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Computation of Aeolian Tones from Twin-Cylinders Using Immersed Surface Dipole Sources

机译:使用沉浸式表面偶极子源计算双圆柱的风音

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Efficient numerical method is developed for the prediction of aerodynamic noise generation and propagation in low Mach number flows such as aeolian tone noise. The proposed numerical method is based on acoustic/viscous splitting techniques of which acoustic solvers use simplified linearised Euler equations, full linearised Euler equations and nonlinear perturbation equations as acoustic governing equations. All of acoustic equations are forced with immersed surface dipole model which is developed for the efficient computation of aerodynamic noise generation and propagation in low Mach number flows in which dipole source, originating from unsteady pressure fluctuation on a solid surface, is known to be more efficient than quadrupole sources. Multi-scale overset grid technique is also utilized to resolve the complex geometries. Initially, aeolian tone from single cylinder is considered to examine the effects that the immersed surface dipole models combined with the different acoustic governing equations have on the overall accuracy of the method. Then, the current numerical method is applied to the simulation of the aeolian tones from twin cylinders aligned perpendicularly to the mean flow and separated 3 diameters between their centers. In this configuration, symmetric vortices are shed from twin cylinders, which leads to the anti-phase of the lift dipoles and the in-phase of the drag dipoles. Due to these phase differences, the directivity of the fluctuating pressure from the lift dipoles shows the comparable magnitude with that from the drag dipoles at 10 diameters apart from the origin. However, the directivity at 100 diameters shows that the lift-dipole originated noise has larger magnitude than, but still comparable to, that of the drag-dipole one. Comparison of the numerical results with and without mean flow effects on the acoustic wave emphasizes the effects of the sheared background flows around the cylinders on the propagating acoustic waves, which is not generally considered by the classic acoustic analogy methods. Through the comparison of the results using the immersed surface dipole models with those using point sources, it is demonstrated that the current methods can allow for the complex interactions between the acoustic wave and the solid wall and the effects of the mean flow on the acoustic waves.
机译:开发了一种有效的数值方法来预测空气动力学噪声在低马赫数流中的产生和传播,如风音噪声。所提出的数值方法基于声学/粘滞分裂技术,其中声学求解器使用简化的线性化Euler方程,完全线性化的Euler方程和非线性摄动方程作为声学控制方程。所有声学方程都被浸入式表面偶极子模型强制,该模型是为有效计算低马赫数流中的空气动力学噪声的产生和传播而开发的,其中偶极子源源自固体表面的不稳定压力波动,因此更加有效。比四极子源多尺度覆盖网格技术也被用来解决复杂的几何形状。最初,考虑来自单个圆柱体的风声,以检查浸入式表面偶极子模型与不同的声学控制方程式相结合对方法整体精度的影响。然后,将当前数值方法应用于模拟垂直于平均流量并在其中心之间分开3个直径的双圆柱的风音。在这种配置中,对称的涡流从双圆柱体上散发出去,这导致了升力偶极子的反相和阻力偶极子的同相。由于这些相位差,来自提升偶极子的脉动压力的方向性在与原点相距10个直径处显示出与来自阻力偶极子的脉动压力可比的幅度。但是,在100个直径处的方向性表明,由偶极子产生的噪声的大小大于但仍与偶极子噪声的大小相当。比较有无平均声波对声波的影响的数值结果强调了在圆柱体周围剪切的背景流对传播的声波的影响,这在经典的声波模拟方法中通常没有考虑。通过将浸入式表面偶极子模型与点源模型的结果进行比较,证明了当前方法可以考虑声波与固体壁之间的复杂相互作用以及平均流对声波的影响。

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