Jet-installation noise reduction with flow-permeable materials

被引:11
|
作者
Rego, Leandro [1 ]
Ragni, Daniele [1 ]
Avallone, Francesco [1 ]
Casalino, Damiano [1 ]
Zamponi, Riccardo [2 ]
Schram, Christophe [2 ]
机构
[1] Delft Univ Technol, Dept Aerodynam Wind Energy & Prop, Kluyverweg 1, NL-2629 HS Delft, Netherlands
[2] von Karman Inst Fluid Dynam, Environm & Appl Fluid Dynam Dept, Waterloosesteenweg 72, B-1640 Rhode St Genese, Belgium
关键词
Aeroacoustics; Jet-installation noise; Porous materials;
D O I
10.1016/j.jsv.2021.115959
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
This paper investigates the application of flow-permeable materials as a solution for reducing jet-installation noise. Experiments are carried out with a flat plate placed in the near field of a single-stream subsonic jet. The flat plate is modular and the solid surface near the trailing edge can be replaced with different flow-permeable inserts, such as a metal foam and a perforated plate structure. The time-averaged jet flow field is characterized through planar PIV measurements at three different velocities (M-a = 0.3, M-a = 0.5 and M-a = 0.8, where M-a is the acoustic Mach number), whereas the acoustic far-field is measured with a microphone arc-array. Acoustic measurements confirm that installation effects cause significant noise increase, up to 17 dB for the lowest jet velocity, particularly at low and mid frequencies (i.e. St < 0.7, with the Strouhal number based on the jet diameter and velocity), and mostly in the upstream direction of the jet. By replacing the solid trailing edge with the metal foam, noise abatement of up to 9 dB is achieved at the spectral peak for M-a = 0.3 and a polar angle theta = 40 degrees, with an overall reduction in the entire frequency range where jet-installation noise is dominant. The perforated plate provides lower noise reduction than the metal foam (7 dB at the spectral peak for M-a = 0.3 and theta= 40 degrees), and it is less effective at low frequencies. This is related to the values of permeability and form coefficient of the materials, which are the major parameters controlling the pressure balance across the trailing edge and, consequently, the noise generated by the plate. However, despite having a high permeability, the plate with the metal-foam trailing edge still has a distinct noise production at mid frequencies (St approximate to 0.43 for M-a = 0.3). Based on the analyses of different treated surface lengths, it is conjectured that the solid-permeable junction in the plate acts as a new scattering region, and thus its position also affects the far-field noise, which is in line with analytical predictions in the literature. Nonetheless, both types of inserts provide significant noise reduction and are potential solutions for the problem of jet-installation noise. (C) 2021 The Authors. Published by Elsevier Ltd.
引用
收藏
页数:17
相关论文
共 50 条
  • [41] Supersonic jet noise reduction by microjet injection
    Zaman, K. B. M. Q.
    INTERNATIONAL JOURNAL OF AEROACOUSTICS, 2012, 11 (7-8) : 917 - 936
  • [42] A test facility for aircraft jet noise reduction
    McGehee, B.L.
    1600, (19):
  • [43] A New Rational Approach to Jet Noise Reduction
    John M. Seiner
    Theoretical and Computational Fluid Dynamics, 1998, 10 : 373 - 383
  • [44] PRACTICAL JET NOISE REDUCTION FOR TACTICAL AIRCRAFT
    Martens, Steve
    Spyropoulos, John T.
    PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 1, 2010, : 389 - 399
  • [45] SUPERSONIC JET SHOCK NOISE REDUCTION.
    Stone, James R.
    NASA Technical Memorandum, 1984,
  • [46] JET ENGINE NOISE REDUCTION RESEARCH AT NACA
    SANDERS, ND
    CALLAGHAN, EE
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1956, 28 (04): : 803 - 803
  • [47] Experiments on Jet Noise Reduction with a Liquid Column
    Zhang, Lei
    Wang, Hao
    Ruan, Wen-jun
    ACOUSTICS AUSTRALIA, 2016, 44 (02): : 291 - 297
  • [48] REDUCTION OF NOISE FROM SUPERSONIC JET FLOWS
    DOSANJH, DS
    YU, JC
    ABDELHAMID, AN
    AIAA JOURNAL, 1971, 9 (12) : 2346 - +
  • [49] Reduction of Jet Impingement Noise by Addition of Swirl
    Balakrishnan, P.
    Srinivasan, K.
    JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 2016, 138 (06):
  • [50] FLOW NOISE - PERSPECTIVE ON SOME ASPECTS OF FLOW NOISE, AND OF JET NOISE IN PARTICULAR .2.
    POWELL, A
    NOISE CONTROL ENGINEERING JOURNAL, 1977, 8 (03) : 108 - 119