期刊文献+

Experimental study of single-row chevron-jet impingement heat transfer on concave surfaces with different curvatures 被引量:5

Experimental study of single-row chevron-jet impingement heat transfer on concave surfaces with different curvatures
原文传递
导出
摘要 To address the curvature effect on single-row chevron-nozzle jet impingement heat transfer on concave surface,a series of experiments are conducted in the present investigation.Four concave surfaces including one semi-cylindrical concave surface and three parabolic concave surfaces with different width-to-depth ratios are tested under three typical Reynolds numbers(Re=5000,10000 and 15000)and several dimensionless nozzle-to-surface distances ranging from 1 to 8.The results show that the concave curvature has a clear impact on chevron-nozzle jet impingement heat transfer,tightly dependent on jet Reynolds number and impinging distance.In general,the semicylindrical concave surface produces the highest longitudinally-averaged Nusselt number at the leading line of concave surface.Under a low jet Reynolds number,the parabolic concave surface with a highly curved curvature produces higher longitudinally-averaged Nusselt number at the leading line and more uniform longitudinally-averaged Nusselt number distribution along the curvilinear direction.However,the longitudinally-averaged Nusselt number at the leading line of concave surface is the lowest for the highly curved surface under a high jet Reynolds number and large impinging distance.In comparison with the round-nozzle,chevron nozzle plays a more significant role on improving jet impingement heat transfer at small impinging distances. To address the curvature effect on single-row chevron-nozzle jet impingement heat transfer on concave surface, a series of experiments are conducted in the present investigation.Four concave surfaces including one semi-cylindrical concave surface and three parabolic concave surfaces with different width-to-depth ratios are tested under three typical Reynolds numbers(Re = 5000,10000 and 15000) and several dimensionless nozzle-to-surface distances ranging from 1 to 8.The results show that the concave curvature has a clear impact on chevron-nozzle jet impingement heat transfer, tightly dependent on jet Reynolds number and impinging distance.In general, the semicylindrical concave surface produces the highest longitudinally-averaged Nusselt number at the leading line of concave surface.Under a low jet Reynolds number, the parabolic concave surface with a highly curved curvature produces higher longitudinally-averaged Nusselt number at the leading line and more uniform longitudinally-averaged Nusselt number distribution along the curvilinear direction.However, the longitudinally-averaged Nusselt number at the leading line of concave surface is the lowest for the highly curved surface under a high jet Reynolds number and large impinging distance.In comparison with the round-nozzle, chevron nozzle plays a more significant role on improving jet impingement heat transfer at small impinging distances.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第10期2275-2285,共11页 中国航空学报(英文版)
基金 the financial supports for this project from the National Natural Science Foundation of China(No.51776097) the Open Fund of Jiangsu Province Key Laboratory of Aerospace Power System(No.APS20A7002) the Postgraduate Research and Practice Innovation Project of Jiangsu Province(No.KYCX17 0280)
关键词 CHEVRON NOZZLE CONCAVE surface Experimental test Heat transfer Jet IMPINGEMENT Chevron nozzle Concave surface Experimental test Heat transfer Jet impingement
  • 相关文献

参考文献4

二级参考文献29

  • 1裘燮纲,余小章.微引射防冰腔热力计算[J].航空学报,1994,15(9):1110-1113. 被引量:3
  • 2李家军,额日其太.脉冲射流强化圆柱喷流混合的三维数值模拟[J].北京航空航天大学学报,2007,33(7):773-776. 被引量:4
  • 3邵万仁,尚守堂,张力,等.大涵道比涡扇发动机排气喷管技术分析.中国航空学会2007年学术年会,动力专题第46期,2007. 被引量:1
  • 4Csanady G T. The effect of mean velocity variations on jet noise. Journal of Fluid Mechanics, 1966, 26(1): 186-197. 被引量:1
  • 5Vinod G M, William N D. Lobed mixer design for noise suppression, acoustic and aerodynamic test data analysis. NASA/CR 2002-210823, 2002. 被引量:1
  • 6Tester B J, Fishe M J. A contribution to the understand ing and prediction of jet noise generation in forced mixers. AIAA 2004-2897, 2004. 被引量:1
  • 7Callender B, Gutmark E. Far-field acoustic investigation into chevron nozzle mechanisms and trends. AIAA Jour- nal, 2005, 43(1): 87-95. 被引量:1
  • 8Henderson B, Kinzie K. Aeroacoustic improvements to fluidic chevron nozzles. AIAA-2006 2706, 2006. 被引量:1
  • 9Calkins F T, Butler G W. Variable geometry chevrons for jet noise reduction. AIAA 2006-2546, 2006. 被引量:1
  • 10Papamoschou D. Noise suppression in moderate-speed multistream jets. AIAA-2002-2557, 2002. 被引量:1

共引文献32

同被引文献20

引证文献5

二级引证文献3

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部