NEW EVIDENCE OF MECHANISMS OF NOISE GENERATION AND RADIATION OF A SUBSONIC JET

被引:3
|
作者
MAESTRELLO, L [1 ]
PAO, SP [1 ]
机构
[1] NASA,LANGLEY RES CTR,HAMPTON,VA 23665
来源
关键词
D O I
10.1121/1.380540
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
引用
收藏
页码:959 / 960
页数:2
相关论文
共 50 条
  • [31] PREDICTION METHOD FOR EFFECTS OF FLIGHT ON SUBSONIC JET NOISE
    COCKING, BJ
    JOURNAL OF SOUND AND VIBRATION, 1977, 53 (03) : 435 - 453
  • [32] GENERATION OF JET NOISE
    LAUFER, J
    KAPLAN, R
    CHU, W
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1974, 55 (02): : 399 - 399
  • [33] Shear-layer acoustic radiation in an excited subsonic jet:: models for vortex pairing and superdirective noise
    Fleury, V
    Bailly, C
    Juvé, D
    COMPTES RENDUS MECANIQUE, 2005, 333 (10): : 754 - 761
  • [34] Investigation of noise source mechanisms in subsonic jets
    Viswanathan, K.
    AIAA JOURNAL, 2008, 46 (08) : 2020 - 2032
  • [35] Downstream subsonic jet noise: link with vortical structures intruding into the jet core
    Bogey, C
    Bailly, C
    COMPTES RENDUS MECANIQUE, 2002, 330 (08): : 527 - 533
  • [36] Sound generation by interacting vortices in a subsonic turbulent jet
    Pimshtein V.G.
    Fluid Dynamics, 2000, 35 (1) : 43 - 47
  • [37] AZIMUTHAL DECOMPOSITION OF POWER SPECTRAL DENSITY OF SUBSONIC JET NOISE
    YAMAMOTO, K
    ARNDT, REA
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1977, 61 : S24 - S25
  • [38] NON-LINEAR PSE ANALYSIS OF SUBSONIC JET NOISE
    Salgado, Adriana M.
    Agarwal, Anurag
    Suponitsky, Victoria
    Sandham, Neil D.
    PROCEEDINGS OF THE 17TH INTERNATIONAL CONGRESS ON SOUND AND VIBRATION, 2010,
  • [39] Instability waves and aerodynamic noise in a subsonic transitional turbulent jet
    Wan, Zhen-Hua
    Yang, Hai-Hua
    Zhang, Xing-Chen
    Sun, De-Jun
    EUROPEAN JOURNAL OF MECHANICS B-FLUIDS, 2016, 57 : 192 - 203
  • [40] Use of downstream fluid injection to reduce subsonic jet noise
    Rajput, Pankaj
    Kumar, Sunil
    INTERNATIONAL JOURNAL OF AEROACOUSTICS, 2019, 18 (4-5) : 554 - 574