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A computational study and correlation of premixed isooctane air laminar reaction fronts diluted with EGR

机译:EGR稀释预混合异辛烷层流反应前沿的计算研究及相关性

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The current work investigates the propagation of premixed laminar reaction fronts for mixtures of isooc-tane-air and recirculated combustion products (or EGR) under high pressure and temperature conditions. The work uses a transient one-dimensional flame simulation with a skeletal 215 species chemical kinetic mechanism to generate laminar burning velocity and front thickness predictions. The simulation was exercised over fuel-air equivalence ratios, unburned gas temperatures, pressures and EGR levels ranging from 0.1 to 1.0, 400 to 1000 K, 1 to 250 bar, and 0% to 60% (by mass) respectively, a range extending beyond that of previous researchers. Steady reaction fronts with burning velocities in excess of 5 cm/s could not be established under all of these conditions, especially when burned gas temperatures were below 1450 K and/or when characteristic reaction front propagation times were on the order of the unburned gas ignition delay. For a given pressure, T_u and T_b, the burning velocity of an EGR dilute mixture was found to be lower than that of an air dilute mixture, with the decrease in burning velocity attributed primarily to the reduced oxygen concentration's effect on chemistry. Steady premixed laminar burning velocities were correlated using a modified two-equation form based on the asymptotic structure of a laminar flame, which produced an average error of 3.4% between the simulated and correlated laminar burning velocities, with a standard deviation of 4.3%, while additional correlations were constructed for reaction front thickness and adiabatic flame temperature. Correlations are presented based on a non-product equivalence ratio φ and a fraction of stoichiometric combustion products X+(SCp). Conversion factors are provided to facilitate application to modern direct injection internal combustion engines with inherent charge stratification where the local global Φ is different from the global Φ of the residual gas.
机译:当前的工作是研究在高压和高温条件下,异辛烷-空气和再循环燃烧产物(或EGR)的混合物的预混合层流反应前沿的传播。该工作使用具有骨架215种化学动力学机制的一维瞬态火焰模拟来生成层流燃烧速度和前沿厚度预测。在燃油-空气当量比,未燃烧气体温度,压力和EGR水平分别为0.1至1.0、400至1000 K,1至250 bar和0%至60%(质量)的范围内进行了模拟,范围扩大了超越以前的研究人员。在所有这些条件下都无法建立燃烧速度超过5 cm / s的稳定反应前沿,特别是当燃烧气体温度低于1450 K和/或特征反应前沿传播时间约为未燃烧气体着火时。延迟。对于给定的压力T_u和T_b,发现EGR稀释混合物的燃烧速度低于空气稀释混合物的燃烧速度,燃烧速度的下降主要归因于氧气浓度降低对化学物质的影响。在层流火焰渐近结构的基础上,使用修正的两方程式对稳定的预混合层流燃烧速度进行关联,模拟和相关层流燃烧速度之间的平均误差为3.4%,标准偏差为4.3%,而还建立了反应前沿厚度和绝热火焰温度的其他相关性。基于非产物当量比φ和化学计量燃烧产物X +(SCp)的分数表示相关性。提供转换因子以便于应用到具有固有装料分层的现代直喷内燃发动机中,其中局部总Φ与残余气体的总Φ不同。

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