Scalar Spatial Correlations in a Supersonic Mixing Flowfield

被引:6
|
作者
Takahashi, Hidemi
Oso, Hiroki [1 ]
Kouchi, Toshinori [1 ]
Masuya, Goro [1 ]
Hirota, Mitsutomo [2 ]
机构
[1] Tohoku Univ, Dept Aerosp Engn, Sendai, Miyagi 9808579, Japan
[2] Muroran Inst Technol, Dept Mech Syst Engn, Muroran, Hokkaido 0508585, Japan
关键词
TURBULENT-BOUNDARY-LAYER; TRANSVERSE INJECTION; CROSS-FLOW; JET; VORTICES; DENSITY;
D O I
10.2514/1.44684
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Single-time two-point spatial correlations of injectant concentrations in the supersonic mixing flowfield produced by a sonic transverse injection of air into a Mach 2.0 supersonic airstream were investigated using acetone planar laser-induced fluorescence data. Side-view and end-view, contour maps were obtained in several planes to characterize the turbulent structure and three-dimensionality of the mixing flowfield. The correlation maps indicated an organized large-scale structure in the upper region of the jet. The side-view correlation maps revealed that the shape of the large dominating structure was elliptic and that its major axis turned from backward-leaning to forward-leaning as the reference point of correlation moved downstream. The end-view correlation maps showed that the instantaneous jet plume appeared by turns either in the top or in the lower sides of the time-averaged injectant plume in each cross section.
引用
收藏
页码:443 / 452
页数:10
相关论文
共 50 条
  • [31] THEORETICAL AND EXPERIMENTAL DESCRIPTION FOR A RADIAL SUPERSONIC FLOWFIELD.
    Rapagnani, N.L.
    Zumpano, F.R.
    1758, (24):
  • [32] Measurement of Supersonic Injection Flowfield Using Acetone PLIF
    Takahashi, Hidemi
    Hirota, Mitsutomo
    Oso, Hiroki
    Masuya, Goro
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2009, 51 (174) : 252 - 258
  • [33] The spatial growth of supersonic reacting mixing layers: Effects of combustion mode
    Chen, Qian
    Wang, Bing
    AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 116 (116)
  • [34] Flowfield characteristics on a vent slot mixer in supersonic flow
    C. Kim
    K. Sung
    I.-S. Jeung
    B. Choi
    T. Kouchi
    G. Masuya
    Shock Waves, 2010, 20 : 559 - 569
  • [35] Flowfield and noise characteristics of twin supersonic impinging jets
    Choutapalli, Isaac M.
    Krothapalli, Anjaneyulu
    Alkislar, Mehmet B.
    Lourenco, Luiz M.
    AIAA JOURNAL, 2007, 45 (04) : 793 - 805
  • [36] Flowfield near a mulitiport injector array in a supersonic flow
    Jacobsen, LS
    Schetz, JA
    Ng, WF
    JOURNAL OF PROPULSION AND POWER, 2000, 16 (02) : 216 - 226
  • [37] AFTERBODY FLOWFIELD COMPUTATIONS AT TRANSONIC AND SUPERSONIC MACH NUMBERS
    GOLDBERG, UC
    GORSKI, JJ
    CHAKRAVARTHY, SR
    JOURNAL OF PROPULSION AND POWER, 1987, 3 (01) : 56 - 62
  • [38] INFLUENCE OF A SUPERSONIC FLOWFIELD ON ELASTIC STABILITY OF CYLINDRICAL SHELLS
    BARR, GW
    STEARMAN, RO
    AIAA JOURNAL, 1970, 8 (06) : 993 - &
  • [39] Flowfield characteristics of swept struts in supersonic annular flow
    Williams, KE
    Gessner, FB
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2000, 21 (03) : 278 - 284
  • [40] Comparative analysis of computational methods of supersonic combustor flowfield
    Wang, Cheng-Peng
    Yang, Yong-Yang
    Liu, Chen
    Wang, Jiang-Feng
    Cheng, Ke-Ming
    Wu, Yi-Zhao
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (05): : 963 - 969