Aeroacoustical study of the TGV pantograph recess

被引:82
作者
Noger, C [1 ]
Patrat, JC [1 ]
Peube, J [1 ]
Peube, JL [1 ]
机构
[1] UMR CNRS 6609, CEAT, Lab Etud Aerodynam, F-86036 Poitiers, France
关键词
D O I
10.1006/jsvi.1999.2545
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
The general focus of this aerodynamic noise research, induced by turbulent incompressible flow, is to improve our knowledge of acoustic production mechanisms in the TGV pantograph recess in order to be able to reduce the radiated noise. This work is performed under contract with SNCF as a part of the German-French Cooperation DEUFRAKO K2, and is supported by French Ministries for Transport and Research. Previous studies on TGV noise source locations (DEUFRAKO K) have identified the pantograph recess as one of the important aerodynamic noise sources, for speeds higher than 300 km/h, due to flow separation. The pantograph recess is a very complex rectangular cavity, located both on the power car and the first coach roofs of the TGV, and has not been studied before due to the complex shapes. Its aeroacoustic features are investigated experimentally in a low-subsonic wind tunnel, on a realistic 1/7th scale mock-up both with and without pantographs. Flow velocities, estimated with hot-wire anemometry, and parietal visualizations show the flow to reattach on the recess bottom wall and to separate again at the downstream face. Wall pressure fluctuations and "acoustic" measurements using 1/4 and 1/2 in microphones respectively are also measured to qualify the flow: no aerodynamic or acoustic oscillations are observed. The study indicates that the pantograph recess has a different behaviour compared to the usual cavity grazing flows. (C) 2000 Academic Press.
引用
收藏
页码:563 / 575
页数:13
相关论文
共 15 条
  • [1] NAVIER-STOKES COMPUTATIONS OF CAVITY AEROACOUSTICS WITH SUPPRESSION DEVICES
    BAYSAL, O
    YEN, GW
    FOULADI, K
    [J]. JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 1994, 116 (01): : 105 - 112
  • [2] ESTIMATION OF POSSIBLE EXCITATION FREQUENCIES FOR SHALLOW RECTANGULAR CAVITIES
    BILANIN, AJ
    COVERT, EE
    [J]. AIAA JOURNAL, 1973, 11 (03) : 347 - 351
  • [3] Bliss, 1976, AEROACOUSTICS STOL N, V45, P281
  • [4] AN INVESTIGATION OF SEPARATED FLOWS .2. FLOW IN THE CAVITY AND HEAT TRANSFER
    CHARWAT, AF
    DEWEY, CF
    ROOS, JN
    HITZ, JA
    [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (07): : 513 - 527
  • [5] FRANKE ME, 1975, 75492 AIAA
  • [6] SOUND GENERATION BY FLOW OVER A 2-DIMENSIONAL CAVITY
    HARDIN, JC
    POPE, DS
    [J]. AIAA JOURNAL, 1995, 33 (03) : 407 - 412
  • [7] KOMERATH NM, 1987, 870166 AIAA
  • [8] A NEW SURFACE-STREAMLINE FLOW-VISUALIZATION TECHNIQUE
    LANGSTON, LS
    BOYLE, MT
    [J]. JOURNAL OF FLUID MECHANICS, 1982, 125 (DEC) : 53 - &
  • [9] MENDOZA JM, 1995, P CEAS AIAA 95, P403
  • [10] NOGER C, 1998, 1P8U10T1DA