Discrimination of acoustic and turbulent components from aeroacoustic wall pressure field

被引:13
|
作者
Druault, Philippe [1 ,2 ]
Hekmati, Abbas [3 ]
Ricot, Denis [3 ]
机构
[1] Univ Paris 06, Inst Jean Le Rond dAlembert, UMR 7190, F-75252 Paris 5, France
[2] CNRS, Inst Jean Le Rond dAlembert, UMR 7190, F-75252 Paris 5, France
[3] RENAULT, Res Dept, F-78288 Guyancourt, France
关键词
LATTICE BOLTZMANN METHOD; COHERENT STRUCTURES; FLOW; CYLINDER;
D O I
10.1016/j.jsv.2013.07.019
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
The investigation of the wall pressure excitations over transportation vehicle panel is of great interest to improve the knowledge of vehicle interior noise transmission and also for future noise reduction strategies. A particularly useful task concerns the characterization and the separation of both acoustic and turbulent components of the wall pressure excitation. A new application of the Proper Orthogonal Decomposition (POD) is tested from two different databases: (i) wall pressure fields synthesized from theoretical average models and (ii) wall pressure fields obtained from Lattice Boltzmann Method numerical simulation. In each case, POD application leads to an energetic partitioning of the wall pressure field that permits to well decouple both acoustic and turbulent fields, especially for mid and high frequencies under interest. To validate such separation and to demonstrate the effectiveness of the POD method, the wavenumber spectrum analysis as well as phase analysis is successively performed. Such a new splitting method provides an instantaneous acoustic-turbulent separation of an inhomogeneous wall pressure field, suggesting many useful future applications. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:7257 / 7278
页数:22
相关论文
共 50 条
  • [41] Analysis of Noise Generation by Turbulent Jets from Consideration of Their Near Acoustic Field
    Krasheninnikov, S. Yu.
    Mironov, A. K.
    Benderskii, L. A.
    ACOUSTICAL PHYSICS, 2018, 64 (06) : 718 - 730
  • [42] Analysis of Noise Generation by Turbulent Jets from Consideration of Their Near Acoustic Field
    S. Yu. Krasheninnikov
    A. K. Mironov
    L. A. Benderskii
    Acoustical Physics, 2018, 64 : 718 - 730
  • [43] On the correlation of acoustic pressures induced by a turbulent wake on a nearby wall
    Max-Planck-Inst fuer Aeronomie, Katlenburg-Lindau, Germany
    Acta Acustica Stuttgart, 1 (9-17):
  • [44] On the correlation of acoustic pressures induced by a turbulent wake on a nearby wall
    Campos, LMBC
    ACUSTICA, 1996, 82 (01): : 9 - 17
  • [45] Discrimination of field components in optical probe microscopy
    Kohlgraf-Owens, D. C.
    Sukhov, S.
    Dogariu, A.
    OPTICS LETTERS, 2012, 37 (17) : 3606 - 3608
  • [46] Influence of pressure gradients on wall pressure beneath a turbulent boundary layer
    Cohen, Elie
    Gloerfelt, Xavier
    JOURNAL OF FLUID MECHANICS, 2018, 838 : 715 - 758
  • [47] ACOUSTIC ANEMOMETER BASED ON TURBULENT PRESSURE-FLUCTUATIONS
    DAWBER, KR
    SINCLAIR, M
    JOURNAL OF PHYSICS E-SCIENTIFIC INSTRUMENTS, 1977, 10 (11): : 1112 - 1114
  • [48] A hydro-acoustic mode decomposition method for velocity and pressure field and application to a subsonic turbulent jet
    Han, Shuaibin
    Li, Hu
    Luo, Yong
    Wang, Yimin
    Ma, Ruixuan
    Zhang, Shuhai
    PHYSICS OF FLUIDS, 2023, 35 (07)
  • [49] Wall effects on pressure fluctuations in turbulent channel flow
    Gerolymos, G. A.
    Senechal, D.
    Vallet, I.
    JOURNAL OF FLUID MECHANICS, 2013, 720 : 15 - 65
  • [50] Simulation of the pressure field beneath a turbulent boundary layer using realizations of uncorrelated wall plane waves
    Maxit, Laurent
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2016, 140 (02): : 1268 - 1285