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空调换热器的噪声特性评价 被引量:8

Noise Performance Investigation of Heat Exchanger of Air Condition
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摘要 采用声学测量装置在半消声实验室风洞中评价了不同入口气流速度和角度条件下换热器的声学特性.结果表明,空调换热器产生的噪声是低流速状态下多腔体耦合共振的结果,而且具有宽频特性.换热器中气流速度的方向和大小对其噪声的影响很大:换热器的气动噪声随着气体流速增加而增大,而小于7m/s的气流不会产生噪声;过大或过小的入口气流角度都不会产生气动噪声.噪声频率随着气体流速增加而呈现出线性增长,给定的换热器存在一个恒定的斯特雷哈尔数. The behaviors of noise through the heat exchanger of indoor unit at a low-speed free stream were studied by aero-acoustic performance measurements in a semi-anechoic chamber with different velocities and angles. The experimental results indicate that the noise can be generated at particular velocity and an- gles which are considered as the most important factor that influences the aerodynamic performance of the heat exchanger. With the increasing in the flow velocity, the frequency of noise increases linearly, and there exists a fixed Strouhal number for the given heat exchanger.
出处 《上海交通大学学报》 EI CAS CSCD 北大核心 2015年第5期633-636,643,共5页 Journal of Shanghai Jiaotong University
基金 国家自然科学基金项目(51076101)资助
关键词 换热器 气动声学 空腔 噪声 heat exchanger aeroacoustic performance cavity noise
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参考文献11

  • 1Yamada S, Sekiguchi K, Ikeda T. Aerodynamic noise generated from heat exchangers with a large inlet angle[J]. Inter Noise Meeting, 1999, 1: 173-176.
  • 2Sarohia V. Experimental investigation of the oscilla- tions in flows over shallow cavities[J]. AIAA Jour- nal, 1977, 15(7): 984-991.
  • 3Stallings R L, Wilcox F J. Experimental cavity pres- sure distributions at supersonic speeds[R]. USA: NASA Tech Pap, 1987:165-162.
  • 4Rajarshi Das,Job Kurian.Acoustic and velocity field over 3D cavities[J].Theoretical & Applied Mechanics Letters,2013,3(1):11-15. 被引量:1
  • 5Zhu Y, Ouyang H, Du Z. Experimental investigation of acoustic oscillations over cavities[J]. Journal of Aerospace Engineering, 2010, 224(6): 1-8.
  • 6Vikramadityal N S, Kurian J. Pressure oscillations- from cavity with a ramp Aeroacoustics Conference. 2009: 3208. [C]// 15th A1AA/CEAS USA, Florida: AIAA,2009: 3208.
  • 7杨党国,范召林,李建强,罗新福,蒋卫民.后壁倒角对空腔噪声的抑制效果[J].实验流体力学,2010,24(5):22-25. 被引量:12
  • 8Rowley C W, Juttijudata V, Williams D R. Cavity flow control simulations and experiments[C]// 43rd AIAA Aerospace Sciences Meeting. USA.. AIAA, 2005:292-296.
  • 9张强,李启,李青.喷口自由剪切层自激振荡优势频率的预测[J].南京航空航天大学学报,2004,36(2):257-261. 被引量:3
  • 10Zhang N, Shen H, Yao H Z. Numerical simulation of cavity flow induce noise by LES and FW-H acous- tic analogy[J]. Journal of Hydrodynamics, 2010, 22 (5) :242-247.

二级参考文献31

  • 1侯中喜,夏刚,秦子增.三维超声速开式空腔振荡特性研究[J].国防科技大学学报,2004,26(6):1-4. 被引量:9
  • 2李晓东,刘靖东,高军辉.空腔流激振荡发声的数值模拟研究[J].力学学报,2006,38(5):599-604. 被引量:41
  • 3杨党国,李建强,罗新福,胡成行.弹穴流动特性高速风洞试验研究[J].实验流体力学,2006,20(4):33-39. 被引量:15
  • 4COFONIUS T. An overview of simulation, modeling, and active control of flow/acoustic resonance in open cavities[R]. ALAA 2001-0076.
  • 5ABRABAM J. An experimental study of open cavity flows at low subsonic speeds[R]. AIAA 2002-0280.
  • 6CHING-WEI M S, PHILIP J M. Comparison of two- and three-dimensional turbulent cavity flows[R]. AIAA 2001-0511.
  • 7HAMED A, BASU D, DAS K. Detached eddy simulations of supersonic flow over cavity[R]. AIAA 2003- 0549.
  • 8LAI H, LUO K H. A three dimensional hybrid LES-acoustic analogy method for predicting open cavity noise [J]. Flow, turbulence and Combustion, 2007,79 ( 1 ) : 55-82.
  • 9HAMED A,DAS K,BASU D. Numerical simulations of fluidic control for transonic cavity flows [R]. AIAA 2004- 429.
  • 10CLARENCE W R, VEJAPONG J. Cavity flow control simulations and experiments[R]. AIAA 2005-0292.

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