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FLOW FEATURES IN A FULLY DEVELOPED RIBBED DUCT FLOW AS A RESULT OF LES

机译:LES结果导致充分发展的带肋管道流动的流动特征

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The present contribution concerns the simulation of a turbulent flow in a stationary square section ribbed duct by means of LES method. The pitch distance of the ribs was fixed to p/h=10, together with a high blockage value of 0.3 h/D, and a Reynolds number (defined with bulk velocity (U) and hydraulic diameter (D)) of 40000. These parameters were chosen to reproduce the experiments of Casarsa (2003). An attempt of topology description is proposed, using concepts of streamsurface, vortex core detection, wall streamline and bifurcation lines. Furthermore, knowledge on flow topology derived from these concepts is qualitatively compared with isosurface of second scalar invariant of the velocity gradient tensor (Q) used on the averaged and/or instantaneous velocity fields. Differences between a 2D ribbed channel and the present flow, where sidewall effect are dominants, are highlighted. Especially, the existence of a strong secondary flow on the windward side of the rib is revealed by the visualization of streamsurfaces, wall streamlines and bifurcation lines. Vorticity dominated regions are detected and extracted using isosurfaces of the (Q). Thanks to well-positioned streamsurfaces and a vortex core detection method, the effect of the lateral walls on the wake of the rib is put in evidence. Apart of this analysis of the average velocity field, a sequence of instantaneous images displaying creation of coherent structures on the leading edge of the rib is presented. These spanwise structures are shaped in Lambda (Λ) type vortices by a mechanism similar than the one already described in Dubief & Delcayre (2000), showing the capabilities of the present approach to reproduce averaged and instantaneous features of complex flows.
机译:本贡献涉及通过LES方法模拟固定方形截面肋形管道中的湍流。肋的间距固定为p / h = 10,同时具有0.3 h / D的高阻值和40000的雷诺数(由体速度(U)和水力直径(D)定义)。选择参数以再现Casarsa(2003)的实验。提出了使用流面,涡流核心检测,壁流线和分叉线的概念进行拓扑描述的尝试。此外,定性地比较了从这些概念得出的关于流动拓扑的知识与在平均和/或瞬时速度场上使用的速度梯度张量(Q)的第二标量不变式的等值面。突出显示了2D带肋通道与当前流量之间的差异,其中侧壁效应占主导地位。尤其是,通过观察水流表面,壁流线和分叉线,可以看出肋骨上风侧存在强的二次流。使用(Q)的等值面检测并提取涡度为主的区域。得益于良好定位的水流表面和涡流核心检测方法,可以证明侧壁对肋骨尾迹的影响。除了对平均速度场的分析之外,还提供了一系列瞬时图像,这些图像显示了肋骨前缘上连贯结构的创建。这些跨展结构在Lambda(Λ)型涡旋中的形成机制与Dubief&Delcayre(2000)中已经描述的机制相似,显示了本方法再现复杂流的平均和瞬时特征的能力。

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