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Flow Characterization and Modeling of Strong Round Synthetic Jets in Crossflow

机译:横流中强圆形合成射流的流动特性与建模

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摘要

This study focuses on the flow field of a round synthetic jet issuing into a crossflow. Six cases are investigated in which the jet-to-freestream velocity ratios range between 2.8 and 8.3. This corresponds to a medium-to-strong transverse jet, which is characterized using both two-dimensional hot-wire anemometry and particle image velocimetry techniques. A self-similar model is developed for the centerline trajectory and velocity of a transverse synthetic jet. The resulting scaling laws are validated with experimental data. The scaling coefficients are found to be independent of the synthetic jet strength (characterized by the stroke ratio) for large-velocity-ratio cases, provided that the jet velocity is calculated based on the momentum flux of the leading vortex ring of the synthetic jet. Furthermore, the velocity component parallel to the crossflow is enhanced over the crossflow velocity in the near field and fundamentally different from continuous jets. This can be explained by the induced effect of the asymmetric vortex rings in the near field, which are a result of the interaction between the crossflow and the synthetic jet.
机译:这项研究的重点是圆形合成射流发出横流的流场。研究了六种情况,其中射流与自由流的速度比在2.8和8.3之间。这对应于中等至强的横向射流,该射流同时使用二维热线风速测定法和粒子图像测速技术来表征。针对横向合成射流的中心线轨迹和速度,开发了自相似模型。由此产生的比例定律已通过实验数据进行了验证。如果比例速度是根据合成喷嘴前涡流环的动量通量计算得出的,则比例系数与大流量比情况下的合成喷嘴强度(以冲程比为特征)无关。此外,平行于错流的速度分量比近场中的错流速度提高,并且与连续射流根本不同。这可以通过近场中非对称涡流环的感应效应来解释,这是横流与合成射流之间相互作用的结果。

著录项

  • 来源
    《AIAA Journal》 |2017年第2期|389-402|共14页
  • 作者

    Xia Xi; Mohseni Kamran;

  • 作者单位

    Univ Florida, Dept Mech & Aerosp Engn, Gainesville, FL 32611 USA;

    Univ Florida, Dept Mech & Aerosp Engn, Gainesville, FL 32611 USA|Univ Florida, Dept Elect & Comp Engn, Gainesville, FL 32611 USA;

  • 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

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