期刊文献+

流管声传播与膜结构相互作用的机理研究 被引量:4

ON THE MECHANISM OF THE INTERACTION BETWEEN FLEXIBLE PANELS AND SOUND WAVES IN FLOW DUCTS
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摘要 以等价分布源方法为基础研究流管声传播与膜结构相互作用的机理.根据广义格林函数给出任意截面管道的通用模型.并在此基础上研究了结构参数、流动马赫数、高阶模态波对膜结构消声器降噪量及临界频率的影响.此外,还讨论了流体介质对声波与膜片相互作用的影响,可以看出膜结构消声器在水下也能得到广泛的应用. The control of sound propagation in ducts has always been a problem of concern. One of new attempts is to make use of the interaction between a soulid wave and a flexible panel to reduce the sound propagation. This paper presents a general model to describe the interaction between flexible panels and sound waves with the emphasis on the effect of flow Mach number, higher order modes and annular or circular geometrical parameters on the control of sound propagation, which is not much studied in the current literature. Based on a comparison with the existing results, some important parametric study is made in the present paper. Further research work is suggested after a detailed discussion and analysis on the numerical results.
出处 《力学学报》 EI CSCD 北大核心 2006年第6期825-830,共6页 Chinese Journal of Theoretical and Applied Mechanics
基金 国家自然科学基金资助项目(50136010 10472009).~~
关键词 流管声传播 膜结构消声器 等价分布源 临界频率 duct acoustics, flexible panel for noise control, equivalent sound source, critical frequency
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参考文献4

  • 1Huang Lixi.A theoretical study of duct noise control by flexible panels.J Acoust Soc Am,1999,106(4):1801~1809
  • 2Huang Lixi.A theoretical study of passive control of duct noise using panels of varying compliance.J Acoust Soc Am,2001,109(6):2805~2814
  • 3Namba M,Fukushige K.Application of the equivalent surface source method to the acoustics of duct systems with non-uniform wall impedance.Journal of Sound and Vibration,1980,73(1):125~146
  • 4孙晓峰 周盛.气动声学[M].北京:国防工业出版社,1994..

共引文献10

同被引文献44

  • 1严红,王松.等压比热在基于壁面放电的激波控制中的影响[J].力学学报,2015,47(1):51-60. 被引量:1
  • 2孙晓峰,王晓宇.一种新的膜结构消声器理论模型[J].北京航空航天大学学报,2006,32(10):1152-1156. 被引量:3
  • 3沈清,王强,庄逢甘.超声速平面剪切层声辐射涡模态数值分析[J].力学学报,2007,39(1):7-14. 被引量:8
  • 4Tam CKW. Jet noise: since 1952. Theoretical and Computational Fluid Dynamics, 1998, 10(1-4): 393-405.
  • 5Tam C, Viswanathan K, Ahuja K, et al. The sources of jet noise: experimental evidence. Journal of Fluid Mechanics, 2008, 615(4): 253-292.
  • 6Hileman J I, Samimy M. Mach number effects on jet noise sources and radiation to shallow angles. AIAA Journal, 2006, 44 (8): 1915- 1918.
  • 7Mitchell BE, Lele SK, Moin P. Direct computation of the sound gen- erated by vortex pairing in an axisymmetric jet. Journal of Fluid Mechanics, 1999, 383(6): 113-142.
  • 8Freund JB, Lele SK, Moin P. Numerical simulation of a mach 1.92 turbulent jet and its sound field. AIAA Journal, 2000, 38(11): 2023- 2031.
  • 9Mohseni K, Colonius T, Freund JB. An evaluation of linear instabil- ity waves as sources of sound in a supersonic turbulent jet. Physics of Fluids, 2002, 14(10): 3593-3600.
  • 10Berland J, Bogey C, Bailly C. Numerical study of screech generation in a planar supersonic jet. Physics of Fluids, 2007, 19(7): 1-14.

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