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Extinction and Re-ignition in Non-Premixed Flame-Vortex Interactions under Diesel Conditions

机译:柴油条件下非预混火焰-涡流相互作用的熄灭和重燃

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In this work, 2-D numerical investigations of extinction and re-ignition during interactions of counter-rotating vortex-pairs with a non-premixed flame are carried out under pressures and temperatures encountered in Diesel chambers. A direct-numerical simulation (DNS) code which employs sixth-order spatial accuracy and fourth-order time-integration is employed to solve the Navier-Stokes equations with chemical reactions. N-heptane is chosen as a representative fuel and irreversible single-step and two-step kinetic models are employed. Several representative values for the vortex circulation and length-scale are chosen from the analysis of the near-field of a Diesel jet. Results show that due to the vortex-induced strain, local extinction occurs along the symmetry axis. This extinction is predicted well by 1-D laminar flamelet libraries provided the time-history of the scalar dissipation rate is taken into account. The flame-edges resulting from local extinction interact leading to re-ignition as the initial vortex size approaches the initial flame thickness. This re-ignition phenomenon is 2-D, involves a partially-premixed flame structure and is not predicted by 1-D diffusion flamelet libraries. The results are summarized in terms of a regime diagram constructed from non-dimensional parameters such as the length-scale ratio and the Damkohler number.
机译:在这项工作中,在柴油机舱中遇到的压力和温度下,进行了逆向旋涡对与非预混火焰相互作用过程中熄灭和重燃的二维数值研究。利用六阶空间精度和四阶时间积分的直接数值模拟(DNS)代码来解决具有化学反应的Navier-Stokes方程。选择正庚烷作为代表燃料,并采用不可逆的单步和两步动力学模型。从对柴油机射流的近场分析中选择了几个代表涡流循环和长度尺度的值。结果表明,由于涡旋引起的应变,沿对称轴发生局部消光。如果考虑了标量耗散率的时间历史,则一维层流小火焰库可以很好地预测这种消光。当初始涡旋尺寸接近初始火焰厚度时,由局部熄灭产生的火焰边缘相互作用导致重新点燃。这种重燃现象是二维的,涉及部分预混合的火焰结构,并且不是一维扩散小火焰库预测的。根据状态图总结了结果,该状态图是由无量纲参数(例如长度比例和Damkohler数)构成的。

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