High speed PIV applied to aerodynamic noise investigation

被引:56
作者
Koschatzky, V. [1 ]
Moore, P. D. [2 ]
Westerweel, J. [1 ]
Scarano, F. [2 ]
Boersma, B. J. [1 ]
机构
[1] Delft Univ Technol, Lab Aero & Hydrodynam, Fac Mech Maritime & Mat Engn, Delft, Netherlands
[2] Delft Univ Technol, High Speed Lab, Fac Aerosp Engn, Delft, Netherlands
关键词
FLOW; CAVITY; OSCILLATIONS; PRESSURE;
D O I
10.1007/s00348-010-0935-8
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, we study the acoustic emissions of the flow over a rectangular cavity. Especially, we investigate the possibility of estimating the acoustic emission by analysis of PIV data. Such a possibility is appealing, since it would allow to directly relate the flow behavior to the aerodynamic noise production. This will help considerably in understanding the noise production mechanisms and to investigate the possible ways of reducing it. In this study, we consider an open cavity with an aspect ratio between its length and depth of 2 at a Reynolds number of 2.4 x 10(4) and 3.0 x 10(4) based on the cavity length. The study is carried out combining high speed two-dimensional PIV, wall pressure measurements and sound measurements. The pressure field is computed from the PIV data. Curle's analogy is applied to obtain the acoustic pressure field. The pressure measurements on the wall of the cavity and the sound measurements are then used to validate the results obtained from PIV and check the range of validity of this approach. This study demonstrated that the technique is able to quantify the acoustic emissions from the cavity and is promising especially for capturing the tonal components on the sound emission.
引用
收藏
页码:863 / 876
页数:14
相关论文
共 26 条
[1]  
Ahuja K., 1995, CR4654 NASA
[2]  
Block P. J. W., 1976, Report No. NASA TN D8351
[3]  
COLONIUS T, 1999, AIAA CEAS AER C EXH
[4]   THE INFLUENCE OF SOLID BOUNDARIES UPON AERODYNAMIC SOUND [J].
CURLE, N .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1955, 231 (1187) :505-514
[5]  
de Kat R., 2008, 14 INT S APPL LAS TE
[6]   THE EFFECT OF FLOW OSCILLATIONS ON CAVITY DRAG [J].
GHARIB, M ;
ROSHKO, A .
JOURNAL OF FLUID MECHANICS, 1987, 177 :501-530
[7]   Experimental investigation of the flow characteristics within a shallow wall cavity for both laminar and turbulent upstream boundary layers [J].
Grace, SM ;
Dewar, WG ;
Wroblewski, DE .
EXPERIMENTS IN FLUIDS, 2004, 36 (05) :791-804
[8]   A time-resolved particle image velocimetry investigation of a cavity flow with a thick incoming turbulent boundary layer [J].
Haigermoser, C. ;
Vesely, L. ;
Novara, M. ;
Onorato, M. .
PHYSICS OF FLUIDS, 2008, 20 (10)
[9]   Application of an acoustic analogy to PIV data from rectangular cavity flows [J].
Haigermoser, Christian .
EXPERIMENTS IN FLUIDS, 2009, 47 (01) :145-157
[10]  
Howe M.S., 2003, THEORY VORTEX SOUND