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
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
中文摘要
实验研究了湍流边界层与具有展向扰动的一对流向涡之间的相互作用过程。在8度迎角的自由流中,一个绳长50 mm、翼展40 mm的三角翼产生了顺流涡流。三角翼的展向振动频率为0.5赫兹和1赫兹,振幅为10毫米,在流向涡对上增加了展向扰动。对于边界层和流向涡相互作用的初始边界层厚度为70倍的流向范围内的脉动速度场,通过热线测量得到了常规的时间平均值和集合平均值。结束语概括为时间和集合平均以及生产过程两个部分。[时间和集合平均]局部表面摩擦系数随平均速度廓线而变化,增强了动量输送。跨向摄动在一定程度上忽略了侧摩阻力系数的跨向变化。然而,动量输送的展宽积分表明,展向摄动对跨边界层的动量输送没有实质性的贡献。平均速度场和扰动幅值沿展向的变化对流向脉动分量的集合平均值的大小有贡献。任何常规平均值可分为集合平均值和随机分量。[生产过程]对时间组分、系综组分和随机组分的动能收支进行了研究。随机分量的动能是在流向涡的涡核周围沿展向振荡产生的。从整个跨度范围内的生产条件考察,目前的管理不存在减阻现象。
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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Hideo Osaka: "Evolution of Turbulent Boundary Layer Distorted by a Pair of Streamwise Vortex"Prepr. Of Jpn. Soc. Mech. Eng. 005-2. 105-106 (2000)
Hideo Osaka:“一对流向涡旋扭曲的湍流边界层的演化”Prepr。
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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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Yoji Kobayashi: "Behavior of a Streamwise Vortex Pair Generated Spanwise Oscillating Delta Wing"Prepr. Of Jpn. Soc. Mech. Eng. 015-1. 193-194 (2001)
Yoji Kobayashi:“流向涡对产生翼展振荡三角翼的行为”准备。
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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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大坂 英雄: "主流中から導入した縦渦対と乱流境界層との干渉過程(平均速度場)"日本機械学会学術講演論文集(九州・中国四国支部合同企画). 018・2. 137-138 (2001)
大阪英夫:“从主流引入的纵向涡对与湍流边界层(平均速度场)之间的干涉过程”日本机械工程学会学术讲座论文集(九州分会和中国四国分会的联合项目) 018・2。137-138(2001)
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共 14 条
Control of the Streaky Structure in Turbulent Boundary Layer by means of Streamwise Vortex Pair
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批准号:14350093
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项目类别:Grant-in-Aid for Scientific Research (B)
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资助金额:$4.42万
-
财政年份:2002
-
负责人:OSAKA Hideo
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依托单位:
Management of the Turbulent Boundary Layer using the Strong Spanwise Deformation by a Pair of Streamwise Vortex
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批准号:09650191
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$1.79万
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财政年份:1997
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负责人:OSAKA Hideo
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依托单位:
Vortex structure model in the turbulent boundary layr interacted with longitudinal vortex arrays (1996)
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批准号:07650208
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$1.41万
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财政年份:1995
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负责人:OSAKA Hideo
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依托单位:
Internal mixing mechanism of a turbulent boundary layr formed by spanwise gaps between roughness element
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批准号:05650164
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.34万
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财政年份:1993
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负责人:OSAKA Hideo
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依托单位:
Relation between the large scale eddy in the plane wall jet and the turbulent generating mechanism
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批准号:03650148
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.28万
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财政年份:1991
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负责人:OSAKA Hideo
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依托单位:
Interaction of a bursting phenomena with a row of longitudinal vortices
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批准号:63550137
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.22万
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财政年份:1988
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负责人:OSAKA Hideo
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依托单位: