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三棱柱的低雷诺数绕流研究

陆建洲 陶建军

陆建洲, 陶建军. 三棱柱的低雷诺数绕流研究[J]. 航空动力学报, 2016, 31(5): 1226-1233. doi: 10.13224/j.cnki.jasp.2016.05.026
引用本文: 陆建洲, 陶建军. 三棱柱的低雷诺数绕流研究[J]. 航空动力学报, 2016, 31(5): 1226-1233. doi: 10.13224/j.cnki.jasp.2016.05.026
LU Jian-zhou, TAO Jian-jun. Low-Reynolds-number wake flows of a triangular prism[J]. Journal of Aerospace Power, 2016, 31(5): 1226-1233. doi: 10.13224/j.cnki.jasp.2016.05.026
Citation: LU Jian-zhou, TAO Jian-jun. Low-Reynolds-number wake flows of a triangular prism[J]. Journal of Aerospace Power, 2016, 31(5): 1226-1233. doi: 10.13224/j.cnki.jasp.2016.05.026

三棱柱的低雷诺数绕流研究

doi: 10.13224/j.cnki.jasp.2016.05.026
基金项目: 

国家自然科学基金(11225209)

详细信息
    作者简介:

    陆建洲(1992-),男,江苏盐城人,博士生,主要从事流动稳定性与转捩方面的研究.

  • 中图分类号: V211;O357.4+1

Low-Reynolds-number wake flows of a triangular prism

  • 摘要: 数值模拟了截面为等腰三角形的棱柱在不可压牛顿流体中的二维绕流问题,分析了不同的截面尺度比以及三角形顶点迎风和背风安置时的尾流稳定性与阻力系数.研究发现对于较大截面尺度比的棱柱,在相同雷诺数的情况下顶点迎风相较于顶点背风的情况更易失稳从而产生侧向力,但阻力系数相对较小,当雷诺数为160时,最多能够减少19.4%.进一步地对比研究了顶点迎风与顶点背风在不同截面尺度比时升、阻力系数及涡脱落频率随雷诺数的变化关系.

     

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出版历程
  • 收稿日期:  2014-05-21
  • 刊出日期:  2016-05-28

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