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Development of an in-Cylinder Heat Transfer Model with Compressibility Effects on Turbulent Prandtl Number, Eddy Viscosity Ratio and Kinematic Viscosity Variation

机译:具有压缩性对湍流普朗特数,涡流粘度比和运动粘度变化的缸内传热模型的开发

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In-cylinder heat transfer has strong effects on engine performance and emissions and heat transfer modeling is closely related to the physics of the thermal boundary layer, especially the effects of conductivity and Prandtl number inside the thermal boundary layer. Compressibility effects.on the thermal boundary layer are important issues in multi-dimensional in-cylinder heat transfer modeling. Nevertheless, the compressibility effects on kinematic viscosity and the variation of turbulent Prandtl number and eddy viscosity ratio have not been thoroughly investigated. In this study, an in-cylinder heat transfer model is developed by introducing compressibility effects on turbulent Prandtl number, eddy viscosity ratio and kinematic viscosity variation with a power-law approximation. This new heat transfer model is implemented to a spark-ignition engine with a coherent flamelet turbulent combustion model and the RNG k-E turbulence model. The model constant of the new heat transfer model which can yield the accurate match with experimental data for various operating conditions is found. The new heat transfer model with the model constant of 1.12 is suggested as an improved heat transfer model.
机译:缸内传热对发动机性能和排放有很大影响,并且传热建模与热边界层的物理特性密切相关,尤其是热边界层内部的电导率和普朗特数的影响。在多维缸内传热模型中,对热边界层的可压缩性影响是重要的问题。然而,可压缩性对运动粘度的影响以及湍流普朗特数和涡流粘度比的变化尚未得到充分研究。在这项研究中,通过引入对幂级近似的湍流普朗特数,涡流粘度比和运动粘度变化的可压缩性影响,建立了缸内传热模型。这种新的热传递模型通过具有相干小火焰湍流燃烧模型和RNG k-E湍流模型的火花点火发动机实现。找到了新的传热模型的模型常数,该常数可以与各种操作条件下的实验数据精确匹配。建议使用模型常数为1.12的新传热模型作为改进的传热模型。

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