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On the Flow Effects of a Small Device

机译:小型设备的流动效应

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An experimental and computational investigation of the interaction mechanismsbetween a single vortex generator (VG) and boundary layer (BL) flow is conducted. Theobjectives are to study the resulting flow-field characteristics and to validate acomputational model. The collected data may be analyzed to obtain simplified modelsfor use in the design case. An important parameter of the investigation is the relativeheights of the VG and the BL, with emphasis on the small device case.The investigated VG is a delta 60°, immersed in a turbulent BL. The ratio between theVG height and the BL thickness is 1/3. The experimental environment is obtained in awind-tunnel of long walls and low speed, where a VG is attached to the ceiling, inclined20°to the main flow. The procedure includes yaw meter measurements in the VG wakeand visualization of the limiting wall flow. CFD simulations performed by a Fluent 6.3numerical code are compared with the experimental findings to validate the theoreticalmodels and to gain more insight into the complex flow interaction.It is found that the VG has a large influence on the BL, despite its small relativedimensions. A wide mixing zone develops inside the BL and a correspondingenhancement of the BL momentum near the wall is obtained. A feeding layer is formedbetween the wall and the vortex, in addition to the known feeding sheet over the leadingedge. A shallow separation region of recirculation is found around the apex and down-streamat the pressure side. A complex wake structure is observed, including arelatively strong side-wash and high shear regions. A good agreement is obtainedbetween the computed results and the experimental data, but the computed diffusion atthe VG down-stream wake is greater than the experimental diffusion. This finding maybe explained by an insufficient density of the numerical grid at the wake region.
机译:相互作用机理的实验和计算研究 在单个涡流发生器(VG)和边界层(BL)之间进行流动。这 目的是研究由此产生的流场特征并验证 计算模型。可以对收集到的数据进行分析以获得简化的模型 用于设计案例。调查的一个重要参数是相对 VG和BL的高度,重点放在小型设备外壳上。 研究的VG为60°Δ,浸入湍流BL中。两者之间的比例 VG高度和BL厚度为1/3。实验环境是在 长壁低速风洞,VG安装在天花板上,倾斜 与主流呈20°角。该程序包括在VG尾迹中测量偏航仪 以及可视化的限制壁流。 Fluent 6.3执行的CFD模拟 将数字代码与实验结果进行比较以验证理论 模型,以更深入地了解复杂的流程交互。 发现相对于VG而言,VG对BL的影响很大 方面。 BL内部形成了一个宽广的混合区, 获得了壁附近BL动量的增强。形成进料层 在壁和涡旋之间,除了前导部分上的已知进料板之外 边缘。在顶端和下游附近发现了一个较浅的分离区 在压力侧。观察到复杂的尾流结构,包括 相对较强的侧洗区和高剪切区。获得了良好的协议 在计算结果和实验数据之间,但在 VG下游尾流大于实验扩散。这一发现可能 可以用尾流区域的数值网格密度不足来解释。

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