INSTABILITY MODES EXCITED BY NATURAL SCREECH TONES IN A SUPERSONIC RECTANGULAR JET

被引:60
|
作者
RAMAN, G [1 ]
RICE, EJ [1 ]
机构
[1] NASA,LEWIS RES CTR,CLEVELAND,OH 44135
关键词
D O I
10.1063/1.868389
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The evolution of hydrodynamic instability modes self-excited by harmonically related natural screech tones was experimentally investigated. A convergent rectangular nozzle with an aspect ratio of 9.63 was used to produce a supersonic shock-containing jet. Measurements in the flow field were made using standard hot-film probes positioned only in the subsonic (outer) portions of the flow. The hydrodynamic instability mode observed in the shear layer at the screech frequency was observed to be antisymmetric (sinuous) about the smaller dimension of the jet, whereas its harmonic was observed to be symmetric (varicose). In addition, the nearfield noise measurements indicated that the radiated screech tone noise was out of phase on either side of the small jet dimension, whereas its harmonic was in phase over the same region. To the authors' knowledge, such an observation on the nature of the harmonic has thus far gone unreported and therefore is the focus of the present work. The hydrodynamic instability modes occurring at the screech frequency and its harmonic satisfied the conditions for resonance. Detailed measurements of the coherent wave evolution in the streamwise and spanwise directions indicated that strong spanwise variations were present downstream. © 1994 American Institute of Physics.
引用
收藏
页码:3999 / 4008
页数:10
相关论文
共 50 条
  • [1] Control methods for supersonic jet screech tones
    Wang, Yang-Hai
    Li, Xiao-Dong
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2007, 28 (02): : 211 - 215
  • [2] THE ROLE OF SCREECH TONES IN MIXING OF AN UNDEREXPANDED RECTANGULAR JET
    KROTHAPALLI, A
    HSIA, Y
    BAGANOFF, D
    KARAMCHETI, K
    [J]. JOURNAL OF SOUND AND VIBRATION, 1986, 106 (01) : 119 - 143
  • [3] Screech tones of supersonic jets from bevelled rectangular nozzles
    Tam, CKW
    Shen, H
    Raman, G
    [J]. AIAA JOURNAL, 1997, 35 (07) : 1119 - 1125
  • [4] Symmetrical oscillation modes in choked-jet edge tones and screech from rectangular nozzles
    Lin, D
    Powell, A
    [J]. JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1997, 102 (02): : 1235 - 1238
  • [5] Pressure field around a rectangular supersonic jet in screech
    Kaji, S
    Nishijima, N
    [J]. AIAA JOURNAL, 1996, 34 (10) : 1990 - 1996
  • [6] Numerical simulation of the generation mechanism of axisymmetric supersonic jet screech tones
    Li, XD
    Gao, JH
    [J]. PHYSICS OF FLUIDS, 2005, 17 (08) : 1 - 8
  • [7] Spiral instability and screech effect in supersonic jet flows
    Menshov, Igor
    Nenashev, Andrey
    [J]. 13TH EUROPEAN TURBULENCE CONFERENCE (ETC13): INSTABILITY, TRANSITION, GRID TURBULENCE AND JETS, 2011, 318
  • [8] Experimental investigation of screech tone mechanism in supersonic rectangular jet
    Zhang, Junlong
    Qin, Chen
    Zhao, Jiaxi
    [J]. Shengxue Xuebao/Acta Acustica, 2024, 49 (05): : 1083 - 1090
  • [9] Harmonics of Jet Screech Tones
    Tam, Christopher K. W.
    Parrish, Sarah A.
    Viswanathan, K.
    [J]. AIAA JOURNAL, 2014, 52 (11) : 2471 - 2479
  • [10] An experimental study of the nozzle lip thickness effect on supersonic jet screech tones
    Aoki, T
    Kweon, YH
    Miyazato, Y
    Kim, HD
    Setoguchi, T
    [J]. JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2006, 20 (04) : 522 - 532