主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司

声学超表面抑制Mack第2模态机理与优化设计

Investigation and Optimization of Acoustic Metasurfaces to Depress Mack Second Mode in Hypersonic Boundary-Layer Flow

  • 摘要: 从理论上推导了声学超表面对平面声波的作用模型,该理论模型计及声波高阶衍射模态,从而能够计及超表面微结构之间的声学干扰.通过与数值结果对比,该模型预测的反射频率精度得到了一定程度的提高,并能够分辨出相邻孔声场之间的耦合模态.讨论了声学超表面吸声特性与阻抗特性对高超声速边界层内Mack第2模态的抑制机理,研究发现通过设计超表面阻抗特性,使得入射声波与反射声波在壁面处相位相反,同样可以抑制Mack第2模态.基于理论模型,分别优化设计得到最优的微结构几何尺寸,并通过对Mach 6平板边界层流动进行稳定性分析,验证了超表面不同声学特性的抑制效果.

     

    Abstract: A theoretical model to describe the acoustic characteristics of plane ultrasonic acoustic waves imping on an acoustic metasurface was developed. The proposed model takes into account the high-order diffracted modes and therefore incorporates mutual coupling among neighboring cavities. With this model, the cavity geometry parameters were optimized to achieve the minimum reflection coefficient and impedance, respectively. Results reveal that the phase opposition between incident and reflective waves at the surface could largely depress the increment ratio of Mack second mode. The proposed effective impedance boundary could open up new possibilities of metasurfaces for hypersonic boundary-layer transition control.

     

/

返回文章
返回