Three-dimensional vortex organization in a high-Reynolds-number supersonic turbulent boundary layer

被引:117
|
作者
Elsinga, G. E. [1 ]
Adrian, R. J. [2 ]
van Oudheusden, B. W. [1 ]
Scarano, F. [1 ]
机构
[1] Delft Univ Technol, Dept Aerosp Engn, NL-2629 HS Delft, Netherlands
[2] Arizona State Univ, Dept Mech & Aerosp Engn, Tempe, AZ 85287 USA
关键词
PARTICLE IMAGE VELOCIMETRY; LARGE-SCALE MOTIONS; DIRECT NUMERICAL-SIMULATION; COHERENT MOTIONS; OUTER REGION; PACKETS; CHANNEL; FLOWS;
D O I
10.1017/S0022112009992047
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Tomographic particle image velocimetry was used to quantitatively visualize the three-dimensional coherent structures in a supersonic (Mach 2) turbulent boundary layer in the region between gamma/delta = 0.15 and 0.89. The Reynolds number based on momentum thickness Re-theta = 34 000. The instantaneous velocity fields give evidence of hairpin vortices aligned in the streamwise direction forming very long zones of low-speed fluid, consistent with Tomkins & Adrian (J. Fluid Mech., vol. 490, 2003, p. 37). The observed hairpin structure is also a statistically relevant structure as is shown by the conditional average flow field associated to spanwise swirling motion. Spatial low-pass filtering of the velocity field reveals streamwise vortices and signatures of large-scale hairpins (height > 0.5 delta), which are weaker than the smaller scale hairpins in the unfiltered velocity field. The large-scale hairpin structures in the instantaneous velocity fields are observed to be aligned in the streamwise direction and spanwise organized along diagonal lines. Additionally the autocorrelation function of the wall-normal swirling motion representing the large-scale hairpin structure returns positive correlation peaks in the streamwise direction (at 1.5 delta distance from the DC peak) and along the 45 degrees diagonals, which also suggest a periodic arrangement in those directions. This is evidence for the existence of a spanwise-stream wise organization of the coherent structures in a fully turbulent boundary layer.
引用
收藏
页码:35 / 60
页数:26
相关论文
共 50 条
  • [21] Validation case for supersonic boundary layer and turbulent aero-optical investigation in high-Reynolds-number freestream by WCNS-E-5
    Sun, Xi-Wan
    Liu, Wei
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2020, 234 (15) : 2153 - 2166
  • [22] Dynamics and scaling of particle streaks in high-Reynolds-number turbulent boundary layers
    Berk, Tim
    Coletti, Filippo
    JOURNAL OF FLUID MECHANICS, 2023, 975
  • [23] Direct numerical simulation of a microramp in a high-Reynolds number supersonic turbulent boundary layer
    Salvadore, Francesco
    Memmolo, Antonio
    Modesti, Davide
    Della Posta, Giacomo
    Bernardini, Matteo
    PHYSICAL REVIEW FLUIDS, 2023, 8 (11)
  • [24] Trajectory of a synthetic jet issuing into high-Reynolds-number turbulent boundary layers
    Berk, Tim
    Hutchins, Nicholas
    Marusic, Ivan
    Ganapathisubramani, Bharathram
    JOURNAL OF FLUID MECHANICS, 2018, 856 : 531 - 551
  • [25] Study of the near-wall-turbulent region of the high-Reynolds-number boundary layer using an atmospheric flow
    Kunkel, GJ
    Marusic, I
    JOURNAL OF FLUID MECHANICS, 2006, 548 (375-402) : 375 - 402
  • [26] Instability of a Three-Dimensional Supersonic Boundary Layer
    Journal of Applied Mechanics and Technical Physics (English translation of PMTF, Zhurnal Prikladnoi Mekhaniki i Tekhnicheskoi Fiziki), 1995, 36 (06):
  • [27] Instability of a three-dimensional supersonic boundary layer
    Levchenko, VY
    Kosinov, AD
    Semionov, NV
    Ermolaev, YG
    IUTAM SYMPOSIUM ON NONLINEAR INSTABILITY AND TRANSITION IN THREE-DIMENSIONAL BOUNDARY LAYERS, 1996, 35 : 361 - 368
  • [28] Some Reynolds number effects on two- and three-dimensional turbulent boundary layers
    Ölçmen, MS
    Simpson, RL
    George, J
    EXPERIMENTS IN FLUIDS, 2001, 31 (02) : 219 - 228
  • [29] Turbulence measurements for a longitudinal vortex interacting with a three-dimensional turbulent boundary layer
    Shizawa, Takaaki
    Eaton, John K.
    AIAA journal, 1992, 30 (01): : 49 - 55
  • [30] Some Reynolds number effects on two- and three-dimensional turbulent boundary layers
    M. S. Ölçmen
    R. L. Simpson
    J. George
    Experiments in Fluids, 2001, 31 : 219 - 228