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Numerical Investigation of Ultrasonically Absorptive Coating for Hypersonic Laminar Flow Control

机译:高超音速层流控制的超声吸收涂层的数值研究

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Parametric studies on porosity and aspect ratio of ultrasonically absorptive coating are performed using a theoretical model. The fluctuation of reflection coefficient is caused by the reinforcement and cancellation of bottom reflection. At altitude H* =30km, the reflection coefficient decreases clearly with increasing porosity. The fluctuation of reflection coefficient decreases with decreasing aspect ratio. This phenomenon reveals that the bottom reflection attenuates due to the high viscous dissipation for low aspect ratio ultrasonically absorptive coating. The linear stability theory is employed to analyze the growth rates of Mack mode developing on flat plate and ultrasonically absorptive coating. The growth rates from present method agree well with the existing data. In contrast to the UAC of n = 16, the fluctuations of pressure and vertical velocity for the UAC of n = 8 are less concentrated, which corresponds to a lower growth rate. A computational aeroacoustics method is implemented based on a 2-2 MacCormack scheme to explore the reflection phenomenon of acoustic wave. The acoustic wave reflections for flat plate and ultrasonically absorptive coating are successfully captured by current computational aeroacoustics method.
机译:使用理论模型对超声吸收涂层的孔隙率和纵横比进行参数研究。反射系数的波动是由底部反射的增强和消除引起的。在高度H * = 30km处,反射系数随孔隙度的增加而明显降低。反射系数的波动随着纵横比的减小而减小。这种现象表明,对于低长宽比的超声波吸收涂层,由于高粘性耗散,底部反射会衰减。线性稳定性理论用于分析在平板和超声吸收涂层上形成的Mack模式的生长速率。现有方法的增长率与现有数据非常吻合。与n = 16的UAC相比,n = 8的UAC的压力和垂直速度波动集中程度较低,这对应于较低的生长速率。基于2-2 MacCormack方案实现了一种计算航空声学方法,以探索声波的反射现象。平板和超声吸收涂层的声波反射已通过当前的计算航空声学方法成功捕获。

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