延伸冲击孔冲击冷却流动与换热特性的数值研究  

Numerical Study on Flow and Heat Transfer Characteristics of Impingement Cooling with Extended Jet Holes

作　　者：吴航 杨星[1] 赵强[1] 武斌 丰镇平[1] WU Hang;YANG Xing;ZHAO Qiang;WU Bin;FENG Zhen-ping(School of Energy and Power Engineering,Xi’an Jiaotong University,Xi’an 710049,China)

机构地区：[1]西安交通大学能源与动力工程学院,陕西西安710049

出　　处：《推进技术》2022年第10期291-298,共8页Journal of Propulsion Technology

基　　金：国家科技重大专项(2017-Ⅲ-0003-0027);中央高校基本科研业务费专项资金(xjh012019020)。

摘　　要：为了研究冲击孔延伸长度对于冲击冷却系统冷却性能的影响,采用数值模拟方法分析了3个冲击雷诺数和5个冲击孔延伸长度对冲击腔内流动与换热特性的影响,给出了靶面努塞尔数分布、靶面压力分布、中心截面流速与综合换热性能的变化。结果表明:延伸冲击孔可以有效地防止横流对冲击射流的偏转作用,同时使射流出口更加贴近冲击靶面壁面,冲击速度更高,可以明显提高靶面的换热系数,并且整个靶面上的换热系数分布也更加均匀。冲击冷却的冷却性能随着冲击孔延伸长度的增加而增加。相较于传统冲击冷却(Baseline),在延伸距离为冲击孔直径的2.5倍时,靶面平均努塞尔数提升达15%以上,但压力损失也相对较高;对比不同延伸长度冲击孔的综合换热性能,发现存在最佳的延伸距离范围,使冲击冷却系统获得最佳的综合冷却性能。在本研究范围内,最佳延伸距离为冲击孔直径的2.5倍。In order to investigate the effects of the impingement hole extended length on the cooling performance of the impingement cooling system,the effects of three impingement jet Reynolds numbers and five impingement hole extended lengths on the flow and heat transfer characteristics in the impingement cavity were analyzed by numerical simulation. The changes of distributions of Nusselt number,pressure,central cross-section velocity and the resulting overall thermal perform were given in detail. The results show that the extended jet hole can effectively prevent the deflection of crossflow to the impingement jet. The extended impingement hole made the jet outlet closer to the wall,and the flow velocity was higher when it reached the target surface,which obviously improved the average Nusselt number on the target surface,and the heat transfer coefficient distribution of the whole target surface is more uniform. The cooling performance of impingement cooling increased with the increase of jet Reynolds number and the extended length of the jet hole. Compared with the traditional jet impingement configuration(baseline),when the impingement hole extended length is 2.5 times the length of impingement hole diameter,the average Nusselt number of target surface increases by more than 15%. But the penalty was higher pressure loss. In term of comprehensive heat transfer performance,there was an optimal range of extended length,which made the impingement cooling system have the highest comprehensive heat transfer performance. In this study,the best extended length is 2.5 times the length of impingement hole diameter.

关 键 词：冲击冷却 延伸冲击孔 换热特性 流动特性 综合换热性能 

分 类 号：TK47[动力工程及工程热物理—动力机械及工程]