期刊文献+

同向双涡合并过程声波研究 被引量:1

Acoustic wave in two corotating vortices pairing
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摘要 为了对常见不稳定流中声波产生过程的基本物理现象进行研究,基于大涡模拟方法与高阶精度加权本质无振荡混合格式,对剪切流中同向双涡合并过程的动力学流场及其声场进行了数值模拟。结果描述了同向旋转双涡合并过程,揭示了双涡合并产生旋转四极子声源的机理,且与相关研究相符。对剪切层的气动声场进行了数值模拟,揭示了剪切层中双涡旋转合并过程,发现涡合并过程产生的声波在整个剪切层声场中占主导作用,且合并在半个周期内完成。 To investigate the basic physics of acoustic wave generation in common unsteady flows,the dynamics flow and acoustic field produced by the coalescing of two corotating vortices in the shear flow are simulated based on the high order hybrid weight essentially non-oscillatory( WENO) scheme and large-eddy simulation( LES). The results reveal the pairing process of two corotating vortices,and show the generating mechanism of the rotating quadrupole source during vortex pairing. The numerical results agree well with the previous investigations. The acoustic field of a mixing layer is simulated,and the vortex pairing process of the mixing layer is shown. The results show that the acoustic wave generated by the vortex pairing dominates the whole acoustic field of the shear layer,and the pairing process completes during one half cycle.
出处 《南京理工大学学报》 EI CAS CSCD 北大核心 2013年第6期886-890,共5页 Journal of Nanjing University of Science and Technology
基金 江苏省高校“青蓝工程”中青年学术带头人培养对象项目 南京理工大学自主科研专项计划(2011ZDJH30 2011YBXM182)
关键词 气动声学 涡合并 声波 大涡模拟 加权本质无振荡混合格式 aeroacoustics vortex pairing acoustic wave large eddy simulation hybrid weight essentially non-oscillatory scheme
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参考文献17

  • 1Wagner C,Huttl T,Sagaut P. Large-eddy simulation for acoustics[M].Cambridge,UK:Cambridge University Press,2007.
  • 2Wang M,Freund J B,Lele S K. Computational prediction of flow-generated sound[J].{H}Annual Review of Fluid Mechanics,2006.483-512.
  • 3Mitchell B E,Lele S K,Moin P. Direct computation of the sound from a compressible co-rotating vortex pair[R].AIAA-92-0374,1922.
  • 4Bailly C,Bogey C,Juve D. Computation of flow noise using source terms in linearized Euler's equations[R].AIAA-2001-2047,2001.
  • 5Colonius T,Lele S K,Moin P. Sound generation in a mixing layer[J].{H}Journal of Fluid Mechanics,1997.375-409.
  • 6Babucke A,Kloker M,Rist U. DNS of a plane mixing layer for the investigation of sound generation mechanisms[J].Computer and Fluids,2008.360-368.
  • 7Voelkl T,Pullin D I,Chan D C. A physical-space version of the stretched-vortex subgrid-stress model for large-eddy simulation[J].{H}Physics of Fluids,2000,(07):1810-1825.
  • 8Lundgren T S. Strained spiral vortex model for turbulent fine structure[J].{H}Physics of Fluids,1982.2193.
  • 9Hill D J,Pullin D I. Hybrid tuned center-difference-WENO method for large eddy simulations in the presence of strong shocks[J].{H}Journal of Computational Physics,2004.435-450.
  • 10Tam C K,Webb J C. Dispersion-relation-preserving finite difference schemes for computational acoustics[J].{H}Journal of Computational Physics,1993.262-281.

二级参考文献6

  • 1傅德薰,马延文.平面混合流拟序结构的直接数值模拟[J].中国科学(A辑),1996,26(7):657-664. 被引量:30
  • 2Vreman B, Geurts B, Kuerten H. A priori tests of large eddy simulation of the compressible plane mixing layer [J ]. Journal of Engineering Mathematics, 1995, 29 (4) : 299 - 327.
  • 3Shao L, Sarkar S, Pantano C. On the relationship between the mean flow and subgrid stresses in large eddy simulation of turbulent shear flows [ J ]. Physics of Fluids, 1999, 11 (5): 1 229-1 248.
  • 4Roshko A. Structure of turbulent shear flows: A new look [J]. AIAA Journal, 1976, 14 (10): 1 349- 1 357.
  • 5Samimy M, Elliott G S. Effects of compressibility on the characteristics of free shear layers [ J ]. AIAA Journal, 1990, 28 (3) : 439 -445.
  • 6刘奕,郭印诚,张会强,王希麟,林文漪.混合层流动拟序结构的大涡模拟[J].应用力学学报,2002,19(2):22-26. 被引量:3

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同被引文献20

  • 1Bridges J E. Application of coherent structure and vortex sound theories to jet noise [ D ]. Houston, US : University of Houston, 1990.
  • 2Jiang X, Avital E J, Luo K h. Direct computation and aeroacoustic modelling of a subsonic axisymmetric jet [ J ]. Journal of Sound and Vibration, 2004,270 ( 3 ) : 525 -538.
  • 3Bogey C, Bailly C, Juve D. Computation of the sound radiated by a 3-D jet using large eddy simulation[ R]. AIAA 2000-2009.
  • 4Constantineseu G S, Lele S K. Large eddy simulation of a near sonic turbulent jet and its radiated noise [ R ]. AIAA 2001-0376.
  • 5Voelkl T, Pullin D I, Chan D C. A physical-space version of the stretched-vortex subgrid-stress model for large-eddy simulation [ J ]. Physics of Fluids, 2000, 12(7) :1810-1825.
  • 6Lundgren T S. Strained spiral vortex model for turbulent fine structure [J]. Physics of Fluids, 1982, 25 : 2193-2203.
  • 7Hill D J, Pullin D I. Hybrid tuned center-difference- WENO method for large eddy simulations in the presence of strong shocks[ J]. Journal of Computational Physics ,2004,194 (2) :435-450.
  • 8Tam C K, Webb J C. Dispersion-relation-preserving finite differentce schemes for computational acoustics [ J ]. Journal of Computational Physics, 1993,107 : 262 -281.
  • 9Zhuang M, Chen R F. Optimized upwind dispersion- relation-preserving finite difference scheme for computational aeroacoustics [ J ]. AIAA Journal, 1998, 36( 11 ) :2146-2148.
  • 10Israeli M, Orszag S A. Approximation of radiationboundary conditions [ J ]. Journal of Computational Physics, 1981,41 ( 1 ) : 115-135.

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