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首页> 外文期刊>Journal of the Brazilian Society of Mechanical Sciences and Engineering >A Lagrangian roughness model integrated with the vortex method for drag coefficient estimation and flow control investigations around circular cylinder for a wide range of Reynolds numbers
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A Lagrangian roughness model integrated with the vortex method for drag coefficient estimation and flow control investigations around circular cylinder for a wide range of Reynolds numbers

机译:拉格朗日粗糙度模型与涡旋法相结合,用于圆柱体周围各种雷诺数的阻力系数估计和流量控制研究

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This paper describes the development of a Lagrangian roughness model to simulate the effect of surface roughness in two-dimensional flow on the proximity of the cylinder, at high Reynolds numbers. The designed numerical model introduces a dynamic disturbance in the vicinity of the wall in addition to the distribution of triangular roughness elements in the body using the panel method, consolidating a refined boundary layer condition. A new discretization strategy for the vorticity field is used to make up a wide range of Reynolds numbers, 2 x 10(4) <= Re <= 6 x 10(5), which also ensures control of turbulence. It is integrated with the discrete vortex method-DVM and the second-order velocity structure function is applied for turbulence closure. The main findings are that numerically the drag coefficient depends on the relative roughness, the Reynolds number and the cutoff width of the characteristic vorticity distribution; the largest reductions in drag are observed for intermediate roughness compared to a smooth surface, reaching 51.6 for a relative roughness of 0.003 and Reynolds number set at 1.0 x 10(5); the core sizes of the discrete vortex need to be generated with different sizes for correct enforcement of the wall influence; it is possible to map the drag crisis under various flow conditions in cylinders with different surfaces, without the use of refined meshes and wall functions, using the DVM. OpenMP is implemented for average reductions of 80 in processing time. The considerable closeness with the experimental results reflects the applicability of the proposed method and the relevance of the two-dimensional approach for predicting unsteady aerodynamic forces on a cylinder with different rough surfaces for engineering purposes.
机译:本文描述了拉格朗日粗糙度模型的发展,以模拟二维流动中表面粗糙度对圆柱体接近度的影响,在高雷诺数下。所设计的数值模型除了采用面板方法在主体内分布三角形粗糙度单元外,还引入了墙体附近的动态扰动,巩固了精细的边界层条件。涡度场的新离散化策略用于构成广泛的雷诺数,2 x 10(4) <= Re <= 6 x 10(5),这也确保了对湍流的控制。与离散涡旋法-DVM集成,应用二阶速度结构函数进行湍流闭合。主要结果表明,阻力系数在数值上取决于相对粗糙度、雷诺数和特征涡度分布的截止宽度;与光滑表面相比,中间粗糙度的阻力降低幅度最大,相对粗糙度为 0.003 且雷诺数设置为 1.0 x 10(5) 时达到 51.6%;离散涡旋的核心尺寸需要生成不同尺寸,以正确执行壁面影响;使用 DVM 可以在具有不同表面的圆柱体中映射各种流动条件下的阻力危机,而无需使用精细的网格和壁函数。OpenMP 的实施旨在平均减少 80% 的处理时间。与实验结果的相当接近反映了所提方法的适用性以及二维方法在预测具有不同粗糙表面的气缸上的非定常空气动力的工程目的的相关性。

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