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Proceeding of Second Symposium on Turbulence and Shear Flow Phenomena最新文献

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MEASUREMENT OF DEVELOPING TURBULENT FLOWS IN A ROTATING 90 DEGREE BEND WITH SQUARE CROSS-SECTION 方形截面90度旋转弯道内发展湍流的测量
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.2210
Y. Choi, K. Chun, Dong Chul Kim
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引用次数: 0
STEREOSCOPIC PIV MEASUREMENTS IN A JET IN CROSSFLOW 横流中射流的立体piv测量
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.1870
K. Meyer, O. Ozcan, P. S. Larsen, C. Westergaard
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引用次数: 3
DIRECT NUMERICAL SIMULATION OF INTERACTIONS BETWEEN A MIXING LAYER AND A WAKE AROUND A CYLINDER 混合层与圆柱体周围尾流相互作用的直接数值模拟
Pub Date : 1900-01-01 DOI: 10.1088/1468-5248/3/1/028
E. Lamballais, J. Silvestrini
Direct numerical simulations of turbulent flows around a cylinder are performed using the virtual boundary technique to model the presence of the obstacle. This method consists of the imposition of a no-slip boundary condition within the flow field, using a specific forcing term added to the momentum equation. In this paper, two different inflow conditions are considered upstream from the cylinder. In the first case, where the inflow conditions correspond to a constant velocity flow, common features of the cylinder wake dynamics are well recovered (three-dimensional vortex shedding) while turbulent statistics (mean velocity and Reynolds stresses) are in good agreement with previous experimental and numerical results. This clearly shows that a code based on high-order finite difference schemes combined with the virtual boundary method can lead to reliable results even if the grid is not well designed for the shape of the obstacle. In the second case, the inflow conditions correspond to a spatially developi...
利用虚拟边界技术模拟障碍物的存在,对圆柱周围的湍流进行了直接数值模拟。该方法包括在流场内施加无滑移边界条件,并在动量方程中加入特定的强迫项。本文考虑了气缸上游两种不同的流入条件。在第一种情况下,入流条件对应于等速流动,气缸尾迹动力学的共同特征(三维涡脱落)得到了很好的恢复,而湍流统计(平均速度和雷诺应力)与先前的实验和数值结果很好地吻合。这清楚地表明,基于高阶有限差分格式的代码与虚拟边界方法相结合,即使网格没有很好地设计成障碍物的形状,也可以得到可靠的结果。在第二种情况下,流入条件对应于空间发展。
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引用次数: 48
DIRECT NUMERICAL SIMULATION OF AN IMPINGING JET 冲击射流的直接数值模拟
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.1190
Yongmann M. Chung, K. Luo, John J. R. Williams
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引用次数: 4
LARGE EDDY SIMULATION USING EXPLICIT FILTERING IN TURBULENT CHANNEL FLOW 紊流通道中显式滤波的大涡模拟
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.1340
J. Gullbrand
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引用次数: 1
LEVEL-SET DYNAMICS AND MIXING EFFICIENCY OF PASSIVE AND ACTIVE SCALARS IN DNS AND LES OF TURBULENT MIXING LAYERS DNS和湍流混合层中被动和主动标量的水平集动力学和混合效率
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.1050
B. Geurts, Bert Vreman, H. Kuerten, K. Luo
The mixing efficiency in a turbulent mixing layer is quantified by monitoring the surface-area of level-sets of scalar fields. The Laplace transform is applied to numerically calculate integrals over arbitrary level-sets. The analysis includes both direct and large-eddy simulation and is used to assess the suitability of specific subgrid parameterizations in relation to predicting mixing efficiency. We incorporate several subgrid models in the comparison, e.g. the scale similarity model of Bardina, the dynamic eddy-viscosity model and the dynamic mixed model. For accurate predictions, dynamic models are favored. It is observed that the ratio between LES-filterwidth Δ and grid-spacing h has a considerable influence; a ratio of four appears suitable. Gravity driven flows can be modeled by 'active' scalar fields which couple to the momentum and energy equations. The significant increase in mixing efficiency due to buoyancy effects is directly quantified.
