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

被引:115
|
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
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