TY - GEN
T1 - Coherent structures in DNS of turbulent boundary layers at Mach 3
AU - Ringuette, Matthew J.
AU - Wu, Minwei
AU - Martín, M. Pino
PY - 2007
Y1 - 2007
N2 - We demonstrate that the data from DNS of turbulent boundary layers at Mach 3 exhibit the same local flow features found in both supersonic and incompressible experiments, such as long, low-speed structures in the log region and hairpin vortex packets. Instantaneous plots of the streamwise mass-flux show very long low-momentum structures in the log layer. We use Taylor's hypothesis to generate a velocity map in the log region with a streamwise length of about 2305, where δ is the boundary layer thickness. The map indicates that the low-speed structures attain streamwise lengths of order 1005. Length scales obtained from correlations of the streamwise mass flux severely under predict the extent of these structures, most likely due to their significant meandering in the spanwise direction. A hairpin packet-finding algorithm is employed to determine the average packet properties, and we find that the streamwise length of the Mach 3 packets is less than one-third of that observed at subsonic conditions. Adopting the technique of Brown & Thomas, 1 we observe a connection between elevated levels of wall shear stress and hairpin packets. Visualization of the instantaneous turbulence structure shows that groups of hairpin packets are frequently located above the long, low-momentum structures, consistent with the very large-scale motion model of Kim & Adrian.2.
AB - We demonstrate that the data from DNS of turbulent boundary layers at Mach 3 exhibit the same local flow features found in both supersonic and incompressible experiments, such as long, low-speed structures in the log region and hairpin vortex packets. Instantaneous plots of the streamwise mass-flux show very long low-momentum structures in the log layer. We use Taylor's hypothesis to generate a velocity map in the log region with a streamwise length of about 2305, where δ is the boundary layer thickness. The map indicates that the low-speed structures attain streamwise lengths of order 1005. Length scales obtained from correlations of the streamwise mass flux severely under predict the extent of these structures, most likely due to their significant meandering in the spanwise direction. A hairpin packet-finding algorithm is employed to determine the average packet properties, and we find that the streamwise length of the Mach 3 packets is less than one-third of that observed at subsonic conditions. Adopting the technique of Brown & Thomas, 1 we observe a connection between elevated levels of wall shear stress and hairpin packets. Visualization of the instantaneous turbulence structure shows that groups of hairpin packets are frequently located above the long, low-momentum structures, consistent with the very large-scale motion model of Kim & Adrian.2.
UR - https://www.scopus.com/pages/publications/34250797323
U2 - 10.2514/6.2007-1138
DO - 10.2514/6.2007-1138
M3 - Conference contribution
AN - SCOPUS:34250797323
SN - 1563478900
SN - 9781563478901
T3 - Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
SP - 13769
EP - 13781
BT - Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 45th AIAA Aerospace Sciences Meeting 2007
Y2 - 8 January 2007 through 11 January 2007
ER -