紊流混合层的混合效率是通过监测标量场水平集的表面积来量化的。应用拉普拉斯变换对任意水平集上的积分进行数值计算。该分析包括直接模拟和大涡模拟,并用于评估特定子网格参数化在预测混合效率方面的适用性。我们采用了几种子网格模型进行比较,如Bardina的尺度相似模型、动态涡粘模型和动态混合模型。为了准确预测,动态模型更受青睐。结果表明,les滤波器宽度Δ与栅格间距h的比值对其影响较大;比率为4似乎比较合适。重力驱动的流动可以通过与动量和能量方程耦合的“活动”标量场来建模。浮力效应对混合效率的显著提高进行了直接量化。
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引用次数: 0
EVOLUTION AND GROWTH OF LARGE SCALE STRUCTURES IN HIGH COMPRESSIBILITY MIXING LAYERS 高压缩性混合层中大尺度结构的演化与成长
Pub Date : 1900-01-01 DOI: 10.1088/1468-5248/3/1/009
T. Rossmann, M. Mungal, R. Hanson
The basic physical mechanisms for shear layer growth have been shown in computations to change at very high compressibilities. A double diaphragm, shock tunnel driven hypersonic mixing layer facility is used to reach compressibility levels not possible in blowdown-type facilities. Mixing layers at M c  = 0.86 and 1.7 are examined in streamwise, plan, and end views using Schlieren and acetone planar laser-induced fluorescence imaging schemes. Analysis of these images yields normalized shear layer growth rates, concentration information on the fast side of the shear layer, and visualization of the behaviour of large-scale structures along with the associated acoustic radiation. Normalized growth rate data are reported for M c  = 0.80–2.25 as derived from averaged Schlieren images. This article was chosen from selected Proceedings of the Second International Symposium on Turbulence and Shear Flow Phenomena (KTH-Stockholm, 27-29 June 2001) ed E Lindborg, A Johansson, J Eaton, J Humphrey, N Kasagi, M Leschzine...
剪切层生长的基本物理机制已经在计算中显示在非常高的压缩性下发生变化。采用双隔膜激波隧道驱动的高超声速混合层设施,可达到排污式设施无法达到的可压缩性水平。采用纹影和丙酮平面激光诱导荧光成像方案,对mc = 0.86和1.7处的混合层进行了流式、平面和端视图的检测。对这些图像的分析可以得到归一化的剪切层生长速率、剪切层快速侧的浓度信息,以及大尺度结构的行为以及相关的声辐射的可视化。归一化的增长率数据报告,mc = 0.80-2.25,从平均纹影图像导出。本文选自第二届国际湍流和剪切流动现象研讨会论文集(KTH-Stockholm, 2001年6月27-29日),作者E Lindborg, A Johansson, J Eaton, J Humphrey, N Kasagi, M Leschzine…
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引用次数: 63
TURBULENT STRUCTURE OF COMBINED-CONVECTION BOUNDARY LAYER ALONG A VERTICAL HEATED PLATE 垂直加热板上联合对流边界层的湍流结构
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.410
Y. Hattori, T. Tsuji, Y. Nagano, Nobukazu Tanaka
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引用次数: 0
REFRACTIVE INDEX MATCHED LDA TECHNIQUE FOR INVESTIGATIONS OF LAMINAR TO TURBULENT BOUNDARY LAYER TRANSITION 折射率匹配lda技术用于层流到湍流边界层转换的研究
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.850
S. Becker, C. Stoots, H. Lienhart, D. McEligot, F. Durst
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引用次数: 1
QUASI-PERIODIC GENERATION OF COHERENT VORTICAL STRUCTURES BEHIND A SURFACE-MOUNTED OBSTACLE 表面障碍物后相干旋涡结构的准周期生成
Pub Date : 1900-01-01 DOI: 10.1615/tsfp2.1240
T. Baur, Joachim von Lukowicz, J. Köngeter
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引用次数: 0
期刊
Proceeding of Second Symposium on Turbulence and Shear Flow Phenomena
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