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COMPUTATIONAL INVESTIGATION OF BACKWARD-FACING STEP FLOW PRECEDING A POROUS MEDIUM

机译:在多孔介质之前的向后步流的计算研究

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Optimal performance of air filters and heat exchangers requires uniform inlet flow, but flow separation produces nonuniformity. The backward-facing step flow has a separation resembling those found in industrial flows. Flow resistance of the devices is a parameter which alters upstream pressure gradients, thereby affecting separation and device performance. Air filters often are modeled as porous media using an extended Darcy Law. The present work applied Computational Fluid Dynamics (CFD) to examine the changes in the step flow resulting from the resistance of a downstream air filter. Computations were performed for a backward-facing step with a 2:1 expansion ratio for a case without a filter (reattachment at ~6 step heights) and for filters located 4.25 and 6.75 step heights downstream. FLUENT commercial CFD software was used and results were compared to many no-filter case results in the literature and our own experimental studies for the step with downstream filters. The simulations were performed for Reynolds numbers based on approach channel mean velocity and hydraulic diameter of 2000, 3750, 6550 and 10000. The different turbulence models available in FLUENT were evaluated and the Realizable k-ε model was used for the final computations. Grid independence studies were conducted. The effects of different values of the filter modeling permeability, inertial constant and thickness also were investigated for Re = 10000 with the filter at 4.25 step heights. It was found that thecomputational results did not compare well to no-filter cases or the experiments with filters at the lower Reynolds numbers. It is believed that the turbulence models were unsuitable for these flows at transitional Reynolds numbers. Good agreement for no-filter results and for the experiments with filters was observed for Re = 10,000. The CFD model seems to capture the physics of the separation better at the higher Reynolds numbers. The CFD velocity profiles at Re = 10,000 with the filters agree with those of the experiments. When the filter is placed at 4.25 step heights, the flow reattaches upstream of the filter with a reduction in recirculation area. When the filter is at 6.75 step heights, the separated flow tends to reattach and the opposite side tends to separate. At Re = 10,000 and the filter at 4.25 step heights, the variations of porous medium permeability, inertial constant and the filter thickness have negligible effects on the recirculation region over the parameter ranges considered.
机译:空气过滤器和热交换器的最佳性能需要均匀的入口流量,但流量分离会产生不均匀性。后向步进流的分离类似于工业流中的分离。装置的流动阻力是改变上游压力梯度,从而影响分离和装置性能的参数。经常使用扩展的达西定律将空气过滤器建模为多孔介质。本工作应用计算流体动力学(CFD)来检查由下游空气过滤器的阻力引起的阶跃流的变化。对于没有过滤器的情况(以〜6步高重新安装)以及位于下游4.25和6.75步高的过滤器,以2:1的膨胀比执行向后步的计算。使用FLUENT商业CFD软件,并将结果与​​文献和我们自己的下游过滤器步骤实验研究中的许多无过滤器案例结果进行了比较。根据进近通道的平均速度和水力直径2000、3750、6550和10000对雷诺数进行了仿真。对FLUENT中可用的不同湍流模型进行了评估,并将Realizablek-ε模型用于最终计算。进行了电网独立性研究。在Re = 10000的情况下,还研究了过滤器建模渗透率,惯性常数和厚度的不同值对Re = 10000的影响,其中过滤器的步距为4.25。发现, 计算结果与没有过滤器的情况或以雷诺数较低的过滤器进行的实验相比效果不佳。据认为,湍流模型不适用于过渡雷诺数下的这些流动。对于无过滤器的结果和使用过滤器的实验,Re = 10,000的结果吻合良好。 CFD模型似乎可以在较高的雷诺数下更好地捕捉分离的物理现象。使用过滤器在Re = 10,000时的CFD速度曲线与实验结果一致。当将过滤器放置在4.25的台阶高度时,流体会重新附着在过滤器的上游,从而减少了再循环面积。当过滤器处于6.75的台阶高度时,分离的气流趋于重新附着,相反的一侧趋于分离。在Re = 10,000且过滤器的高度为4.25的情况下,在所考虑的参数范围内,多孔介质渗透率,惯性常数和过滤器厚度的变化对再循环区域的影响可忽略不计。

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