Applied Mathematics and Mechanics (English Edition) ›› 2008, Vol. 29 ›› Issue (8): 985-998 .doi: https://doi.org/10.1007/s10483-008-0802-3

• Articles • 上一篇    下一篇

超声速钝锥湍流边界层DNS入口边界条件的研究

董明1,2,周恒1   

  1. 1.天津大学 力学系,天津 300072;
    2.天津市现代工程力学重点实验室,天津 300072
  • 收稿日期:2008-06-16 修回日期:2008-06-24 出版日期:2008-08-18 发布日期:2008-08-18
  • 通讯作者: 周恒

Inflow boundary condition for DNS of turbulent boundary layers on supersonic blunt cones

DONG Ming1,2, ZHOU heng1   

  1. 1. Department of Mechanics, Tianjin University, Tianjin 300072, P. R. China;
    2. Tianjin Key Laboratory of Modern Engineering Mechanics, Tianjin 300072, P. R. China
  • Received:2008-06-16 Revised:2008-06-24 Online:2008-08-18 Published:2008-08-18

摘要: 如何选取适当的入口条件,是进行湍流边界层直接数值模拟时必须考虑的一个问题,为此建议了一种方法,只需要有平板湍流边界层时间模式直接数值模拟(DNS)所得的一个瞬时的流场,而且其Mach数、Reynolds数及壁面温度条件无需和实际问题中的完全相同,就可导出超声速钝锥湍流边界层空间模式直接数值模拟所需的入口条件.通过3个典型算例,将结果与用其它方法所得结果相比,证实了该方法的可行性.

关键词: 超声速, 湍流边界层, 直接数值模拟(DNS), 钝锥, 入口条件

Abstract: For direct numerical simulation (DNS) of turbulent boundary layers, generation of an appropriate inflow condition needs to be considered. This paper proposes a method, with which the inflow condition for spatial-mode DNS of turbulent boundary layers on supersonic blunt cones with different Mach numbers, Reynolds numbers and wall temperature conditions can be generated. This is based only on a given instant flow field obtained by a temporal-mode DNS of a turbulent boundary layer on a flat plate. Effectiveness of the method is shown in three typical examples by comparing the results with those obtained by other methods.

Key words: turbulent boundary layer, direct numerical simulation, supersonic, blunt cone, inflow condition

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