期刊文献+

Effects of injection temperature on the jet evolution under supercritical conditions 被引量:1

Effects of injection temperature on the jet evolution under supercritical conditions
原文传递
导出
摘要 A nitrogen jet with subcritical and supercritical injection temperatures injected into a supercritical environment, in which both the pressure and temperature exceed those of the thermodynamic critical state, has been investigated numerically using large-eddy simulation technique. The effects of the injection temperature on the flow evolution are studied. We find that the jet surface is more unstable with the instability waves growing up and rolling into a succession of ring vortices for supercritical injection temperature, and the jet surface is nearly straight with the strong density stratification suppressing the development of the instability waves for subcritical injection temperature. With increasing injection temperature, the spatial growth rate of the surface instability wave strengthens and the frequency of the most unstable mode increases. This behavior is of importance in enhancing the fluid mixing effect. The results obtained in this study provide physical insight into the understanding of fundamental mechanisms of the jet evolution under supercritical conditions. A nitrogen jet with subcritical and supercritical injection temperatures injected into a supercritical environment, in which both the pressure and temperature exceed those of the thermodynamic critical state, has been investigated numerically using large-eddy simulation technique. The effects of the injection temperature on the flow evolution are studied. We find that the jet surface is more unstable with the instability waves growing up and rolling into a succession of ring vortices for supercritical injection temperature, and the jet surface is nearly straight with the strong density stratification suppressing the development of the instability waves for subcritical injection temperature. With increasing injection temperature, the spatial growth rate of the surface instability wave strengthens and the frequency of the most unstable mode increases. This behavior is of importance in enhancing the fluid mixing effect. The results obtained in this study provide physical insight into the understanding of fundamental mechanisms of the jet evolution under supercritical conditions.
出处 《Chinese Science Bulletin》 SCIE EI CAS 2009年第22期4197-4204,共8页
基金 Supported by the National Natural Science Foundation of China (Grant No. 90405007) Fundamental Research Project of the Chinese Academy of Sciences (Grant No. CXJJ-237)
关键词 超临界条件 注射温度 进化 不稳定波 喷气 飞机表面 流体混合作用 注入氮气 large-eddy simulation, supercritical flow, turbulent jet, shear layer instability
  • 相关文献

参考文献14

二级参考文献35

  • 1JIANGYong QIURong ZHOUWei FANWeicheng.Conditional moment closure modeling of a lifted turbulent flame[J].Chinese Science Bulletin,2005,50(12):1261-1269. 被引量:4
  • 2王海峰,陈义良.抬举湍流H_2/N_2射流火焰的PDF模拟(英文)[J].计算物理,2006,23(1):73-79. 被引量:4
  • 3ZHAO YuXin YI ShiHe HE Lin CHENG ZhongYu TIAN LiFeng.The experimental study of interaction between shock wave and turbulence[J].Chinese Science Bulletin,2007,52(10):1297-1301. 被引量:18
  • 4Macha J M.Drag of circular cylinders at transonic mach numbers[].Journal of Aircraft.1977
  • 5Murthy V S,Rose W C.Detailed measurements on a circular cylin- der in cross flow[].AIAA Journal.1978
  • 6Botta N.The inviscid transonic flow about a cylinder[].Journal of Fluid Mechanics.1995
  • 7Pandolfi M,Larocca F.Transonic flow about circular cylinder[].Computers and Fluids.1989
  • 8Miserda R F B,Leal R G.Numerical simulation of the unsteady aerodynamic forces over a circular cylinder in transonic flow. AIAA Paper2006-1408 . 2006
  • 9Sagaut P,Deck S,Terracol M.Multiscale and Multiresolution Ap- proaches in Turbulence[]..2006
  • 10Simon F,Deck S,Guillen P, et al.Numerical simulation of the com- pressible mixing layer past an axisymmetric trailing edge[].Journal of Fluid Mechanics.2007

共引文献20

引证文献1

二级引证文献4

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