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Upstream condition effects on the evolution of symmetric and asymmetric near-wakes of a flat plate

机译:上游条件对平板对称和不对称近尾流演变的影响

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摘要

An experimental study was conducted in order to investigate the influence of upstream conditions with respect to near-wakes evolution by using a two-dimensional flat plate. A position of x_(B.L)/C =0.98 for the flat plate with a blunt trailing edge was settled upon as an upstream condition point. Three upstream conditions (i.e., natural laminar, bypass transitional, and turbulent boundary layers) were applied by tripping wires that were placed on the upper surface of the plate. The free-stream velocity was 6.0 m/s and the local Reynolds numbers based on momentum thickness at the upstream conditions point were 259, 303, and 331. The boundary layers and the near-wakes were measured by hot-wire anemometry. It was observed that for the symmetric near-wakes, the local similarity profiles of the mean defect velocity matched well with the traditional similarity profile in the center part, whereas some difference in the outer part occurred due to the different trailing edge shape. For the asymmetric upstream conditions, the center of the local similarity profiles moved to one side, and the amplitude of the local similarity profiles over the wakes edge varied according to the momentum thickness of the upstream conditions. Also, the collapse of the normalized Reynolds shear stress depended on turbulent quantities included in the upstream conditions, and these results showed that the evolution of the near-wakes is clearly affected by upstream conditions.
机译:为了研究上游条件对使用二维平板的近来尾流演变的影响,进行了实验研究。将具有钝后缘的平板的x_(B.L)/C=0.98的位置确定为上游条件点。通过放置在平板上表面的跳闸线施加三个上游条件(即自然层流,旁路过渡层和湍流边界层)。自由流速度为6.0 m / s,基于上游条件点动量厚度的局部雷诺数为259、303和331。边界层和近来苏醒是通过热线风速法测量的。可以看出,对于对称的近尾流,平均缺陷速度的局部相似度分布在中心部分与传统相似度分布很好地匹配,而外部部分由于后缘形状的不同而出现了一些差异。对于非对称上游条件,局部相似性轮廓的中心移到一侧,并且在尾流边缘上局部相似性轮廓的幅度根据上游条件的动量厚度而变化。同样,归一化雷诺剪切应力的崩溃取决于上游条件中包括的湍流量,这些结果表明,近流的演变显然受到上游条件的影响。

著录项

  • 来源
    《Aerospace science and technology》 |2010年第1期|49-55|共7页
  • 作者单位

    Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Hanggongdae gil 100 Hwajeon-dong, Deogyang-gu, Goyang city, Gyeonggi-Do, 412-791, Republic of Korea;

    Department of Aeronautical Science and Hight Operation, Korea Aerospace University, Hanggongdae gil 100 Hwajeon-dong, Deogyang-gu, Coyang city, Cyeonggi-Do, 412-791, Republic of Korea;

    Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Hanggongdae gil 100 Hwajeon-dong, Deogyang-gu, Goyang city, Gyeonggi-Do, 412-791, Republic of Korea;

    Department of Aerospace Engineering, Korea Air Force Academy, Ssangsuri, Namil-myun, Chungwon-gun, Chungbuk-Do, 363-849, Republic of Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    flat plate; turbulent boundary layer; upstream condition; near-wake; similarity profile; reynolds shear stress;

    机译:平板湍流边界层上游条件;近醒相似性雷诺剪切应力;
  • 入库时间 2022-08-18 02:37:10

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