期刊文献+

小口径喷嘴冲击射流噪声锯齿特性及机理研究 被引量:5

ON THE SAW-TOOTH CHARACTERISTIC AND ITS MECHANISM OF THE IMPINGING JET NOISE FROM SMALL DIAMETER NOZZLE ONTO LARGE FLAT PLATE
下载PDF
导出
摘要 测量了 3毫米口径轴对称收缩喷嘴射流冲击大平板产生的噪声随冲击距离变化的特性。发现远场噪声随冲击距离的变化呈锯齿状 ,射流上游的噪声频谱上有粗缓、跨较宽频带的尖峰。根据不同唇厚喷嘴的实验对比 ,判断这些现象跟反馈有关 ,称为反馈噪声 ,而且正是反馈噪声与湍流噪声的相互作用 。 The characteristics of the far-field noise of impinging jet with 3-millimeter diameter axisymmetric convergent nozzle under the condition of variable nozzle-to-plate distance,and their methanism were investigated experimentally.It is found that the far-field noise intensity of the 3 mm nozzle impinging jet has a saw-tooth behavior with the variation of nozzle-to-plate distance,and there are some chunky broadband peaks on the narrow-band noise spectrum,and these peaks exist only on the upstream of the jet.According to the consideration of key factors responsible for the feedback loop and results of the experiments performed to detect the effect of nozzle exit lip thickness on these new phenomena,the feedback mechanism is suggested to be responsible for these phenomena,and the associated noise is defined as weak feedback noise.The interaction of the turbulent noise and weak feedback noise induces the saw-tooth behavior of the total noise intensity with the variation of nozzle-to-plate distance.
出处 《振动与冲击》 EI CSCD 北大核心 2003年第4期36-39,48,共5页 Journal of Vibration and Shock
基金 国家自然科学基金项目 (1 990 2 0 0 9)
关键词 锯齿特性 噪声频谱 冲击射流 气动技术 自激振动 impinging jet,noise,saw-tooth,feedback,small diamster nozzle
  • 相关文献

参考文献20

  • 1[1]Rockwell D.Self-sustained oscillations of impinging free shear layers.Ann.Rev.Fluid Mech.1979,11:67-94 被引量:1
  • 2[2]Ho C M,Nosseir N S.Dynamics of an impinging jet.Part 1.The feedback phenomenon.J.Fluid Mech.1981,105:119-142 被引量:1
  • 3[3]Nosseir N S,Ho C M.Dynamics of an impinging jet.Part 2.The noise generation.J.Fluid Mech.1982,116:379-391 被引量:1
  • 4[4]Nosseir N S.On the feedback phenomenon and noise generation of an impinging jet.1979 Ph.D.thesis,Univ.of Southern Cali.,U.S.A 被引量:1
  • 5[5]Tam C K W,Ahuja,K K.Theoretical model of discrete tone generation by impinging jets.J.Fluid Mech.1990,214:67-87 被引量:1
  • 6[6]Krothapalli A.Discrete tones generated by an impinging underexpanded rectangular jet.AIAA J.1985,23(12):1910-1915 被引量:1
  • 7[7]Powell A.The sound-Producing oscillations of round underexpand-ed jets impinging on normal plates.J.Acoust.Soc.Am.1988,83(2):515-533 被引量:1
  • 8[8]Norum,T D.Supersonic Rectangular Jet Impingement Noise Experiments AIAA J.1991,29(7):1051-1057 被引量:1
  • 9[9]Tam C K W,Norum T D.Impingement tones of large aspect ratio supersonic rectangular jets.AIAA J.1992,30(2):304-311 被引量:1
  • 10[10]Sheplak M,Spina E F.Control of high-speed impinging-jet resonance.AIAA J.1994,32(8):1583-1588 被引量:1

同被引文献30

引证文献5

二级引证文献21

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部