航空学报 > 2002, Vol. 23 Issue (5): 405-410

穿孔板切向流效应的理论和实验研究

景晓东, 孙晓峰   

  1. 北京航空航天大学动力系 北京 100083
  • 收稿日期:2002-01-17 修回日期:2002-09-01 出版日期:2002-10-25 发布日期:2002-10-25

INVESTIGATION OF GRAZING FLOW EFFECT ON THE IMPEDANCE OF A PERFORATED PLATE

JING Xiao-dong, SUN Xiao-feng   

  1. Department of Jet Propulsion,Beijing University of Aeronautics and Astronautics, Beijing 100083,China
  • Received:2002-01-17 Revised:2002-09-01 Online:2002-10-25 Published:2002-10-25

摘要: 建立了一种有关切向流对小孔声阻抗影响的小扰动势流模型,其要点是使用法向质点速度连续而非广为采用的质点位移连续边界条件来匹配小孔剪切层两侧的声场,并在小孔前缘施加Kutta条件以反映切向流效应的机理———锐缘处的声涡转化。模型中还包含了实际应用中经常遇到的小孔形状和穿孔板厚度两个重要因素。理论预测的声阻和声抗与实验结果良好吻合。

关键词: 涡声干涉, 穿孔板声衬, 剪切层, 小扰动理论

Abstract: A linearized potential flow model is developed to study the grazing flow effect on the acoustic impedance of a perforated plate. This model uses the particle velocity continuity boundary condition rather than the widely used displacement continuity to match the unsteady flowfields separated by the orifice shear layer. The underlying sound vortex interaction mechanism is taken into account by applying the Kutta at the leading edge of the orifice. The influences of the finite plate thickness and the orifice shape are also incorporated. Good agreement is obtained between the theoretical prediction and the experimental data both for the acoustic resistance and reactance.

Key words: sound-vortex interaction, perforated liner, shear layer, linear perturbation theory