Experimental investigation of interactions between turbulent cylinder wake and spherical shock wave

被引:8
|
作者
Aruga, Kenta [1 ]
Inokuma, Kento [1 ]
Watanabe, Tomoaki [1 ]
Nagata, Koji [1 ]
Sakai, Yasuhiko [2 ]
机构
[1] Nagoya Univ, Dept Aerosp Engn, Nagoya, Aichi, Japan
[2] Nagoya Univ, Dept Mech Syst Engn, Nagoya, Aichi, Japan
关键词
SONIC-BOOM; ATMOSPHERE; SIMULATION;
D O I
10.1063/1.5128267
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Interactions between a spherical shock wave and a turbulent cylinder wake are studied with wind tunnel experiments. The shock wave is generated outside the wake and propagates across the turbulent wake. Instantaneous streamwise velocity is measured on the wake centerline while peak overpressure of the shock wave is measured outside the wake after the shock wave has passed across the wake. The experiments are performed for various conditions of the cylinder wake to investigate the influences of the root-mean-squared (rms) velocity fluctuation and of the length of the turbulent region through which the shock wave propagates. The velocity fluctuation opposite to the shock propagation direction is positively correlated with the peak-overpressure fluctuation. The mean peak overpressure decreases after the shock wave propagates in the wake. These relations between velocity and peak overpressure are explained by the shock-surface deformation, where the peak overpressure is increased and decreased, respectively, for the shock surfaces with concave and convex shapes in relation to the shock propagation direction. The correlation coefficients between the velocity and peak-overpressure fluctuations and the rms peak-overpressure fluctuation increase with the rms velocity fluctuation. The rms peak-overpressure fluctuation becomes independent of the turbulent length on the shock ray once the shock wave has propagated through a sufficiently long turbulent region. The peak-overpressure fluctuation has a probability density function (PDF) close to a Gaussian shape even though the PDF of velocity fluctuations in the wake is negatively skewed.
引用
收藏
页数:12
相关论文
共 50 条
  • [1] Experimental investigation of interactions between laminar or turbulent boundary layer and shock wave
    Quan Peng-Cheng
    Yi Shi-He
    Wu Yu
    Zhu Yang-Zhu
    Chen Zhi
    ACTA PHYSICA SINICA, 2014, 63 (08)
  • [2] Experimental investigation of cylindrical shock wave interactions
    Rabinowitz, Grace I.
    Wilson, Finnegan
    Bjerke, Gabriel
    Tucker, Kadyn J.
    Kustic, Russell R.
    Nederbragt, Joshua G.
    Anderson, Mitchell P.
    Golson, Jacob
    Morales, Rodrigo Chaves
    Eliasson, Veronica
    MULTISCALE AND MULTIDISCIPLINARY MODELING EXPERIMENTS AND DESIGN, 2024, 7 (03) : 2635 - 2647
  • [3] Characteristics of the cylinder-induced shock wave and turbulent boundary layer interactions
    Gang, Dun-dian
    Yi, Shi-he
    He, Lin
    JOURNAL OF VISUALIZATION, 2016, 19 (04) : 581 - 585
  • [4] Experimental investigation of axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions
    Murray, N.
    Hillier, R.
    Williams, S.
    JOURNAL OF FLUID MECHANICS, 2013, 714 : 152 - 189
  • [5] Characteristics of the cylinder-induced shock wave and turbulent boundary layer interactions
    Dun-dian Gang
    Shi-he Yi
    Lin He
    Journal of Visualization, 2016, 19 : 581 - 585
  • [6] Numerical investigation of optical distortions by turbulent wake and shock wave in the transonic flow
    Tan, Xiao-Tong
    Xu, He-Yong
    Yin, Kai
    PHYSICS OF FLUIDS, 2024, 36 (03)
  • [7] EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A SHOCK-WAVE IMPINGEMENT ON A CYLINDER
    BROSH, A
    KUSSOY, MI
    HUNG, CM
    AIAA JOURNAL, 1985, 23 (06) : 840 - 846
  • [8] EXPERIMENTAL INVESTIGATION OF THE WAKE OF A DISCONTINUOUS CYLINDER
    Mandava, V. S. R.
    Kopp, Gregory A.
    Herrero, Joan
    Giralt, Francesc
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER CONFERENCE - 2010 - VOL 1, PTS A-C, 2010, : 871 - 879
  • [9] Inviscid interactions between an oblique shock wave and a concave cylinder
    Yan B.
    Hong Y.
    Li Y.
    Li Z.
    Tuijin Jishu/Journal of Propulsion Technology, 2024, 45 (01):
  • [10] Experimental investigation into the interaction of the stationary shock wave with the turbulent layer
    Pavlenko, AV
    Baishev, AI
    Kucherenko, YA
    Litvin, AT
    Sorokatyi, NN
    LASER AND PARTICLE BEAMS, 2000, 18 (02) : 171 - 174