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A NUMERICAL STUDY ON MECHANISM OF AERODYNAMIC NOISE REDUCTION BY POROUS MATERIAL

机译:多孔材料空气动力降噪机理的数值研究

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Vortex shedding behind bluff bodies slackens off and the resulting aerodynamic noise is well reduced when they are covered with porous materials. To clarify this mechanism we simulate a flow around a circular cylinder covered with a porous material. We perform a large eddy simulation at Reynolds number 100,000 to obtain the flow field around the circular cylinder. To solve the fluid flow with a porous interface, we impose a permeable boundary condition. The transpiration is assumed to be proportional to the local pressure fluctuation. The simulated flow fields are compared with experimental ones and good agreements are obtained. The computation reveals blowing flows at the porous interface play a vital role in the vortex shedding suppression. The mechanism is summarized as follows: 1) The blowing flow at the cylinder sides makes the flow separation points upstream along the body. It results in weakened the strength of the separated shear layers and increased a distance between the shear layers at both sides. The former eases the shear layer instability and the latter makes positions of the vortices formation downstream. 2) The blowing flow behind the cylinder decreases a reverse flow and therefore hinders the vortices formation.
机译:在虚张声势上放松凹部的涡流脱落,当用多孔材料覆盖时,由此产生的空气动力学噪音变得很好。为了阐明这种机制,我们模拟围绕着多孔材料覆盖的圆柱体的流动。我们在雷诺数100,000处执行大的涡流模拟,以获得圆柱周围的流场。为了解决多孔界面的流体流动,我们施加可渗透的边界条件。假设蒸腾率与局部压力波动成比例。将模拟的流场与实验结果进行比较,并且获得了良好的协议。该计算揭示了多孔界面处的吹流在涡旋脱落抑制中起着至关重要的作用。该机构总结如下:1)汽缸侧的吹流使流动分离点沿着主体上游。导致分离剪切层的强度削弱了分离的剪切层的强度,并增加了两侧剪切层之间的距离。前者简化了剪切层不稳定性,后者使涡流的位置在下游形成。 2)滚筒后面的吹流量降低了反向流动,因此阻碍了涡流形成。

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