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首页> 外文期刊>Journal of Fluid Mechanics >The naturally oscillating flow emerging from a fluidic precessing jet nozzle
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The naturally oscillating flow emerging from a fluidic precessing jet nozzle

机译:流体进动喷嘴产生的自然振荡流

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摘要

Phase-averaged and directionally triggered digital particle image velocimetry measurements were taken in longitudinal and transverse planes in the near field of the flow emerging from a fluidic precessing jet nozzle. Measurements were performed at nozzle inlet Reynolds and Strouhal numbers of 59000 and 0.0017, respectively. Results indicate that the jet emerging from the nozzle departs with an azimuthal component in a direction opposite to that of the jet precession. In addition, the structure of the 'flow convergence' region, reported in an earlier study, is better resolved here. At least three unique vortex-pair regions containing smaller vortical 'blobs' are identified for the first time. These include a vortex-pair region originating from the foci on the downstream face of the nozzle centrebody, a vortex-pair region shed from the edge of the centrebody and a vortex-pair region originating from the downstream surface of the nozzle exit lip.
机译:在从流体进动喷嘴产生的流动的近场中,在纵向和横向平面上进行了相位平均和方向触发的数字粒子图像测速仪的测量。在喷嘴入口的雷诺数和斯特劳哈尔数分别为59000和0.0017时进行测量。结果表明,从喷嘴射出的射流沿与射流进动方向相反的方向偏离了方位角分量。另外,在较早的研究中报道的“流动收敛”区域的结构在此得到更好的解决。首次识别出至少三个包含较小涡旋“斑点”的独特涡旋对区域。这些包括源自喷嘴中心体的下游面上的焦点的涡流对区域,源自中心体的边缘的涡流对区域以及源自喷嘴出口唇的下游表面的涡流对区域。

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