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Role of the intake generated thermal stratification on the temperature distribution at top dead center of the compression stroke

机译:进气口产生的热分层对压缩冲程上止点温度分布的作用

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This work investigates the role of the intake generated thermal stratification in the temperature field evolution during the compression stroke using direct numerical simulation. The analysis compares two direct numerical simulations during the compression stroke, from which one is initialized with a homogeneous temperature distribution and the other one with a stratified temperature field resulting from a precursor direct numerical simulation of the intake stroke. All other initial and boundary conditions are identically imposed. The results show that the thermal situation at bottom dead center has nearly no impact on the evolution of the temperature field and the wall heat transfer during compression. Dominating mechanism for the temperature field evolution is found to be the convective transport of cold gases from the boundary layers toward the cylinder center. As a consequence, the wall temperature and the flow field are the main influencing parameters controlling the evolution of the temperature distribution during compression. This finding can assist practical engine experiments, since it points out which mechanisms are promising to affect the temperature field during the compression stroke. In addition, it explains why the stratification of the temperature field during intake by varying the gas temperatures in the two intake channels showed only a minor impact on the thermal situation at top dead center.
机译:这项工作使用直接数值模拟研究了进气冲程产生的热分层在压缩冲程期间温度场演变中的作用。该分析比较了在压缩冲程期间的两个直接数值模拟,其中一个以均匀的温度分布初始化,另一个以分层的温度场初始化,该温度场是由进气冲程的前驱直接数值模拟产生的。所有其他初始条件和边界条件均被强加。结果表明,下死点的热态对压缩过程中温度场的演化和壁传热几乎没有影响。发现温度场演化的主要机制是冷气体从边界层向气缸中心的对流传输。因此,壁温和流场是控制压缩过程中温度分布变化的主要影响参数。这个发现可以帮助实际的发动机实验,因为它指出了在压缩冲程期间哪些机制有望影响温度场。此外,它解释了为什么通过改变两个进气通道中的气体温度来使进气过程中的温度场分层仅对上止点的热状况产生很小的影响。

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