TY - GEN
T1 - Large-eddy simulation of MHD turbulent duct flows using a dynamic subgrid-scale model
AU - Kobayashi, Hiromichi
PY - 2007
Y1 - 2007
N2 - At low magnetic Reynolds number, turbulent duct flows in a uniform magnetic field are examined using large-eddy simulation to reveal a sidewall effect on the skin friction. The duct has a square cross section and entirely insulated walls. The duct flow has two kinds of boundary layers: Hartmann layer and sidewall layer. The Hartmann layer is located on the wall perpendicular to the magnetic field, while the sidewall layer exists on the wall parallel to the magnetic field. As the magnetic field increases in the range of turbulent flows, the Hartmann layer becomes thin because of the "Hartmann flattening" -flattening effect of the flow by the Lorentz force. The sidewall layer, however, becomes thick because of the turbulence suppression until the laminarization takes place. When the Reynolds number Re based on the hydraulic diameter, molecular viscosity, and bulk velocity is 5300, the Hartmann and sidewall layers are laminarized at the same Hartmann number that is proportional to the magnetic field. When the Hartmann layer is laminarized at Re = 29000, the sidewall layer remains turbulence. This allows the skin friction to become maximum. When the sidewall layer is laminarized, the flow totally becomes laminar and the skin friction becomes minimum.
AB - At low magnetic Reynolds number, turbulent duct flows in a uniform magnetic field are examined using large-eddy simulation to reveal a sidewall effect on the skin friction. The duct has a square cross section and entirely insulated walls. The duct flow has two kinds of boundary layers: Hartmann layer and sidewall layer. The Hartmann layer is located on the wall perpendicular to the magnetic field, while the sidewall layer exists on the wall parallel to the magnetic field. As the magnetic field increases in the range of turbulent flows, the Hartmann layer becomes thin because of the "Hartmann flattening" -flattening effect of the flow by the Lorentz force. The sidewall layer, however, becomes thick because of the turbulence suppression until the laminarization takes place. When the Reynolds number Re based on the hydraulic diameter, molecular viscosity, and bulk velocity is 5300, the Hartmann and sidewall layers are laminarized at the same Hartmann number that is proportional to the magnetic field. When the Hartmann layer is laminarized at Re = 29000, the sidewall layer remains turbulence. This allows the skin friction to become maximum. When the sidewall layer is laminarized, the flow totally becomes laminar and the skin friction becomes minimum.
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U2 - 10.2514/6.2007-4369
DO - 10.2514/6.2007-4369
M3 - Conference contribution
AN - SCOPUS:35649028766
SN - 1563479001
SN - 9781563479007
T3 - Collection of Technical Papers - 38th AIAA Plasmadynamics and Lasers Conference
SP - 688
EP - 704
BT - Collection of Technical Papers - 38th AIAA Plasmadynamics and Lasers Conference
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 38th AIAA Plasmadynamics and Lasers Conference
Y2 - 25 June 2007 through 28 June 2007
ER -