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Management of Spatial Variation in Turbulent Boundary Layer by a Pair of streamwise Vortices with Spanwise Perturbation

Management of Spatial Variation in Turbulent Boundary Layer by a Pair of streamwise Vortices with Spanwise Perturbation
一对流向涡与展向扰动管理湍流边界层的空间变化
批准号:
12650171
负责人:
OSAKA Hideo
金额:
$2.18万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2000
资助国家:
日本
项目状态:
已结题
起止时间:
2000 至 2001

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中文摘要
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英文摘要
Interaction process between turbulent boundary layer and a pair of streamwise vortices with spanwise perturbation was investigated experimentally. The streamwise vortices were generated by a delta wing that is 50mm in cord length and 40mm in wingspan located in the free stream with 8 degree in angle of attack. Spanwise oscillation of the delta wing with constant frequencies 0.5Hz and 1Hz and 10mm amplitude added spanwise perturbation onto the streamwise vortex pair. Conventional time averages and ensembles averages were obtained by hot-wire measurements of fluctuation velocity field for the streamwise extent of 70 times initial boundary thickness at starting location for interaction between boundary layer and streamwise vortex. Concluding remarks are summarized in the following two pars such as time and ensemble averages and production process.[Time and ensemble averages] Local skin friction coefficient has spanwise variation depending on mean velocity profile and enhance the momentum transport. Spanwise perturbation somewhat leaves off the spanwise variation of the skin friction coefficient. However, spanwise integral of momentum transport shows that the spanwise perturbation has no substantial contribution to momentum transport across the boundary layer. Spanwise variation of mean velocity field and spanwise amplitude of perturbation contribute to magnitude of the ensemble average of streamwise fluctuation component. The any conventional average can be divided into ensemble average and random components. The log low profile can be observed through the streamwise extent.[Production process] Kinetic energy budget was investigated for time, ensemble and random components. Kinetic energy of random component is generated by spanwise oscillation around vortex core of the streamwise vortices. From investigation of production term in whole spanwise extent, there is no drag reduction phenomenon with the present management.
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小林 洋司: "横方向擾乱をもつデルタ翼から生成された縦渦対の挙動"日本機械学会中国四国支部第39期総会・講演会講演論文集. 015・1. 193-194 (2001)
小林洋二:“带有横向扰动的三角翼产生的纵向涡对的行为”日本机械工程学会中国四国分会第39次大会论文集和演讲(2001年193-194年) )
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大坂英雄: "横方向擾乱を加えた縦渦対と乱流境界層との干渉過程"日本機械学会2001年度年次大会講演論文集(II). 01・1. 217-218 (2001)
大阪秀夫:“横向扰动的纵向涡对与湍流边界层之间的干涉过程”日本机械工程学会2001年年会论文集(II)01・1(2001)。
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14
    Control of the Streaky Structure in Turbulent Boundary Layer by means of Streamwise Vortex Pair
    • 批准号:
      14350093
    • 项目类别:
      Grant-in-Aid for Scientific Research (B)
    • 资助金额:
      $4.42万
    • 财政年份:
      2002
    • 负责人:
      OSAKA Hideo
    • 依托单位:
    Management of the Turbulent Boundary Layer using the Strong Spanwise Deformation by a Pair of Streamwise Vortex
    • 批准号:
      09650191
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $1.79万
    • 财政年份:
      1997
    • 负责人:
      OSAKA Hideo
    • 依托单位:
    Vortex structure model in the turbulent boundary layr interacted with longitudinal vortex arrays (1996)
    • 批准号:
      07650208
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $1.41万
    • 财政年份:
      1995
    • 负责人:
      OSAKA Hideo
    • 依托单位:
    Internal mixing mechanism of a turbulent boundary layr formed by spanwise gaps between roughness element