反应区制度典型湍流强度的3D正庚烷/空气预混湍流冷火焰的第一直接数值模拟。化学由129种,1234-反应机制(从CALTECHMECH降低)描述。在当前条件下(1atm,650k和0.7的等效率为0.7),初始层状冷火焰受到自动点火的强烈影响,预期在发动机条件下发生,并且具有点火前(或波)结构。随着湍流的火焰发育,湍流扩散变得足够大以引发冷火焰的自蔓延。观察火焰以稳定地在上游传播直至其到达入口。发现稳态湍流火焰高度扭曲并具有高度分布式的反应区。结果,与参考层光火焰相比,在温度下调节的化学源术语和散热速率强烈降低(超过50%)。然而,这种强烈的湍流不会影响全球化学途径,而是仅在温度空间中的幅度和位置。

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