微尺度受限冲击冷却通道换热特性研究  

Investigation of Jet Impingement Heat Transfer for Micro-channel

作　　者：郑杰[1] 朱惠人[1] 孟通[1] 路宏康 闫建坤[1] 

机构地区：[1]西北工业大学动力与能源学院,陕西西安710072

出　　处：《机械与电子》2014年第8期22-25,51,共5页Machinery & Electronics

摘　　要：为了更进一步研究真实发动机尺寸下冲击通道的流动与换热情况,针对冲击孔与气膜孔组合形式的受限冲击通道,在保证与真实发动机工况相等的克努森数,通过实验研究与数值模拟研究,进一步解释了不同结构微小冲击通道的整体换热情况,结果表明,在相同的雷诺数下,冲击射流孔径越小,冲击靶面驻点区域内换热越强,冲击平均对流换热系数越大。孔间距越小,冲击靶面平均对流换热系数越大,并且随着射流冲击距的增大,换热减弱。In order to investigate the flow and heat transfer characteristics of inner cooling chan-nel with real engine sizes.This paper mainly to in-vestigate the heat transfer characteristics of micro scale confined impingement cooling structures. Knudsen number is equal to the Knudsen number in real working condition of engine.The thermody-namic characteristics of micro scale impingement channels with different geometry are studied by ex-periment and numerical simulation.The results show that with the same Reynolds number,average heat transfer coefficient of channel increases as the holes diameter decreases,and it decreases as the magnitude of impingement distance or hole spacing increases.

关 键 词：冲击冷却 微尺度 数值模拟 换热系数 雷诺数 

分 类 号：V239[航空宇航科学与技术—航空宇航推进理论与工程]