首页 | 本学科首页   官方微博 | 高级检索  
     检索      

穿孔板切向流效应的理论和实验研究
引用本文:景晓东,孙晓峰.穿孔板切向流效应的理论和实验研究[J].航空学报,2002,23(5):405-410.
作者姓名:景晓东  孙晓峰
作者单位:北京航空航天大学,动力系,北京,100083
基金项目:国家自然科学基金 (5 0 13 60 10,5 992 5 616),航空基础科学基金 (0 0C5 10 40 )资助项目
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  
文章编号:1000-6893(2002)05-0405-06
修稿时间:2002年1月17日

INVESTIGATION OF GRAZING FLOW EFFECT ON THE IMPEDANCE OF A PERFORATED PLATE
JING Xiao dong,SUN Xiao feng.INVESTIGATION OF GRAZING FLOW EFFECT ON THE IMPEDANCE OF A PERFORATED PLATE[J].Acta Aeronautica et Astronautica Sinica,2002,23(5):405-410.
Authors:JING Xiao dong  SUN Xiao feng
Institution:Department of Jet Propulsion,Beijing University of Aeronautics and Astronautics, Beijing 100083,China
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.
Keywords:sound  vortex interaction  perforated liner  shear layer  linear perturbation theory
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号