SHOCK ASSOCIATED NOISE OF INVERTED-PROFILE COANNULAR JETS .3. SHOCK STRUCTURE AND NOISE CHARACTERISTICS

被引:7
|
作者
TAM, CKW [1 ]
TANNA, HK [1 ]
机构
[1] LOCKHEED GEORGIA CO,MARIETTA,GA 30063
关键词
D O I
10.1016/0022-460X(85)90407-9
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
引用
收藏
页码:127 / 145
页数:19
相关论文
共 50 条
  • [31] Equivalent shock-associated noise source reconstruction of screeching underexpanded unheated round jets
    Tan, D.J.
    Honnery, D.
    Kalyan, A.
    Gryazev, V.
    Karabasov, S.A.
    Edgington-Mitchell, D.
    AIAA Journal, 2019, 57 (03): : 1200 - 1214
  • [32] EFFECT OF DENSITY ON NOISE RADIATION FROM SUBSONIC INVERTED VELOCITY PROFILE JETS
    SAROHIA, V
    MASSIER, PF
    AIAA JOURNAL, 1980, 18 (06) : 630 - 635
  • [33] Broadband shock-cell noise from dual stream jets
    Tam, Christopher K. W.
    Pastouchenko, N. N.
    Viswanathan, K.
    JOURNAL OF SOUND AND VIBRATION, 2009, 324 (3-5) : 861 - 891
  • [34] Scaling law for shock-cell length and its correlation with shock-associated noise of circular and elliptic supersonic free jets
    Perumal, Arun Kumar
    Rathakrishnan, Ethirajan
    PHYSICS OF FLUIDS, 2021, 33 (09)
  • [35] EXPERIMENTAL-STUDY OF JET NOISE .2. SHOCK ASSOCIATED NOISE
    TANNA, HK
    JOURNAL OF SOUND AND VIBRATION, 1977, 50 (03) : 429 - 444
  • [36] STOCHASTIC-MODEL THEORY OF BROAD-BAND SHOCK ASSOCIATED NOISE FROM SUPERSONIC JETS
    TAM, CKW
    JOURNAL OF SOUND AND VIBRATION, 1987, 116 (02) : 265 - 302
  • [37] Prediction of Scattered Broadband Shock-Associated Noise
    Miller, Steven A. E.
    AIAA JOURNAL, 2016, 54 (01) : 343 - 359
  • [38] Design of a Facility for Studying Shock-Cell Noise on Single and Coaxial Jets
    Guariglia, Daniel
    Carpio, Alejandro Rubio
    Schram, Christophe
    AEROSPACE, 2018, 5 (01)
  • [39] Azimuthal decomposition of the radiated noise from supersonic shock-containing jets
    Wong, Marcus H.
    Kirby, Rhiannon
    Jordan, Peter
    Edgington-Mitchell, Daniel
    JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2020, 148 (04): : 2015 - 2027
  • [40] A Theoretical Basis for the Scaling Law of Broadband Shock Noise Intensity in Supersonic Jets
    Kandula, Max
    ADVANCES IN ACOUSTICS AND VIBRATION, 2011, 2011