一种类螺纹孔结构的旋转射流换热特性数值模拟

徐亮; 兰进; 高建民; 李云龙

doi:10.7652/xjtuxb201709002

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一种类螺纹孔结构的旋转射流换热特性数值模拟

更新时间：2025-07-09

- 一种类螺纹孔结构的旋转射流换热特性数值模拟
- Heat Transfer Characteristics Research of Screw Thread Swirling Impinging Jets Based on Numerical Simulation Method
- 西安交通大学学报 2017年51卷第9期页码：11-18
- 作者机构：
  
  西安交通大学机械制造系统工程国家重点实验室,西安,710049
- 作者简介：
- 基金信息：
  
  : 2017-03-13。作者简介: 徐亮(1980—),男,副教授。基金项目: 陕西省自然科学基础研究计划资助项目(2015JQ5126)
- DOI：10.7652/xjtuxb201709002
  中图分类号： TK124
- 网络首发：2017-09-10，
  
  纸质出版：2017
- 稿件说明：
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徐亮, 兰进, 高建民, 等. 一种类螺纹孔结构的旋转射流换热特性数值模拟[J]. 西安交通大学学报, 2017,51(9):11-18.

Heat Transfer Characteristics Research of Screw Thread Swirling Impinging Jets Based on Numerical Simulation Method[J]. 2017, 51(9): 11-18.
徐亮, 兰进, 高建民, 等. 一种类螺纹孔结构的旋转射流换热特性数值模拟[J]. 西安交通大学学报, 2017,51(9):11-18. DOI： 10.7652/xjtuxb201709002.

Heat Transfer Characteristics Research of Screw Thread Swirling Impinging Jets Based on Numerical Simulation Method[J]. 2017, 51(9): 11-18. DOI： 10.7652/xjtuxb201709002.

摘要

为了提高传统圆孔射流换热的均匀性

提出了一种新型的射流孔结构

即在普通圆孔周围设置螺旋槽

类似于内螺纹

并基于已有文献中的一种置入螺旋杆喷嘴的旋转射流实验数据

发展了一种采用RNG k-ε湍流模型的旋转射流传热数值计算方法。采用该方法

研究了雷诺数(4 000～12 000)、冲击距离(1～8倍当量直径)、螺旋角(0°～75°)等参数对所设计的螺纹孔旋转射流传热的影响。数值结果表明:提高雷诺数可以有效提高换热效率

并且能获得良好的换热均匀性; 随着冲击距离的增大

旋转射流的局部努塞尔数先增大后减小

双峰值特性逐渐消失并转变为单峰值特性

在4倍当量直径的冲击距离时

换热系数达到最大值; 随着螺旋角增大

中心点的局部努塞尔数也随之增大

同时换热均匀性会变差。研究还发现

不同冲击距离下换热性能最佳时对应的螺旋角也不同。

Abstract

To improve the uniformity of traditional impinging jet heat transfer

a new type of jet structure with some circumferential spiral channels set inside the normal nozzle

like the internal thread

is proposed in this paper. First

several numerical methods are adopted to process the experimental data of the swirling impinging jet from a swirl generator

and the data are referenced from a published literature. Results show that the RNG k-ε turbulence model is more suitable for simulation of the swirling impingement jet. Then

the effects of such parameters as Reynolds number(4 000-12 000)

impact distance(1-8 times of equivalent diameter)and helix angle(0°-75°)on the heat transfer performance of such threaded hole are studied. The research is focused on the flow field and heat transfer characteristics. The experimental results indicate that the heat transfer rate and the uniformity of impinging target will increase with the Reynolds number

and the local Nusselt number will increase first and then decrease with the increasing impact distance. Meanwhile

the double-peak feature of the local Nusselt number will change to single-peak shape

and the maximum local Nusselt number can be obtained at the 4-fold equivalent diameter. The local Nusselt number at the center point will increase with the helix angle

but the heat transfer uniformity will be worse. In addition

it is found that the helix angle corresponding to the best heat transfer performance also changes with different impact distances.

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Keywords

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