TY - GEN
T1 - Control of near-wall streamwise vortices using an electromagnetic force in a conducting fluid
AU - Choi, Haecheon
AU - Lee, Donghoon
AU - Lim, Junwoo
AU - Kim, John
N1 - Publisher Copyright:
© 1997 by American Institute of Aeronautics and Astronautics. Inc. All rights reserved.
PY - 1997
Y1 - 1997
N2 - Effects of electromagnetic forcing on the near-wall vortices are investigated by applying a uniform magnetic flux in a turbulent channel flow in the streamwise and spanwise directions, respectively. The electromagnetic force induced from the magnetic fluxes inhibits the motion induced by the streamwise vortices and reduces their strength, and thus drag is significantly reduced. The wall-normal and spanwise turbulence intensities and the Reynolds shear stress decrease with the increased magnetic flux in both directions. The streamwise turbulence intensity increases with the streamwise magnetic flux, whereas it decreases with the spanwise magnetic flux. It is also shown that the spanwise magnetic flux is much more effective than the streamwise magnetic flux in reducing the skin-friction drag in the turbulent channel flow.
AB - Effects of electromagnetic forcing on the near-wall vortices are investigated by applying a uniform magnetic flux in a turbulent channel flow in the streamwise and spanwise directions, respectively. The electromagnetic force induced from the magnetic fluxes inhibits the motion induced by the streamwise vortices and reduces their strength, and thus drag is significantly reduced. The wall-normal and spanwise turbulence intensities and the Reynolds shear stress decrease with the increased magnetic flux in both directions. The streamwise turbulence intensity increases with the streamwise magnetic flux, whereas it decreases with the spanwise magnetic flux. It is also shown that the spanwise magnetic flux is much more effective than the streamwise magnetic flux in reducing the skin-friction drag in the turbulent channel flow.
UR - https://www.scopus.com/pages/publications/84983122056
M3 - Conference contribution
AN - SCOPUS:84983122056
SN - 9780000000002
T3 - 4th Shear Flow Control Conference
BT - 4th Shear Flow Control Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 4th AIAA Shear Flow Control Conference, 1997
Y2 - 29 June 1997 through 2 July 1997
ER -