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Nonpremixed n -heptane autoignition in unsteady counterflow

机译:非预混合正庚烷自燃,不稳定逆流

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The effect of unsteady strain on n-heptane autoignition at elevated pressure is studied numerically with detailed chemistry and transport in the counterflow configuration. Specifically, fuel and air temperatures are chosen so that two-stage ignition occurs, as is typical, in the negative temperature-coefficient regime, and the strain perturbations are selected to rapidly rise and fall to mimic rapid turbulent strain-rate fluctuations. For these rapid fluctuations, the response of the mixing layer is unsteady. Small to moderate strain-rate fluctuations result in a small increase in the ignition delay. For sufficiently large strain rates such that the critical scalar dissipation rate is exceeded, the ignition delay is substantially greater. The latter delay results from both the time required for the dissipation rate to decay to below its critical value and the longer ignition delay time for systems with dissipation rates near the critical dissipation rate. For all magnitudes of strain-rate fluctuation, there is evidence that the second stage of the two-stage ignition is more sensitive to inhibition by higher dissipation rates. For sufficiently large dissipation rates, the heat losses force the second stage to the border between the low- and intermediate-temperature chemistries.
机译:数值研究了非定常应变对高压下正庚烷自燃的影响,并详细研究了化学反应和逆流构型下的转运。具体而言,选择燃料和空气温度,以便在负温度系数状态下发生两阶段点火(通常是这样),并且选择应变摄动来快速上升和下降以模仿湍流应变率的快速波动。对于这些快速波动,混合层的响应不稳定。小到中等的应变率波动会导致点火延迟的增加很小。对于足够大的应变率,使得超过临界标量耗散率,点火延迟明显更大。对于耗散率接近临界耗散率的系统,耗散率衰减到低于其临界值所需的时间以及较长的点火延迟时间都是后一种延迟的结果。对于所有大小的应变率波动,都有证据表明,两阶段点火的第二阶段对较高耗散率的抑制作用更为敏感。对于足够大的耗散率,热量损失迫使第二级进入低温和中温化学物质之间的边界。

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