首页> 外文会议>11th International Conference on Computational Methods and Experimental Measurements (CMEM 2003) 2003 Halkidiki, Greece >Investigation of vortex shedding in transitional separating ― reattaching flow on a blunt plate
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Investigation of vortex shedding in transitional separating ― reattaching flow on a blunt plate

机译:钝分离板上过渡分离-再附着流中涡旋脱落的研究

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It has been reported in transitional and turbulent separating-reattaching flows that different vortex shedding frequencies exist, in particular the so called low-frequency flapping. In addition it has been reported that a higher-frequency shedding also exists by Tafti and Vanka. It is quite debatable if these low and high frequency vortex shedding exist in all transitional and turbulent separating-reattaching flows. It is also not clear what the working mechanisms are behind the so called low-frequency flapping as reported by several researchers. The major purpose of the paper is trying to address these issues. Large-Eddy Simulation of the transitional flow over a blunt plate held normal to a uniform stream has been carried out to study the physics of separated boundary layer transition. The Reynolds number based on the uniform inlet velocity and the plate thickness is 6500. A dynamic subgrid-scale model is employed to compute the subgrid-scale stresses more accurately in the transitional flow case where the subgrid eddy-viscosity should be zero in the laminar region and starts to increase in the transition region and eventually to full turbulent value. Statistics of the LES are found to be in acceptable agreement with the available experimental data. Time histories of three velocity components and pressure have been taken at many selected points in the flow field, concentrated mainly in the separation bubble region. Detailed processing of these data has been done by Fourier analyses and comprehensive results will be presented.
机译:据报道,在过渡和湍流的分离-再附着流中,存在不同的涡旋脱落频率,特别是所谓的低频扑动。另外,据报道,塔夫蒂(Tafti)和万卡(Vanka)也存在较高频率的脱落。这些低频和高频涡旋脱落是否存在于所有过渡和湍流的分离-再附着流中,这是有争议的。正如一些研究人员所报道的那样,所谓的低频振荡背后的工作机制还不清楚。本文的主要目的是试图解决这些问题。为了研究分离的边界层过渡的物理过程,已经进行了大涡流模拟,该过渡流是保持在垂直于均匀流的钝板上的。基于均匀入口速度和板厚的雷诺数为6500。在层流中子网格涡流粘度应为零的过渡流动情况下,采用动态子网格比例模型来更准确地计算子网格比例应力。区域,并在过渡区域开始增加,最终达到全湍流值。发现LES的统计数据与可用的实验数据一致。在流场中许多选定的点上都记录了三个速度分量和压力的时间历史,主要集中在分离气泡区域。这些数据的详细处理已通过傅立叶分析完成,并将提供综合结果。

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