半圆柱形凹靶面单排射流冲击换热实验研究
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作者单位:

1.南京航空航天大学能源与动力学院, 航空发动机热环境与热结构工业和信息化部重点实验室,南京,210016;2.先进航空发动机协同创新中心,北京,100191

作者简介:

通讯作者:

张靖周,男,教授,博士生导师, E-mail: zhangjz@nuaa.edu.cn。

中图分类号:

V244.1

基金项目:

国家自然科学基金(51776097)资助项目。


Experimental Investigation of Single-Row Jet Impingement Heat Transfer on Semi-cylindrical Concave Surface
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Affiliation:

1.College of Energy and Power Engineering, Nanjing University of Aeronautics & Astronautics, Aero-engine Thermal Environment and Structure Key Laboratory of Ministry of Industry and Information Technology, Nanjing, 210016, China;2.Collaborative Innovation Center for Advanced Aero-engine, Beijing, 100191, China

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    摘要:

    对半圆柱形凹形靶面单排圆形喷管和冠齿形喷管射流冲击换热进行了实验研究。凹形靶面直径与喷管直径之比D/d为10,射流孔节距与直径之比W/d为5,射流雷诺数分别为5 000、10 000和20 000,冲击间距比H/d分别为2、4、6和8。实验结果表明:两种形状喷管均在冲击间距比H/d=4时获得最强的驻点对流换热,但凹靶面前缘附近纵向平均努塞尔数基本呈现随射流冲击间距增加而减小的单调变换趋势;相对于圆形喷管,冠齿喷管射流冲击使得凹形靶面前缘线上的纵向平均努塞尔数最大提高幅度约为16%,凹形靶面前缘±2d区域的面积平均努塞尔数最大提高幅度约为18%。

    Abstract:

    Experimental investigations are performed on the single-row jet impingement heat transfer onto a semi-cylindrical concave surface. Two kinds of nozzle shapes are taken into consideration. They are circular nozzle and chevron nozzle. The semi-cylindrical concave surface has a diameter ratio (D/d) of 10. The jet-to-jet pitch is 5d. The experiments are conducted under three Reynolds numbers (Re=5 000, 10 000, and 20 000) and four dimensionless nozzle-to-surface distances (H/d=2, 4, 6, and 8). The results show that both nozzles achieve their respective maximum stagnation Nusselt numbers at H/d=4. However, the longitudinally-averaged Nusselt number in the vicinity of concave leading is monotonously reduced with the increase of nozzle-to-surface distance in general. The chevron nozzle is confirmed to produce higher convective heat transfer than that of circular nozzle. In comparison with the circular nozzle jet impingement, the maximum increase of longitudinally-averaged Nusselt number at the concave leading is about 16% and the maximum increase of the locally area-averaged Nusselt number in the vicinity of concave leading (within ±2d) is about 18%, produced by the chevron-nozzle jet impingement.

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刘锡晨,吕元伟,张靖周.半圆柱形凹靶面单排射流冲击换热实验研究[J].南京航空航天大学学报,2020,52(5):808-816

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  • 收稿日期:2019-05-21
  • 最后修改日期:2019-11-11
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  • 在线发布日期: 2020-11-12
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