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The Effects of Non-Uniform Boundary Temperatures on Ignition Delay Time Measurements from Heated Rapid Compression Machine Experiments

机译:加热快速压缩机实验中非均匀边界温度对点火延迟时间测量的影响

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Computational fluid dynamics (CFD) simulations are used to investigate the role that non-uniform boundary temperatures have on ignition delay time predictions and temporal compressed gas temperature field development in rapid compression machine (RCM) experiments that use either creviced or flat pistons. Five boundary temperature cases are investigated at a compressed pressure of 7 bar for five different compression ratios. For each compression ratio, a uniform boundary temperature case was used as a baseline for comparison to the other cases which represent non-uniform boundary temperatures. Initial gas temperature fields were based on steady state simulations which account for the effect that non-uniform boundary temperatures have on the gas temperature field prior to the RCM compression stroke. The steady state simulations were used as the initial temperature fields in transient RCM simulations of the compression stroke and the post-compression period. These simulations reveal that non-uniform boundary temperatures significantly influence the development of the compressed temperature field, but their impact on ignition delay times depends on the experimental conditions. The thermal stratification in the compressed gas only becomes consequential to ignition delay time if the controlling chemistry occurs in the region affected by the non-uniformities. This is particularly relevant for measurements made in the negative temperature coefficient region.
机译:计算流体动力学(CFD)模拟用于研究不均匀边界温度在使用弯曲活塞或扁平活塞的快速压缩机(RCM)实验中对点火延迟时间预测和临时压缩气体温度场发展的作用。在五个压缩比下,在7 bar的压缩压力下研究了五个边界温度情况。对于每个压缩比,均以均匀的边界温度为基准,以与代表不均匀边界温度的其他情况进行比较。初始气体温度场基于稳态模拟,该稳态模拟考虑了非均匀边界温度对RCM压缩冲程之前的气体温度场的影响。稳态模拟被用作压缩冲程和压缩后周期的瞬态RCM模拟中的初始温度场。这些模拟表明,不均匀的边界温度会显着影响压缩温度场的发展,但它们对点火延迟时间的影响取决于实验条件。如果控制化学物质在受不均匀影响的区域内发生,则压缩气体中的热分层仅会引起点火延迟时间。这对于在负温度系数区域中进行的测量尤其重要。

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