偏心射流对加热圆柱面的冲击冷却数值研究

V. Chauhan, Karuna Kumari, Pankaj Kumar, Vinod Kumar Venkiteswaran, Mohamed M. Awad
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摘要

本文对使用偏心槽射流撞击冷却(SJIC)冷却气缸的效果进行了全面的数值分析。研究重点是在撞击冷却过程中,当狭缝射流偏离中心时的热和流体行为。通过评估气缸周围不同位置的局部努塞尔特数曲线,比较了 k-e 和 k-ε 系列的几个湍流模型,并将这些结果与实验数据进行了比较。研究结果表明,SST k-ω 模型在估算停滞区的努塞尔特数方面优于其他湍流模型,而标准 k-ω 模型在气缸其他位置的性能有所提高。此外,该研究还发现局部最大努塞尔特数有所下降,喷嘴位移方向也发生了变化。气缸尾端的漩涡/再循环流体增强了气缸后端附近的热传递。流体流的分离和重新附着因雷诺数而异,低雷诺数导致重新附着在槽射流的一侧,高雷诺数导致反方向重新附着。此外,随着喷嘴与气缸间距(H/S)的增加,再循环区和漩涡区的长度也会增加。然而,随着偏心率(E/S)的增加,漩涡循环区的面积减小,在 E/S = 4 时完全消失。这项研究为优化冷却设计提供了宝贵的见解。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Numerical Study of Eccentric Jet Impingement Cooling On a Heated Cylindrical Surface
This article presents a comprehensive numerical analysis of the effects of cooling a cylinder using an eccentric Slot Jet Impingement Cooling (SJIC). The study focuses on examining the thermal and fluid behaviour when the slot jet is off-centre, during impingement cooling. Several turbulence models from the k-e and k-ε families were compared by evaluating the local Nusselt number profiles at different locations around the cylinder, and these results were compared to experimental data. The findings indicate that the SST k-ω model outperforms the other turbulence models in estimating the Nusselt number in the stagnation region, while the standard k-ω model shows improved performance elsewhere on the cylinder. Furthermore, this study reveals a decrease in the maximum local Nusselt number and a shift in the direction of the nozzle displacement. The presence of swirling/recirculating fluid at the trailing end of the cylinder enhances heat transfer near the back end of the cylinder. The separation and the reattachment of the fluid stream differ depending on the Reynolds number, with low Reynolds numbers resulting in reattachment on the side of the slot jet and higher Reynolds numbers leading to reattachment in the opposite direction. Additionally, the length of the recirculation and swirling zones increases as the nozzle-to-cylinder spacing (H/S) increases. However, as the eccentricity (E/S) increases, the size of the swirl circulation zones decreases and completely vanishes for E/S = 4. This study provides valuable insights for optimal cooling design.
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