...
首页> 外文期刊>Journal of Fluid Mechanics >Cavitation dynamics and vortex shedding in the wake of a bluff body
【24h】

Cavitation dynamics and vortex shedding in the wake of a bluff body

机译:在虚张声势尾部的空化动力学和涡旋脱落

获取原文
获取原文并翻译 | 示例

摘要

Cavitating flow in the wake of a wedge-shaped bluff body is examined to understand the role of the presence of high void-fraction regions in the near-wake region on the process of vortex formation and shedding. Previous studies have noted that developed cavitation forming in the wake of bluff bodies typically leads to an increase in the vortex shedding rate, peaking at a particular cavitation number. Further reduction in cavitation number leads to a return to lower shedding rates as the cavity grows into a super-cavity. The underlying flow processes that lead to this phenomenon are explored using traditional flow visualisation combined with time-resolved void-fraction flow fields based on X-ray densitometry. These measurements allow us to relate the compressibility of the near-wake bubbly flow to the underlying flow processes. Specifically, we use proper orthogonal decomposition (POD) of the void-fraction fields to show that the increased rate of vortex shedding is associated with a pulsating mode of the void-fraction flow field, compared with a sinusoidal variation corresponding to the lower void-fraction shedding processes similar to that of the non-cavitating wake. The pulsating mode becomes more pronounced when the wake void fraction increases with decreasing cavitation number, with the maximum shedding occurring near the point that the wake flow becomes locally supersonic. The important influence of flow compressibility on the wake dynamics is confirmed through the examination of the effect of non-condensable gas injection.
机译:研究了楔形钝体尾迹中的空化流动,以了解近尾迹区高含气率区的存在对旋涡形成和脱落过程的作用。以前的研究已经指出,钝体尾迹中形成的空化通常会导致涡流脱落率增加,在特定空化数下达到峰值。空化数的进一步减少导致空化腔发展为超级空化腔时,空化率恢复到较低水平。利用传统的流动可视化技术,结合基于X射线密度测量的时间分辨空隙率流场,探索了导致这种现象的潜在流动过程。这些测量使我们能够将近尾迹泡状流的可压缩性与底层流动过程联系起来。具体而言,我们使用含气率场的固有正交分解(POD)来表明,与对应于与非空化尾迹相似的较低含气率脱落过程的正弦变化相比,涡流脱落率的增加与含气率流场的脉动模式有关。随着空化数的减少,尾迹空泡率增加时,脉动模式变得更加明显,最大脱落发生在尾迹流成为局部超音速的点附近。通过对不凝性气体注入效果的研究,证实了流动可压缩性对尾流动力学的重要影响。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号