...
首页> 外文期刊>Physics of fluids >Fluid-acoustic interactions in self-sustained oscillations in turbulent cavity flows. I. Fluid-dynamic oscillations
【24h】

Fluid-acoustic interactions in self-sustained oscillations in turbulent cavity flows. I. Fluid-dynamic oscillations

机译:湍流腔流中自持振荡中的流体声相互作用。 I.流体动力振荡

获取原文
获取原文并翻译 | 示例
           

摘要

The fluid-acoustic interactions in a flow over a two-dimensional rectangular cavity are investigated by directly solving the compressible Navier-Stokes equations. The upstream boundary layer is turbulent. The depth-to-length ratio of the cavity is 0.5. Phase-averaged flow fields reveal the mechanism for the acoustic radiation. Large-scale vortices form in the shear layer that separates from the upstream edge of the cavity. When a large-scale vortex collides with the downstream wall, the low-pressure fluid in the vortex spreads along the downstream wall. As a result, a local downward velocity is induced by the local pressure gradient, causing the upstream fluid to expand. Finally, an expansion wave propagates to the outside of the cavity. The large-scale vortices originate from the convective disturbances that develop in the shear layer. The disturbances grow due to the Kelvin-Helmholtz instability, similar to the growth of those in a laminar cavity flow. To clarify the mechanism for the generation of the initial convective disturbances, computations for backward-facing step flows with an artificial acoustic source are also performed. As the artificial acoustic waves become more intense, the initial convective disturbances in the shear layer become more intense while the spatial growth rate of these disturbances does not change. This means that the initial convective disturbances in the shear layer are induced by the acoustic waves.
机译:通过直接求解可压缩的Navier-Stokes方程,研究了二维矩形腔上的流动中的流体声相互作用。上游边界层是湍流的。空腔的深度与长度之比为0.5。相平均流场揭示了声辐射的机理。在与腔室上游边缘分开的剪切层中形成了大型旋涡。当大涡旋与下游壁碰撞时,涡旋中的低压流体沿下游壁扩散。结果,局部压力梯度引起局部向下的速度,导致上游流体膨胀。最后,膨胀波传播到空腔的外部。大规模涡旋是由剪切层中产生的对流扰动引起的。由于开尔文-亥姆霍兹(Kelvin-Helmholtz)不稳定性,扰动增大,类似于层流中的扰动增大。为了阐明产生初始对流扰动的机制,还使用人工声源对后向阶跃流进行了计算。当人造声波变得更强时,剪切层中的初始对流扰动变得更强,而这些扰动的空间增长率没有改变。这意味着剪切层中的初始对流扰动是由声波引起的。

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