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Numerical simulation of two-dimensional turbulence based on Immersed Boundary Lattice Boltzmann method

机译:基于浸没边界格螺栓玻璃法的二维湍流数值模拟

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The two-dimensional turbulence is numerically investigated using Immersed Boundary Lattice Boltzmann Method. The 2D turbulence should be considered as 2D channel flow where the flow is forced by the arrays of cylinders vertically placed in the inlet of 2D channel. The inverse cascade in two cases, the normal wall boundary case and rough wall boundary case, is obtained in the inertial range. The scaling behavior of energy spectrum in the inverse cascade is k(-5/3), which is according with the Kraichnan theory of 2D turbulence. It is found that the time-evolving vortex number density distribution n(A) similar to t(-1) A(-1), based on the Rortex vortex definition criterion, which is in fair agreement with the theory of Burgess and Scott at intermediate scales sufficiently far from the forcing and the largest vortex scale. The energy flux of the normal wall boundary case cascades to the large scale. The energy flux of the rough wall boundary case cascades to large scale when the scale l< D. The energy flux at l> D cascades to the small scale. The energy dissipation filed epsilon(l) coarse grained at the scale l has the pow-law behaviors with the scale. The intermittency measured by PDF exists in the inverse inertial range of 2D turbulence. On the basis of the vortex scaling law of Burgess and Scott and our simulation results, the universal scaling law of velocity structure function in the inverse cascade is obtained by extending the 3D turbulent S-L intermittency model to the inverse inertial range of 2D turbulence. (C) 2019 Elsevier Ltd. All rights reserved.
机译:使用浸没边界格子Boltzmann方法进行数值研究二维湍流。 2D湍流应被认为是2D通道流,其中通过垂直放置在2D通道的入口中的圆柱体的阵列被迫使流动。在两个情况下,在惯性范围内获得正常壁边界壳体和粗糙壁边界壳体的逆级联。逆级联中的能谱的缩放行为是K(-5/3),其是根据kraichnan理论的2D湍流。发现,基于Rortex Vortex定义标准,类似于T(-1)A(-1)的时间不断发展的涡旋数密度分布n(a),这与Burgess和Scott的理论公平协议中间尺度远远远离迫使和最大的涡旋量表。正常墙边界盒的能量通量级联到大规模。当刻度L D级联的能量通量梯级。在规模L处粗糙粒度的epsilon(l)粗粒子的能量耗散粗糙的血管粒度具有规模。通过PDF测量的间歇性存在于2D湍流的反向惯性范围内。在抗核欲绝和斯科特的涡旋扩大法和模拟结果的基础上,通过将3D湍流S-L间歇性模型扩展到逆型湍流的逆惯性范围来获得逆级联中的速度结构功能的通用缩放规律。 (c)2019年elestvier有限公司保留所有权利。

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