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An analysis of the acoustic energy in a flow duct with a vortex sheet

机译:用涡旋板流动管道中声能的分析

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Modelling the acoustic scattering and absorption at an area expansion in a flow duct requires the incorporation of the flow-acoustic interaction. One way to quantify the interaction is to study the energy in the incident and the scattered field respectively. If the interaction is strong, energy may be transferred between the acoustic and the main flow field. In particular, shear layers, that may he the result of the flow separation, are unstable to low frequency perturbations such as acoustic waves. The vortex sheet model is an analytical linear acoustic model, developed to study scattering of acoustic waves in duct with sharp edges including the interaction with primarily the separated flows that arise at sharp edges and corners. In the model the flow field at an area expansion in a duct is described as a jet issuing into the larger part of the duct. In this paper, the flow-acoustic interaction is described in terms of energy flow. The linear convective wave equation is solved for a two-dimensional, rectangular flow duct geometry. The resulting modes are classified as "hydrodynamic" and "acoustic" when separating the acoustic energy from the part of the energy arising from the steady flow field. In the downstream duct, the set of modes for this complex flow field are not orthogonal. For small Strouhal numbers, the plane wave and the two hydrodynamic waves are all plane, although propagating with different wave speeds. As the Strouhal numbers increases, the hydrodynamic modes changes to get a shape where the amplitude is concentrated near the vortex sheet. In an intermediate Strouhal number region, the mode shape of the first higher order mode is very similar to the damped hydrodynamic mode. A physical interpretation of this is that we have a strong coupling between the flow field and the acoustic field when the modes are non-orthogonal. Energy concepts for this duct configuration and mean flow profile are introduced. The energy is formulated such that the vortex sheet turns out as a sink for the acoustic field, but a source for the unstable hydrodynamic wave. This model is physical only close to the edge, due to an exponentially growing hydrodynamic mode. In a real flow, non-linearities will limit the growth, but this is not included in the model.
机译:在流动管道中建模声学散射和吸收,需要掺入流动声相互作用。量化相互作用的一种方法是分别研究入射和散射场中的能量。如果相互作用强,则可以在声学和主流场之间传递能量。特别地,剪切层,可以是流动分离的结果,对低频扰动(例如声波)不稳定。涡旋板模型是一种分析线性声学模型,用于研究管道中的声波的散射,其具有锋利的边缘,包括与锋利边缘和角落产生的分离的流动的相互作用。在模型中,管道中的区域膨胀处的流场被描述为喷射进入管道的较大部分。在本文中,根据能量流来描述流动声相互作用。线性对流波方程被解决为二维矩形流动管道几何形状。当将声能与来自稳定流场引起的能量的一部分分离时,所得模式被分类为“流体动力学”和“声学”。在下游管道中,该复杂流场的一组模式不是正交的。对于小斯特鲁姆数,平面波和两个流体动力波是所有平面,尽管以不同的波速传播。随着Strouhal数字的增加,流体动力学模式改变以获得振幅集中在涡流板附近的形状。在中间斯特鲁姆数区域中,第一高阶模式的模式形状与阻尼流体动力模式非常相似。对此的物理解释是,当模式是非正交时,我们在流场和声场之间具有强烈的耦合。引入了该管道配置的能量概念和平均流动轮廓。配方能量使得涡流作为声场的水槽,而是不稳定流体动力波的源极。由于流体动力学模式指数增长,该模型仅靠近边缘。在真实流动中,非线性将限制增长,但这不包括在模型中。

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